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@@ -0,0 +1,6 @@
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+383
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@@ -1,6 +1,387 @@
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## Ignore Visual Studio temporary files, build results, and
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||||
## files generated by popular Visual Studio add-ons.
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##
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## Get latest from https://github.com/github/gitignore/blob/master/VisualStudio.gitignore
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# User-specific files
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*.rsuser
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*.suo
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*.user
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*.userosscache
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*.sln.docstates
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# User-specific files (MonoDevelop/Xamarin Studio)
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*.userprefs
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# Mono auto generated files
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mono_crash.*
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[Dd]ebug/
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[Dd]ebugPublic/
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[Rr]elease/
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[Rr]eleases/
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x64/
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[Ww][Ii][Nn]32/
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[Aa][Rr][Mm]/
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[Aa][Rr][Mm]64/
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[Bb]in/
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[Oo]bj/
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[Oo]ut/
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[Ll]og/
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[Ll]ogs/
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Generated\ Files/
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[Tt]est[Rr]esult*/
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[Bb]uild[Ll]og.*
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|
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*.VisualState.xml
|
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TestResult.xml
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nunit-*.xml
|
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# Build Results of an ATL Project
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[Dd]ebugPS/
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[Rr]eleasePS/
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dlldata.c
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# Benchmark Results
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BenchmarkDotNet.Artifacts/
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# .NET Core
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project.lock.json
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project.fragment.lock.json
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artifacts/
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ScaffoldingReadMe.txt
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StyleCopReport.xml
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*_i.c
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*_p.c
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*_h.h
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*.ilk
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*.meta
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*.iobj
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_Chutzpah*
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ipch/
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*.aps
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*.VC.VC.opendb
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*.vsp
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*.vspx
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*.sap
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*.e2e
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$tf/
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_ReSharper*/
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*.[Rr]e[Ss]harper
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_TeamCity*
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*.dotCover
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.axoCover/*
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coverage*.json
|
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coverage*.xml
|
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coverage*.info
|
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||||
# Visual Studio code coverage results
|
||||
*.coverage
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*.coveragexml
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|
||||
_NCrunch_*
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.*crunch*.local.xml
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nCrunchTemp_*
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|
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# MightyMoose
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*.mm.*
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AutoTest.Net/
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# Web workbench (sass)
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.sass-cache/
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# Installshield output folder
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[Ee]xpress/
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DocProject/buildhelp/
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DocProject/Help/*.HxT
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DocProject/Help/*.HxC
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DocProject/Help/*.hhc
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DocProject/Help/*.hhk
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DocProject/Help/*.hhp
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DocProject/Help/Html2
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DocProject/Help/html
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# Click-Once directory
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publish/
|
||||
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||||
# Publish Web Output
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||||
*.[Pp]ublish.xml
|
||||
*.azurePubxml
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||||
# Note: Comment the next line if you want to checkin your web deploy settings,
|
||||
# but database connection strings (with potential passwords) will be unencrypted
|
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*.pubxml
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*.publishproj
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# Microsoft Azure Web App publish settings. Comment the next line if you want to
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||||
# checkin your Azure Web App publish settings, but sensitive information contained
|
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# in these scripts will be unencrypted
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PublishScripts/
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|
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# NuGet Packages
|
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*.nupkg
|
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# NuGet Symbol Packages
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*.snupkg
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**/[Pp]ackages/*
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# except build/, which is used as an MSBuild target.
|
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!**/[Pp]ackages/build/
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#!**/[Pp]ackages/repositories.config
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|
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*.nuget.props
|
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*.nuget.targets
|
||||
|
||||
# Microsoft Azure Build Output
|
||||
csx/
|
||||
*.build.csdef
|
||||
|
||||
# Microsoft Azure Emulator
|
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ecf/
|
||||
rcf/
|
||||
|
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# Windows Store app package directories and files
|
||||
AppPackages/
|
||||
BundleArtifacts/
|
||||
Package.StoreAssociation.xml
|
||||
_pkginfo.txt
|
||||
*.appx
|
||||
*.appxbundle
|
||||
*.appxupload
|
||||
|
||||
# Visual Studio cache files
|
||||
# files ending in .cache can be ignored
|
||||
*.[Cc]ache
|
||||
# but keep track of directories ending in .cache
|
||||
!?*.[Cc]ache/
|
||||
|
||||
# Others
|
||||
ClientBin/
|
||||
~$*
|
||||
*~
|
||||
*.dbmdl
|
||||
*.dbproj.schemaview
|
||||
*.jfm
|
||||
*.pfx
|
||||
*.publishsettings
|
||||
orleans.codegen.cs
|
||||
|
||||
# Including strong name files can present a security risk
|
||||
# (https://github.com/github/gitignore/pull/2483#issue-259490424)
|
||||
#*.snk
|
||||
|
||||
# Since there are multiple workflows, uncomment next line to ignore bower_components
|
||||
# (https://github.com/github/gitignore/pull/1529#issuecomment-104372622)
|
||||
#bower_components/
|
||||
|
||||
# RIA/Silverlight projects
|
||||
Generated_Code/
|
||||
|
||||
# Backup & report files from converting an old project file
|
||||
# to a newer Visual Studio version. Backup files are not needed,
|
||||
# because we have git ;-)
|
||||
_UpgradeReport_Files/
|
||||
Backup*/
|
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UpgradeLog*.XML
|
||||
UpgradeLog*.htm
|
||||
ServiceFabricBackup/
|
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*.rptproj.bak
|
||||
|
||||
# SQL Server files
|
||||
*.mdf
|
||||
*.ldf
|
||||
*.ndf
|
||||
|
||||
# Business Intelligence projects
|
||||
*.rdl.data
|
||||
*.bim.layout
|
||||
*.bim_*.settings
|
||||
*.rptproj.rsuser
|
||||
*- [Bb]ackup.rdl
|
||||
*- [Bb]ackup ([0-9]).rdl
|
||||
*- [Bb]ackup ([0-9][0-9]).rdl
|
||||
|
||||
# Microsoft Fakes
|
||||
FakesAssemblies/
|
||||
|
||||
# GhostDoc plugin setting file
|
||||
*.GhostDoc.xml
|
||||
|
||||
# Node.js Tools for Visual Studio
|
||||
.ntvs_analysis.dat
|
||||
node_modules/
|
||||
|
||||
# Visual Studio 6 build log
|
||||
*.plg
|
||||
|
||||
# Visual Studio 6 workspace options file
|
||||
*.opt
|
||||
|
||||
# Visual Studio 6 auto-generated workspace file (contains which files were open etc.)
|
||||
*.vbw
|
||||
|
||||
# Visual Studio LightSwitch build output
|
||||
**/*.HTMLClient/GeneratedArtifacts
|
||||
**/*.DesktopClient/GeneratedArtifacts
|
||||
**/*.DesktopClient/ModelManifest.xml
|
||||
**/*.Server/GeneratedArtifacts
|
||||
**/*.Server/ModelManifest.xml
|
||||
_Pvt_Extensions
|
||||
|
||||
# Paket dependency manager
|
||||
.paket/paket.exe
|
||||
paket-files/
|
||||
|
||||
# FAKE - F# Make
|
||||
.fake/
|
||||
|
||||
# CodeRush personal settings
|
||||
.cr/personal
|
||||
|
||||
# Python Tools for Visual Studio (PTVS)
|
||||
__pycache__/
|
||||
*.pyc
|
||||
|
||||
# Cake - Uncomment if you are using it
|
||||
# tools/**
|
||||
# !tools/packages.config
|
||||
|
||||
# Tabs Studio
|
||||
*.tss
|
||||
|
||||
# Telerik's JustMock configuration file
|
||||
*.jmconfig
|
||||
|
||||
# BizTalk build output
|
||||
*.btp.cs
|
||||
*.btm.cs
|
||||
*.odx.cs
|
||||
*.xsd.cs
|
||||
|
||||
# OpenCover UI analysis results
|
||||
OpenCover/
|
||||
|
||||
# Azure Stream Analytics local run output
|
||||
ASALocalRun/
|
||||
|
||||
# MSBuild Binary and Structured Log
|
||||
*.binlog
|
||||
|
||||
# NVidia Nsight GPU debugger configuration file
|
||||
*.nvuser
|
||||
|
||||
# MFractors (Xamarin productivity tool) working folder
|
||||
.mfractor/
|
||||
|
||||
# Local History for Visual Studio
|
||||
.localhistory/
|
||||
|
||||
# BeatPulse healthcheck temp database
|
||||
healthchecksdb
|
||||
|
||||
# Backup folder for Package Reference Convert tool in Visual Studio 2017
|
||||
MigrationBackup/
|
||||
|
||||
# Ionide (cross platform F# VS Code tools) working folder
|
||||
.ionide/
|
||||
|
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# Fody - auto-generated XML schema
|
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FodyWeavers.xsda
|
||||
|
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# Custom
|
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|
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Packages
|
||||
_PackageInt
|
||||
PackagesMetadata
|
||||
PackageSources/js-bundle/__generated__
|
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PackageSources/js-bundle/.rollup.cache
|
||||
PackageSources/js-bundle/node_modules
|
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PackageSources/html_ui
|
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PackageSources/html_ui
|
||||
PackageSources/wasm-module/MSFS
|
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|
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node_modules
|
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|
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*.blend1
|
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*.tsbuildinfo
|
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|
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PackageSources/SimObjects/Airplanes/**/*.wasm
|
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EFB/efb.css
|
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EFB/efb.js
|
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EFB/efb.html
|
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EFB/efb.index.js
|
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EFB/patched/
|
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|
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*.su
|
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Vendored
+29
@@ -0,0 +1,29 @@
|
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{
|
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|
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{
|
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"name": "Win32",
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|
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"C:\\MSFS 2024 SDK\\WASM\\wasi-sysroot\\include\\c++\\v1",
|
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"C:\\MSFS 2024 SDK\\WASM\\include",
|
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"C:\\MSFS 2024 SDK\\SimConnect SDK\\include"
|
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],
|
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"defines": [
|
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"_DEBUG",
|
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"UNICODE",
|
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"_UNICODE"
|
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],
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"compilerArgs": [
|
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"/Zc:__cplusplus"
|
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],
|
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"windowsSdkVersion": "10.0.26100.0",
|
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"compilerPath": "cl.exe",
|
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"cStandard": "c17",
|
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"intelliSenseMode": "windows-msvc-x64",
|
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"cppStandard": "c++14"
|
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}
|
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],
|
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"version": 4
|
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|
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Vendored
+3
@@ -18,5 +18,8 @@
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"[xml]": {
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|
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},
|
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"[typescriptreact]": {
|
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|
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}
|
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}
|
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@@ -0,0 +1,14 @@
|
||||
Index: EFB.html
|
||||
===================================================================
|
||||
--- EFB.html
|
||||
+++ EFB.html
|
||||
@@ -4,7 +4,8 @@
|
||||
</div>
|
||||
</script>
|
||||
|
||||
|
||||
-<script type="text/html" import-async="false" import-script="/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.index.js"></script>
|
||||
+<script type="text/html" import-async="false" import-script="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/efb.index.js"></script>
|
||||
|
||||
<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.css" />
|
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+<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.css" />
|
||||
@@ -0,0 +1,15 @@
|
||||
Index: EFB.index.js
|
||||
===================================================================
|
||||
--- EFB.index.js
|
||||
+++ EFB.index.js
|
||||
@@ -27,9 +27,9 @@
|
||||
}
|
||||
|
||||
connectedCallback() {
|
||||
super.connectedCallback();
|
||||
- Include.addScript("/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.js");
|
||||
+ Include.addScript("/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/efb.js");
|
||||
}
|
||||
|
||||
Update() {
|
||||
super.Update();
|
||||
@@ -0,0 +1,46 @@
|
||||
Index: EFB.js
|
||||
===================================================================
|
||||
--- EFB.js
|
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+++ EFB.js
|
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@@ -50833,11 +50833,11 @@
|
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),
|
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/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
|
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"button",
|
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{
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- onClick: loadPayload,
|
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+ onClick: () => dispatch(setRoute({ path: "/payload" })),
|
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className: "middle none center rounded-lg bg-green-700 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none",
|
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- children: "Set payload & fuel"
|
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+ children: "Manage payload & fuel"
|
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}
|
||||
),
|
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/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
|
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"button",
|
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@@ -51343,8 +51343,27 @@
|
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] })
|
||||
] }) }) });
|
||||
}
|
||||
|
||||
+// Exports for add. script
|
||||
+ window.reactExports = __toESM(require_react());
|
||||
+ window.reactDomExports = __toESM(require_react_dom());
|
||||
+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
|
||||
+ window.useSelector = useSelector;
|
||||
+ window.v4 = v4_default;
|
||||
+ window.ArrowBigUp = ArrowBigUp;
|
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+ window.Delete = Delete;
|
||||
+ window.Space = Space;
|
||||
+ window.X = X;
|
||||
+ // Include
|
||||
+ var script = document.createElement('script');
|
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+ script.onload = function () {
|
||||
+ console.log("LM App injected");
|
||||
+ routes["/payload"].page = window.KH_LM
|
||||
+ };
|
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+ script.src = "/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.js";
|
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+ document.head.appendChild(script); //or something of the likes
|
||||
+
|
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// src/components/Router.tsx
|
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init_common();
|
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var import_jsx_runtime15 = __toESM(require_jsx_runtime());
|
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var routes = {
|
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@@ -0,0 +1,26 @@
|
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const { createTwoFilesPatch } = require("diff");
|
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const fs = require("fs");
|
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|
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// HTML
|
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|
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let file1Contents = fs.readFileSync("EFB.html").toString();
|
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let file2Contents = fs.readFileSync("patched/EFB.html").toString();
|
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let patch = createTwoFilesPatch(
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"EFB.html",
|
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"EFB.html",
|
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file1Contents,
|
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file2Contents
|
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);
|
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fs.writeFileSync("efb-html.patch", patch);
|
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|
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// JS
|
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|
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file1Contents = fs.readFileSync("EFB.index.js").toString();
|
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file2Contents = fs.readFileSync("patched/EFB.index.js").toString();
|
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patch = createTwoFilesPatch("EFB.index.js", "EFB.index.js", file1Contents, file2Contents);
|
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fs.writeFileSync("efb-index-js.patch", patch);
|
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|
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file1Contents = fs.readFileSync("EFB.js").toString();
|
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file2Contents = fs.readFileSync("patched/EFB.js").toString();
|
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patch = createTwoFilesPatch("EFB.js", "EFB.js", file1Contents, file2Contents);
|
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fs.writeFileSync("efb-js.patch", patch);
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style="display:inline;fill:none;stroke:#646464;stroke-width:4;stroke-linecap:butt;stroke-linejoin:miter;stroke-dasharray:none;stroke-dashoffset:0;stroke-opacity:1"
|
||||
d="m 1735.962,616.7647 v 84.15891 z m 657.6119,99.08378 v 43.38354 z" /></svg>
|
||||
|
After Width: | Height: | Size: 6.8 KiB |
@@ -1,5 +1,5 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<AssetPackage Version="0.1.0">
|
||||
<AssetPackage Version="1.3.0">
|
||||
<ItemSettings>
|
||||
<ContentType>MISC</ContentType>
|
||||
<Title>TFDi Design MD-11 Load Manager</Title>
|
||||
@@ -10,31 +10,37 @@
|
||||
<VisibleInStore>false</VisibleInStore>
|
||||
<CanBeReferenced>false</CanBeReferenced>
|
||||
</Flags>
|
||||
<PackageOrderHint>CUSTOM_SIMOBJECTS_PATCH</PackageOrderHint>
|
||||
<AssetGroups>
|
||||
<AssetGroup Name="ContentInfo">
|
||||
<Type>ContentInfo</Type>
|
||||
<Type Version="0">ContentInfo</Type>
|
||||
<Flags>
|
||||
<FSXCompatibility>false</FSXCompatibility>
|
||||
</Flags>
|
||||
<AssetDir>PackageDefinitions\xkhofmann-tfdidesign-md11-load-manager\ContentInfo</AssetDir>
|
||||
<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager</OutputDir>
|
||||
<AssetDir>PackageDefinitions\xkhofmann-tfdidesign-md11-load-manager\ContentInfo\</AssetDir>
|
||||
<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
|
||||
</AssetGroup>
|
||||
<AssetGroup Name="html-ui">
|
||||
<Type>Copy</Type>
|
||||
<Type Version="0">Copy</Type>
|
||||
<Flags>
|
||||
<FSXCompatibility>false</FSXCompatibility>
|
||||
</Flags>
|
||||
<AssetDir>PackageSources\html_ui\</AssetDir>
|
||||
<OutputDir>html_ui\</OutputDir>
|
||||
<Config>
|
||||
<Exclude>vendor-*</Exclude>
|
||||
</Config>
|
||||
</AssetGroup>
|
||||
<AssetGroup Name="load-manager-panel">
|
||||
<Type>SPB</Type>
|
||||
<AssetGroup Name="wasm">
|
||||
<Type Version="0">Copy</Type>
|
||||
<Flags>
|
||||
<FSXCompatibility>false</FSXCompatibility>
|
||||
</Flags>
|
||||
<AssetDir>PackageSources\load-manager-panel\</AssetDir>
|
||||
<OutputDir>InGamePanels\</OutputDir>
|
||||
<AssetDir>PackageSources\SimObjects\Airplanes\</AssetDir>
|
||||
<OutputDir>SimObjects\Airplanes\</OutputDir>
|
||||
<Config>
|
||||
<Exclude>.gitkeep</Exclude>
|
||||
</Config>
|
||||
</AssetGroup>
|
||||
</AssetGroups>
|
||||
</AssetPackage>
|
||||
|
||||
|
||||
@@ -0,0 +1,59 @@
|
||||
// Panel Configuration File
|
||||
// TFDi Design MD-11
|
||||
|
||||
[VCockpit01]
|
||||
size_mm=2048,2048
|
||||
visible=1
|
||||
pixel_size=2048,2048
|
||||
texture=vc1
|
||||
background_color=0,0,0
|
||||
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU1,0,0,509,510
|
||||
htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU2,514,0,510,510
|
||||
htmlgauge02=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU3,1027,0,510,510
|
||||
htmlgauge03=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU4,1539,0,510,510
|
||||
htmlgauge04=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU5,0,513,511,510
|
||||
htmlgauge05=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU6,513,512,510,511
|
||||
htmlgauge06=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=LMCDU, 0,1050,666,574
|
||||
htmlgauge07=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RMCDU,678,1050,666,574
|
||||
htmlgauge08=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=CMCDU,1353,1050,666,574
|
||||
htmlgauge09=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=ISFD,1032,519,544,505
|
||||
htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core,0,0,1,1
|
||||
//KH new gauge
|
||||
htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
|
||||
|
||||
[VIEWS]
|
||||
VIEW_FORWARD_DIR=2.000, 0.000, 0.000
|
||||
|
||||
[Color]
|
||||
Day=255,255,255
|
||||
Night=255,255,255
|
||||
Luminous=201,64,64
|
||||
|
||||
[Vcockpit02]
|
||||
Background_color=0,0,0
|
||||
size_mm=1024,1024
|
||||
visible=1
|
||||
pixel_size=1024,1024
|
||||
texture=vc2
|
||||
|
||||
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=AFS,3,0,1015,185
|
||||
htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=FUEL,4,200,1016,196
|
||||
//above should actually be 3,192,1018,199 - moved due to visual offset
|
||||
|
||||
[Vcockpit03]
|
||||
Background_color=0,0,0
|
||||
size_mm=1024,1024
|
||||
visible=1
|
||||
pixel_size=1024,1024
|
||||
texture=RADIOS_XPNDR
|
||||
|
||||
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RADIOS_XPNDR,0,5,1019,295
|
||||
|
||||
[VCockpit04]
|
||||
Background_color=0,0,0
|
||||
size_mm=1536,1024
|
||||
visible=1
|
||||
pixel_size=1536,1024
|
||||
texture=EFB
|
||||
|
||||
htmlgauge00=aircraft_efb/KH_TFDi_MD11_efb/efb.html,0,0,1536,1024
|
||||
+418
@@ -0,0 +1,418 @@
|
||||
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 283975
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 21
|
||||
//KH START Empty default
|
||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
|
||||
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
|
||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
||||
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
|
||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
||||
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 202.16
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 13
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
|
||||
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
|
||||
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
|
||||
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
|
||||
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+418
@@ -0,0 +1,418 @@
|
||||
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 283975
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 21
|
||||
//KH START Empty default
|
||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
|
||||
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
|
||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
||||
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
|
||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
||||
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 202.16
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 13
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
|
||||
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
|
||||
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
|
||||
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
|
||||
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+417
@@ -0,0 +1,417 @@
|
||||
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 283975
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 21
|
||||
//KH START Empty default
|
||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
|
||||
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
|
||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
||||
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
|
||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
||||
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 200.92
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 13
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
|
||||
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
|
||||
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
|
||||
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
|
||||
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+419
@@ -0,0 +1,419 @@
|
||||
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 283975
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 21
|
||||
//KH START Empty default
|
||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
|
||||
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
|
||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
||||
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
|
||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
||||
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 200.92
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 13
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
|
||||
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
|
||||
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
|
||||
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
|
||||
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+409
@@ -0,0 +1,409 @@
|
||||
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 248567
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 15
|
||||
//KH START Empty default
|
||||
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
|
||||
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
|
||||
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||
station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
|
||||
station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
|
||||
station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
|
||||
station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
|
||||
station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
|
||||
station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
|
||||
station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
|
||||
station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 202.16
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 8
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+409
@@ -0,0 +1,409 @@
|
||||
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 248567
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 15
|
||||
//KH START Empty default
|
||||
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
|
||||
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
|
||||
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||
station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
|
||||
station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
|
||||
station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
|
||||
station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
|
||||
station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
|
||||
station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
|
||||
station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
|
||||
station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 202.16
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 8
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+408
@@ -0,0 +1,408 @@
|
||||
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 248567
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 15
|
||||
//KH START Empty default
|
||||
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
|
||||
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
|
||||
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||
station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
|
||||
station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
|
||||
station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
|
||||
station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
|
||||
station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
|
||||
station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
|
||||
station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
|
||||
station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 200.92
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 8
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
+408
@@ -0,0 +1,408 @@
|
||||
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
|
||||
|
||||
[MODULAR_MERGE]
|
||||
auto = true
|
||||
|
||||
[VERSION]
|
||||
//KH Bump major
|
||||
major = 4
|
||||
minor = 8
|
||||
|
||||
[WEIGHT_AND_BALANCE]
|
||||
max_gross_weight = 630500
|
||||
empty_weight = 248567
|
||||
reference_datum_position = 0, 0, 0
|
||||
empty_weight_CG_position = -10.0, 0, 0
|
||||
CG_forward_limit = 0.12
|
||||
CG_aft_limit = 0.34
|
||||
empty_weight_pitch_MOI = 20897456
|
||||
empty_weight_roll_MOI = 6368555
|
||||
empty_weight_yaw_MOI = 40761191
|
||||
empty_weight_coupled_MOI = 0
|
||||
activate_mach_limit_based_on_cg = 0
|
||||
activate_cg_limit_based_on_mach = 0
|
||||
max_number_of_stations = 15
|
||||
//KH START Empty default
|
||||
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||
station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
||||
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
|
||||
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
|
||||
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||
station_load.6=0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
|
||||
station_load.7=0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
|
||||
station_load.8=0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
|
||||
station_load.9=0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
|
||||
station_load.10=0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
|
||||
station_load.11=0, 30.0, 0.0, -4.5, Lower forward cargo, 0
|
||||
station_load.12=0, -30.0, 0.0, -4.5, Lower rear cargo, 0
|
||||
station_load.13=0, 5.0, -2.0, -4.5, Left aux tank, 0
|
||||
station_load.14=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||
//KH END
|
||||
|
||||
[CONTACT_POINTS]
|
||||
static_pitch = 0
|
||||
static_cg_height = 16.4
|
||||
gear_system_type = 1
|
||||
tailwheel_lock = 0
|
||||
max_number_of_points = 16
|
||||
gear_locked_on_ground = 0
|
||||
gear_locked_above_speed = -1
|
||||
max_speed_full_steering = 25
|
||||
min_available_steering_angle_pct = 0.2
|
||||
max_speed_decreasing_steering = 45
|
||||
max_speed_full_steering_castering = 20
|
||||
max_speed_decreasing_steering_castering = 35
|
||||
emergency_extension_type = 2
|
||||
hyd_need_power_to_function= 0
|
||||
min_castering_angle = 0.05236
|
||||
max_castering_angle = 3.142
|
||||
allow_stopped_steering = 1
|
||||
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
|
||||
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
|
||||
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
|
||||
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
|
||||
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
|
||||
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
|
||||
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
|
||||
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
|
||||
|
||||
[FUEL]
|
||||
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
|
||||
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
|
||||
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
|
||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
|
||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
|
||||
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
||||
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
|
||||
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
|
||||
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||
fuel_type = 2
|
||||
number_of_tank_selectors = 3
|
||||
electric_pump = 0
|
||||
engine_driven_pump = 1
|
||||
manual_transfer_pump = 0
|
||||
manual_pump = 0
|
||||
anemometer_pump = 0
|
||||
fuel_dump_rate = 0.02
|
||||
default_fuel_tank_selector.1 = 1
|
||||
default_fuel_tank_selector.2 = 1
|
||||
default_fuel_tank_selector.3 = 1
|
||||
|
||||
[AIRPLANE_GEOMETRY]
|
||||
wing_area = 3648
|
||||
wing_span = 170.5
|
||||
wing_root_chord = 34.68
|
||||
wing_camber = 1
|
||||
wing_thickness_ratio = 0.04
|
||||
wing_dihedral = 2.2
|
||||
wing_incidence = 1.5
|
||||
wing_twist = -0.5
|
||||
oswald_efficiency_factor = 0.72
|
||||
wing_winglets_flag = 1
|
||||
wing_sweep = 38
|
||||
wing_pos_apex_lon = 1
|
||||
wing_pos_apex_vert = -2.75
|
||||
htail_area = 920
|
||||
htail_span = 59.5
|
||||
htail_pos_lon = -88
|
||||
htail_pos_vert = 5.0
|
||||
htail_incidence = 0.8
|
||||
htail_sweep = 36.5
|
||||
htail_thickness_ratio = 0.02
|
||||
vtail_area = 760
|
||||
vtail_span = 28.1
|
||||
vtail_sweep = 43
|
||||
vtail_pos_lon = -79.5
|
||||
vtail_pos_vert = 28
|
||||
vtail_thickness_ratio = 0.03
|
||||
fuselage_length = 200.92
|
||||
fuselage_diameter = 19.75
|
||||
fuselage_center_pos = 10, 0, 1.0
|
||||
elevator_area = 327.0
|
||||
aileron_area = 225.0
|
||||
rudder_area = 190.0
|
||||
elevator_up_limit = 25
|
||||
elevator_down_limit = 15
|
||||
aileron_up_limit = 25
|
||||
aileron_down_limit = 15
|
||||
rudder_limit = 23
|
||||
rudder_trim_limit = 20
|
||||
elevator_trim_limit = 30
|
||||
spoiler_limit = 60
|
||||
spoilerons_available = 1
|
||||
aileron_to_spoileron_gain = 3
|
||||
min_ailerons_for_spoilerons = 10
|
||||
min_flaps_for_spoilerons = 0
|
||||
spoiler_extension_time = 2.0
|
||||
spoiler_handle_available = 1
|
||||
auto_spoiler_available = 1
|
||||
auto_spoiler_auto_retracts = 0
|
||||
auto_spoiler_min_speed = 72
|
||||
positive_g_limit_flaps_up = 5.0
|
||||
positive_g_limit_flaps_down = 4.0
|
||||
negative_g_limit_flaps_up = -4.0
|
||||
negative_g_limit_flaps_down = -3.0
|
||||
load_safety_factor = 1.5
|
||||
elevator_trim_neutral = -1
|
||||
aileron_to_rudder_scale = 0
|
||||
flap_to_aileron_scale = 0
|
||||
fly_by_wire = 0
|
||||
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
|
||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
|
||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
|
||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
|
||||
|
||||
[AERODYNAMICS]
|
||||
lift_coef_pitch_rate = -8.09375
|
||||
lift_coef_daoa = 2.68359
|
||||
lift_coef_delta_elevator = -0.28906
|
||||
lift_coef_horizontal_incidence = 0.91357
|
||||
lift_coef_flaps = 1
|
||||
lift_coef_spoilers = 0
|
||||
drag_coef_zero_lift = 0.02539
|
||||
drag_coef_flaps = 0.1339
|
||||
drag_coef_gear = 0.0549
|
||||
drag_coef_spoilers = 0.05207
|
||||
side_force_slip_angle = -0.77392
|
||||
side_force_roll_rate = 0.15478
|
||||
side_force_yaw_rate = 0
|
||||
side_force_delta_rudder = -0.14746
|
||||
pitch_moment_horizontal_incidence = 4.24755
|
||||
pitch_moment_delta_elevator = -2.37011
|
||||
pitch_moment_delta_trim = 0
|
||||
pitch_moment_pitch_damping = -214.1455
|
||||
pitch_moment_aoa_0 = 0.11621
|
||||
pitch_moment_daoa = 8.87255
|
||||
pitch_moment_flaps = 0.0105
|
||||
pitch_moment_gear = 0.0171
|
||||
pitch_moment_spoilers = 0
|
||||
pitch_moment_delta_elevator_propwash = -2.37011
|
||||
pitch_moment_pitch_propwash = -214.1455
|
||||
roll_moment_slip_angle = 0.26855
|
||||
roll_moment_roll_damping = -3.40869
|
||||
roll_moment_yaw_rate = -0.27197
|
||||
roll_moment_spoilers = 0.07
|
||||
roll_moment_delta_aileron = -0.34521
|
||||
roll_moment_delta_rudder = 0.01660
|
||||
roll_moment_delta_aileron_trim_scalar = -0.2
|
||||
yaw_moment_slip_angle = 0.18066
|
||||
yaw_moment_roll = 0.07470
|
||||
yaw_moment_yaw_damping = -2.49023
|
||||
yaw_moment_yaw_propwash = 0
|
||||
yaw_moment_delta_aileron = -0.00683
|
||||
yaw_moment_delta_rudder = 0.07128
|
||||
yaw_moment_delta_rudder_propwash = 0.075
|
||||
yaw_moment_delta_rudder_trim_scalar = -0.2
|
||||
compute_aero_center = 0
|
||||
aero_center_lift = -13.75
|
||||
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
|
||||
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
|
||||
lift_coef_mach_table = 0:1
|
||||
lift_coef_delta_elevator_mach_table = 0:0
|
||||
lift_coef_daoa_mach_table = 0:0
|
||||
lift_coef_pitch_rate_mach_table = 0:0
|
||||
lift_coef_horizontal_incidence_mach_table = 0:0
|
||||
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
|
||||
side_force_slip_angle_mach_table = 0:0
|
||||
side_force_delta_rudder_mach_table = 0:0
|
||||
side_force_yaw_rate_mach_table = 0:0
|
||||
side_force_roll_rate_mach_table = 0:0
|
||||
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
|
||||
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
|
||||
pitch_moment_horizontal_incidence_aoa_table = 0:1
|
||||
pitch_moment_daoa_aoa_table = 0:1
|
||||
pitch_moment_pitch_alpha_table = 0:1
|
||||
pitch_moment_delta_elevator_mach_table = 0:0
|
||||
pitch_moment_daoa_mach_table = 0:0
|
||||
pitch_moment_pitch_rate_mach_table = 0:0
|
||||
pitch_moment_horizontal_incidence_mach_table = 0:0
|
||||
pitch_moment_aoa_0_mach_table = 0:0
|
||||
roll_moment_aoa_table = 0:0
|
||||
roll_moment_slip_angle_aoa_table = 0:1
|
||||
roll_moment_roll_rate_aoa_table = 0:1
|
||||
roll_moment_delta_aileron_aoa_table = 0:1
|
||||
roll_moment_slip_angle_mach_table = 0:0
|
||||
roll_moment_delta_rudder_mach_table = 0:0
|
||||
roll_moment_delta_aileron_mach_table = 0:0
|
||||
roll_moment_yaw_rate_mach_table = 0:0
|
||||
roll_moment_roll_rate_mach_table = 0:0
|
||||
yaw_moment_aoa_table = 0:0
|
||||
yaw_moment_slip_angle_aoa_table = 0:1
|
||||
yaw_moment_yaw_rate_aoa_table = 0:1
|
||||
yaw_moment_delta_rudder_aoa_table = 0:1
|
||||
yaw_moment_slip_angle_mach_table = 0:0
|
||||
yaw_moment_delta_rudder_mach_table = 0:0
|
||||
yaw_moment_delta_aileron_mach_table = 0:0
|
||||
yaw_moment_yaw_rate_mach_table = 0:0
|
||||
yaw_moment_roll_rate_mach_table = 0:0
|
||||
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
|
||||
aileron_scaling_table = -0.785:1 ;0:1
|
||||
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
|
||||
elevator_lift_coef=3
|
||||
rudder_lift_coef=2
|
||||
aileron_load_factor_effectiveness_table = 0:1
|
||||
lift_coef_at_drag_zero = 0.1
|
||||
lift_coef_at_drag_zero_flaps = 0.1
|
||||
|
||||
[FLIGHT_TUNING]
|
||||
modern_fm_only = 1
|
||||
cruise_lift_scalar = 1
|
||||
parasite_drag_scalar = 1
|
||||
induced_drag_scalar = 1
|
||||
flap_induced_drag_scalar = 1
|
||||
elevator_effectiveness = 1.1
|
||||
elevator_maxangle_scalar = 1
|
||||
aileron_effectiveness = 1
|
||||
rudder_effectiveness = 1
|
||||
rudder_maxangle_scalar = 1
|
||||
pitch_stability = 5
|
||||
roll_stability = 1
|
||||
yaw_stability = 1
|
||||
pitch_gyro_stability = 1
|
||||
roll_gyro_stability = 1
|
||||
yaw_gyro_stability = 1
|
||||
empty_CG_deviation_limit=0
|
||||
elevator_trim_effectiveness = 1.5
|
||||
aileron_trim_effectiveness = 1
|
||||
rudder_trim_effectiveness = 1
|
||||
hi_alpha_on_roll = 0
|
||||
hi_alpha_on_yaw = 0
|
||||
p_factor_on_yaw = 0
|
||||
torque_on_roll = 0
|
||||
gyro_precession_on_roll = 0
|
||||
gyro_precession_on_yaw = 0
|
||||
engine_wash_on_roll = 0
|
||||
wingflex_scalar = 2
|
||||
wingflex_offset = 0
|
||||
stall_coef_at_min_weight = 0.71
|
||||
ground_crosswind_effect_zero_speed=10
|
||||
ground_crosswind_effect_max_speed=150
|
||||
ground_high_speed_steeringwheel_static_friction_scalar=1.5
|
||||
ground_high_speed_otherwheel_static_friction_scalar=1.2
|
||||
|
||||
[REFERENCE SPEEDS]
|
||||
full_flaps_stall_speed = 115
|
||||
flaps_up_stall_speed = 149
|
||||
cruise_speed = 345
|
||||
cruise_mach = 0.85
|
||||
crossover_speed = 330
|
||||
max_mach = 0.9
|
||||
max_indicated_speed = 395
|
||||
max_flaps_extended = 170
|
||||
normal_operating_speed = 325
|
||||
airspeed_indicator_max = 562.5
|
||||
rotation_speed_min = 145
|
||||
climb_speed = 250
|
||||
cruise_alt = 41000
|
||||
takeoff_speed = 165
|
||||
spawn_cruise_altitude = 5000
|
||||
spawn_descent_altitude = 500
|
||||
best_angle_climb_speed = 0
|
||||
approach_speed = 0
|
||||
best_glide = 0
|
||||
max_gear_extended = 200
|
||||
|
||||
[INTERACTIVE POINTS]
|
||||
number_of_interactive_points = 8
|
||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
|
||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
|
||||
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
|
||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
|
||||
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
||||
|
||||
[STALL PROTECTION]
|
||||
stall_protection = 1 ; Alpha Protection
|
||||
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
|
||||
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
|
||||
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
|
||||
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
|
||||
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
|
||||
|
||||
;===================== FLAPS =====================
|
||||
|
||||
[FLAPS.0]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.25
|
||||
extending-time = 22
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.1]
|
||||
type = 1
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 23
|
||||
damaging-speed = 280
|
||||
blowout-speed = 310
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.1
|
||||
drag_scalar = 1.1
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 7
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 0, -1, 0
|
||||
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
||||
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||
flaps-position.6 = 35, 160, 0.32, 1
|
||||
flaps-position.7 = 50, 155, 0.43, 1
|
||||
|
||||
[FLAPS.2]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.2
|
||||
extending-time = 8
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
|
||||
[FLAPS.3]
|
||||
type = 2
|
||||
system_type = 1
|
||||
span-outboard = 0.7
|
||||
extending-time = 21
|
||||
damaging-speed = 300
|
||||
blowout-speed = 330
|
||||
maneuvering_flaps = 0
|
||||
lift_scalar = 0.5
|
||||
drag_scalar = 0.75
|
||||
pitch_scalar = 1
|
||||
max_on_ground_position = 1
|
||||
flaps-position.0 = 0, -1, 0
|
||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||
Vendored
+7
@@ -1 +1,8 @@
|
||||
/// <reference types="@microsoft/msfs-types/js/common.d.ts" />
|
||||
/// <reference types="@microsoft/msfs-types/pages/vcockpit/instruments/shared/baseinstrument.d.ts" />
|
||||
/// <reference types="@microsoft/msfs-types/js/datastorage.d.ts" />
|
||||
/// <reference types="@microsoft/msfs-types/js/buttons.d.ts" />
|
||||
/// <reference types="@microsoft/msfs-types/js/services/toolbarpanels.d.ts" />
|
||||
/// <reference types="@microsoft/msfs-types/js/simvar.d.ts" />
|
||||
|
||||
function useSelector(selector: (state: any) => any): any;
|
||||
@@ -1,6 +1,6 @@
|
||||
{
|
||||
"name": "tfdidesign-md11-load-manager",
|
||||
"version": "0.1.0",
|
||||
"name": "js-bundle",
|
||||
"version": "0.2.34",
|
||||
"description": "",
|
||||
"main": "index.js",
|
||||
"type": "module",
|
||||
@@ -10,10 +10,11 @@
|
||||
"licenses": "license-report --output=markdown > ./src/assets/licenses_node.md",
|
||||
"debugger": "cd \"%MSFS_SDK%\\Tools\\CoherentGT Debugger\" && Debugger.exe",
|
||||
"locale": "cd \"%MSFS_SDK%\\Tools\\MSFS_Localization\" && MSFSLocalizationManager.exe",
|
||||
"clean": "rimraf ..\\html_ui\\Pages\\VCockpit\\Instruments\\aircraft_efb\\KH_TFDi_MD11_efb",
|
||||
"dev": "npx rollup -c -w",
|
||||
"clean": "rimraf ../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel/ && rimraf .rollup.cache",
|
||||
"build": "npm version patch && npx rollup -c",
|
||||
"release": "pnpm types && pnpm lint && pnpm run licenses && pnpm clean && npm version patch && cross-env NODE_ENV=production npx rollup -c"
|
||||
"build": "npm version patch && npx rollup -c && pnpm efb",
|
||||
"release": "pnpm types && pnpm lint && pnpm run licenses && pnpm clean && npm version patch && cross-env NODE_ENV=production npx rollup -c && pnpm efb ",
|
||||
"efb": "cd ..\\.. && node insert-efb && rm PackageSources\\html_ui\\Pages\\VCockpit\\Instruments\\aircraft_efb\\KH_TFDi_MD11_efb/vendor*"
|
||||
},
|
||||
"engines": {
|
||||
"node": ">=22"
|
||||
@@ -23,48 +24,45 @@
|
||||
"license": "ISC",
|
||||
"devDependencies": {
|
||||
"@microsoft/msfs-types": "^1.14.6",
|
||||
"@rollup/plugin-commonjs": "^25.0.0",
|
||||
"@rollup/plugin-json": "^6.0.0",
|
||||
"@rollup/plugin-node-resolve": "^15.1.0",
|
||||
"@rollup/plugin-commonjs": "^28.0.3",
|
||||
"@rollup/plugin-json": "^6.1.0",
|
||||
"@rollup/plugin-node-resolve": "^16.0.1",
|
||||
"@rollup/plugin-replace": "^6.0.2",
|
||||
"@rollup/plugin-terser": "^0.4.3",
|
||||
"@rollup/plugin-typescript": "^11.1.1",
|
||||
"@types/react": "^18.2.8",
|
||||
"@types/react-dom": "^18.2.4",
|
||||
"@types/uuid": "^9.0.7",
|
||||
"@typescript-eslint/eslint-plugin": "^6.10.0",
|
||||
"@typescript-eslint/parser": "^6.10.0",
|
||||
"autoprefixer": "^10.4.14",
|
||||
"@rollup/plugin-terser": "^0.4.4",
|
||||
"@rollup/plugin-typescript": "^12.1.2",
|
||||
"@types/node": "^24.3.1",
|
||||
"@types/react": "^19.1.6",
|
||||
"@types/react-dom": "^19.1.6",
|
||||
"@types/uuid": "^10.0.0",
|
||||
"@typescript-eslint/eslint-plugin": "^6.21.0",
|
||||
"@typescript-eslint/parser": "^6.21.0",
|
||||
"autoprefixer": "^10.4.21",
|
||||
"cross-env": "^7.0.3",
|
||||
"eslint": "^8.42.0",
|
||||
"eslint-plugin-import": "^2.27.5",
|
||||
"eslint-plugin-react": "^7.32.2",
|
||||
"eslint-plugin-react-hooks": "^4.6.0",
|
||||
"license-report": "^6.5.0",
|
||||
"postcss": "^8.4.24",
|
||||
"prettier": "^3.0.3",
|
||||
"prettier-plugin-organize-imports": "^3.2.4",
|
||||
"rimraf": "^5.0.1",
|
||||
"rollup": "^4.3.1",
|
||||
"rollup-plugin-copy": "^3.4.0",
|
||||
"eslint": "^8.57.1",
|
||||
"eslint-plugin-import": "^2.31.0",
|
||||
"eslint-plugin-react": "^7.37.5",
|
||||
"eslint-plugin-react-hooks": "^4.6.2",
|
||||
"license-report": "^6.7.2",
|
||||
"postcss": "^8.5.4",
|
||||
"postcss-import": "^16.1.0",
|
||||
"prettier": "^3.5.3",
|
||||
"prettier-plugin-organize-imports": "^4.1.0",
|
||||
"rimraf": "^6.0.1",
|
||||
"rollup": "^4.42.0",
|
||||
"rollup-plugin-copy": "^3.5.0",
|
||||
"rollup-plugin-postcss": "^4.0.2",
|
||||
"rollup-plugin-react-svg": "^3.0.3",
|
||||
"rollup-plugin-version-injector": "^1.3.3",
|
||||
"sass": "^1.89.1",
|
||||
"svg-slim": "^2.0.5",
|
||||
"tslib": "^2.5.3",
|
||||
"typed-scss-modules": "^7.1.0",
|
||||
"typescript": "5.2.2"
|
||||
"tslib": "^2.8.1",
|
||||
"typed-scss-modules": "^8.1.1",
|
||||
"typescript": "5.8.3"
|
||||
},
|
||||
"dependencies": {
|
||||
"@emotion/react": "^11.11.1",
|
||||
"@emotion/styled": "^11.11.0",
|
||||
"@mui/icons-material": "^5.14.16",
|
||||
"@mui/material": "^5.14.17",
|
||||
"postcss-import": "^15.1.0",
|
||||
"react": "^18.2.0",
|
||||
"react-dom": "^18.2.0",
|
||||
"uuid": "^9.0.1"
|
||||
"lucide-react": "^0.555.0",
|
||||
"react": "^19.1.0",
|
||||
"react-dom": "^19.1.0",
|
||||
"uuid": "^11.1.0"
|
||||
},
|
||||
"packageManager": "pnpm@10.11.1+sha512.e519b9f7639869dc8d5c3c5dfef73b3f091094b0a006d7317353c72b124e80e1afd429732e28705ad6bfa1ee879c1fce46c128ccebd3192101f43dd67c667912"
|
||||
}
|
||||
|
||||
Generated
+567
-1296
File diff suppressed because it is too large
Load Diff
@@ -2,7 +2,6 @@ import commonjs from '@rollup/plugin-commonjs';
|
||||
import json from '@rollup/plugin-json';
|
||||
import resolve from '@rollup/plugin-node-resolve';
|
||||
import replace from '@rollup/plugin-replace';
|
||||
import terser from '@rollup/plugin-terser';
|
||||
import typescript from '@rollup/plugin-typescript';
|
||||
import autoprefixer from 'autoprefixer';
|
||||
import atImport from 'postcss-import';
|
||||
@@ -10,29 +9,29 @@ import copy from 'rollup-plugin-copy';
|
||||
import postcss from 'rollup-plugin-postcss';
|
||||
import reactSvg from 'rollup-plugin-react-svg';
|
||||
import versionInjector from 'rollup-plugin-version-injector';
|
||||
import svgs from 'svg-slim';
|
||||
|
||||
const { NODE_ENV: targetEnv = 'development' } = process.env;
|
||||
const outDirBase = '../html_ui';
|
||||
const panelDirBase = `${outDirBase}/InGamePanels/tfdidesign-md11-load-manager-panel`;
|
||||
|
||||
function svgSlim(code, id) {
|
||||
if (!id.endsWith('.svg')) return code;
|
||||
return svgs(code.toString(), {}).then((res) => res);
|
||||
}
|
||||
const panelDirBase = `${outDirBase}/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb`;
|
||||
|
||||
export default {
|
||||
input: 'src/index.ts',
|
||||
input: 'src/App.tsx',
|
||||
output: {
|
||||
dir: panelDirBase,
|
||||
format: 'es',
|
||||
sourcemap: targetEnv !== 'production',
|
||||
manualChunks: (id) => {
|
||||
if (id.includes('node_modules')) {
|
||||
return 'vendor';
|
||||
}
|
||||
|
||||
return null;
|
||||
},
|
||||
},
|
||||
plugins: [
|
||||
replace({
|
||||
'process.env.NODE_ENV': JSON.stringify(targetEnv),
|
||||
'import.meta.env': true,
|
||||
'import.meta.env.MODE': JSON.stringify(targetEnv),
|
||||
'process.env.NODE_ENV': targetEnv,
|
||||
preventAssignment: true,
|
||||
}),
|
||||
versionInjector(),
|
||||
postcss({
|
||||
@@ -45,22 +44,15 @@ export default {
|
||||
reactSvg(),
|
||||
resolve(),
|
||||
json(),
|
||||
typescript(),
|
||||
typescript({
|
||||
outputToFilesystem: false,
|
||||
}),
|
||||
commonjs({
|
||||
requireReturnsDefault: 'auto',
|
||||
}),
|
||||
targetEnv === 'production' && terser(),
|
||||
// targetEnv === 'production' && terser(), // Disabled due to script running afterwards
|
||||
copy({
|
||||
targets: [
|
||||
{ src: ['src/assets/*', '!**/*.svg'], dest: `${panelDirBase}/assets` },
|
||||
{ src: 'src/assets/img/*', dest: `${panelDirBase}/assets/img`, transform: svgSlim },
|
||||
{ src: ['src/index.html'], dest: `${panelDirBase}` },
|
||||
{
|
||||
src: ['src/assets/ICON_TFDIDESIGN_MD11_LOAD_MANAGER.svg'],
|
||||
dest: [`${outDirBase}/icons/toolbar`, `${outDirBase}/Textures/Menu/toolbar`],
|
||||
transform: svgSlim,
|
||||
},
|
||||
],
|
||||
targets: [{ src: ['src/assets/*', '!**/*.svg'], dest: `${panelDirBase}/assets` }],
|
||||
}),
|
||||
],
|
||||
onwarn: function (warning, warn) {
|
||||
|
||||
@@ -1,9 +0,0 @@
|
||||
@import 'fonts/300.css';
|
||||
@import 'fonts/400.css';
|
||||
@import 'fonts/500.css';
|
||||
@import 'fonts/700.css';
|
||||
|
||||
.app {
|
||||
width: 100%;
|
||||
height: 100%;
|
||||
}
|
||||
@@ -1,141 +1,59 @@
|
||||
import ThemeProvider from '@mui/material/styles/ThemeProvider';
|
||||
import { FC, StrictMode } from 'react';
|
||||
import styles from './App.module.scss';
|
||||
import Freight from './components/freight/Freight';
|
||||
import { FC, useCallback, useEffect, useState } from 'react';
|
||||
import Freighter from './components/freighter/Freighter';
|
||||
import Pax from './components/pax/Pax';
|
||||
import { ArmsFreight, PayloadFreight } from './configs/freighter';
|
||||
import { ArmsPax, PayloadPax } from './configs/pax';
|
||||
import { ArmsFuel, EmptyArm, Fuel, toPercentMAC } from './configs/shared';
|
||||
import { COHERENT_COMM_BUS_WASM_CALL } from './constants';
|
||||
import { WASMDataF, WASMDataPax } from './types/WASMData';
|
||||
import { CommBusCall, CommBusEvent } from './types/general';
|
||||
|
||||
interface IAppProps {
|
||||
dataListener: ViewListener.ViewListener;
|
||||
}
|
||||
|
||||
const App: FC<IAppProps> = () => {
|
||||
// TODO: Get from EFB settings
|
||||
const [unit, setUnit] = useState<'lbs' | 'kg'>('lbs');
|
||||
// TODO: Look into EFB, infer the same way
|
||||
const [aircraft, setAircraft] = useState<'f' | 'pax'>('f');
|
||||
const [payload, setPayload] = useState<PayloadPax | PayloadFreight>();
|
||||
const [fuel, setFuel] = useState<Fuel>();
|
||||
|
||||
const [ZFWCG, setZFWCG] = useState(0);
|
||||
const [TOCG, setTOCG] = useState(0);
|
||||
|
||||
const requestRef = useRef<number | undefined>(undefined);
|
||||
|
||||
const mainLoop = () => {
|
||||
try {
|
||||
if (SimVar.IsReady()) {
|
||||
const conversion = SimVar.GetSimVarValue('FUEL WEIGHT PER GALLON', unit);
|
||||
const emptyWeight = SimVar.GetSimVarValue('EMPTY WEIGHT', unit);
|
||||
|
||||
const payload: PayloadPax | PayloadFreight = {
|
||||
pilot: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:1', unit),
|
||||
firstOfficer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:2', unit),
|
||||
engineer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:3', unit),
|
||||
upper1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:4', unit),
|
||||
cabinCrewFront: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:4', unit),
|
||||
upper1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:5', unit),
|
||||
business1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:5', unit),
|
||||
upper2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:6', unit),
|
||||
business1Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:6', unit),
|
||||
upper2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:7', unit),
|
||||
business1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:7', unit),
|
||||
upper3Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:8', unit),
|
||||
business2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:8', unit),
|
||||
upper3Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:9', unit),
|
||||
business2Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:9', unit),
|
||||
upper4Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:10', unit),
|
||||
business2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:10', unit),
|
||||
upper4Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:11', unit),
|
||||
economy1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:11', unit),
|
||||
lowerForward: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:12', unit),
|
||||
economy1Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:12', unit),
|
||||
lowerRear: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:13', unit),
|
||||
economy1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:13', unit),
|
||||
leftAuxF: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:14', unit),
|
||||
economy2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:14', unit),
|
||||
rightAuxF: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:15', unit),
|
||||
economy2Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:15', unit),
|
||||
economy2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:16', unit),
|
||||
cabinCrewRear: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:17', unit),
|
||||
forwardCargo: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:18', unit),
|
||||
rearCargo: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:19', unit),
|
||||
leftAuxPax: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:20', unit),
|
||||
rightAuxPax: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:21', unit),
|
||||
};
|
||||
|
||||
const fuel = {
|
||||
main1: SimVar.GetSimVarValue('FUEL TANK LEFT MAIN QUANTITY', 'gal') * conversion,
|
||||
main3: SimVar.GetSimVarValue('FUEL TANK RIGHT MAIN QUANTITY', 'gal') * conversion,
|
||||
main2: SimVar.GetSimVarValue('FUEL TANK CENTER QUANTITY', 'gal') * conversion,
|
||||
upperAux: SimVar.GetSimVarValue('FUEL TANK CENTER2 QUANTITY', 'gal') * conversion,
|
||||
lowerAux: SimVar.GetSimVarValue('FUEL TANK CENTER3 QUANTITY', 'gal') * conversion,
|
||||
main1Tip: SimVar.GetSimVarValue('FUEL TANK LEFT TIP QUANTITY', 'gal') * conversion,
|
||||
main3Tip: SimVar.GetSimVarValue('FUEL TANK RIGHT TIP QUANTITY', 'gal') * conversion,
|
||||
tail: SimVar.GetSimVarValue('FUEL TANK EXTERNAL1 QUANTITY', 'gal') * conversion,
|
||||
forwardAux1: SimVar.GetSimVarValue('FUEL TANK LEFT AUX QUANTITY', 'gal') * conversion,
|
||||
forwardAux2: SimVar.GetSimVarValue('FUEL TANK RIGHT AUX QUANTITY', 'gal') * conversion,
|
||||
};
|
||||
|
||||
let totalMoment = EmptyArm * emptyWeight;
|
||||
let totalWeight = emptyWeight;
|
||||
const arms = aircraft === 'f' ? ArmsFreight : ArmsPax;
|
||||
for (const key in arms) {
|
||||
if (Object.prototype.hasOwnProperty.call(payload, key)) {
|
||||
const stationWeight = payload[key as keyof (PayloadFreight | PayloadPax)];
|
||||
const arm = arms[key as keyof typeof arms];
|
||||
|
||||
totalWeight += stationWeight;
|
||||
totalMoment += arm * stationWeight;
|
||||
}
|
||||
}
|
||||
setZFWCG(toPercentMAC(totalMoment / totalWeight));
|
||||
|
||||
for (const key in ArmsFuel) {
|
||||
if (Object.prototype.hasOwnProperty.call(fuel, key)) {
|
||||
const stationWeight = fuel[key as keyof Fuel];
|
||||
const arm = ArmsFuel[key as keyof typeof ArmsFuel];
|
||||
|
||||
totalWeight += stationWeight;
|
||||
totalMoment += arm * stationWeight;
|
||||
}
|
||||
}
|
||||
setTOCG(toPercentMAC(totalMoment / totalWeight));
|
||||
|
||||
setPayload(payload);
|
||||
setFuel(fuel);
|
||||
}
|
||||
} catch {}
|
||||
|
||||
requestRef.current = requestAnimationFrame(mainLoop);
|
||||
};
|
||||
const App: FC = () => {
|
||||
const [SBUsername, setSBUsername] = useState<string>();
|
||||
const [WASMData, setWASMData] = useState<WASMDataPax | WASMDataF>();
|
||||
|
||||
// CommBus
|
||||
const usernameCallback = useCallback((username: string) => {
|
||||
setSBUsername(username);
|
||||
}, []);
|
||||
const wasmCallback = useCallback((data: string) => {
|
||||
setWASMData(JSON.parse(data));
|
||||
}, []);
|
||||
useEffect(() => {
|
||||
requestRef.current = requestAnimationFrame(mainLoop);
|
||||
console.log(
|
||||
'[KHOFMANN TFDi MD-11 Load Manager] JS Version [VI]{version}[/VI]: process.env.NODE_ENV [VI]{date}[/VI]'
|
||||
);
|
||||
|
||||
if (requestRef.current !== undefined) return () => cancelAnimationFrame(requestRef.current as number);
|
||||
}, [unit, aircraft]);
|
||||
console.log('[KHOFMANN TFDi MD-11 Load Manager] Initialising CommBus');
|
||||
|
||||
//DEBUG
|
||||
useEffect(() => {
|
||||
console.log('Payload', payload);
|
||||
console.log('Fuel', fuel);
|
||||
console.log('ZFWCG', ZFWCG);
|
||||
console.log('TOCG', TOCG);
|
||||
}, [ZFWCG, TOCG]);
|
||||
const commBus = RegisterViewListener('JS_LISTENER_COMM_BUS');
|
||||
|
||||
commBus.on(CommBusEvent.TFDI_SIMBRIEF_USERNAME, usernameCallback);
|
||||
commBus.on(CommBusEvent.LIVE_DATA, wasmCallback);
|
||||
|
||||
Coherent.call(COHERENT_COMM_BUS_WASM_CALL, CommBusCall.TFDI_SIMBRIEF_USERNAME, 'null');
|
||||
|
||||
return () => {
|
||||
console.log('[KHOFMANN TFDi MD-11 Load Manager] De-Initialising CommBus');
|
||||
|
||||
commBus.off(CommBusEvent.TFDI_SIMBRIEF_USERNAME, usernameCallback);
|
||||
commBus.off(CommBusEvent.LIVE_DATA, wasmCallback);
|
||||
|
||||
commBus.unregister();
|
||||
};
|
||||
}, []);
|
||||
|
||||
return (
|
||||
<StrictMode>
|
||||
<div className={styles.app}>
|
||||
<button onClick={() => (unit === 'lbs' ? setUnit('kg') : setUnit('lbs'))}>Change unit from {unit}</button>
|
||||
<button onClick={() => (aircraft === 'f' ? setAircraft('pax') : setAircraft('f'))}>
|
||||
Change aircraft from {aircraft}
|
||||
</button>
|
||||
{aircraft === 'f' ? <Freight /> : <Pax unit={unit} payload={payload as PayloadPax} />}
|
||||
<div className="flex w-full justify-center py-5 bg-zinc-900">
|
||||
<div className="flex w-3/4 flex-col items-center">
|
||||
{WASMData ? (
|
||||
WASMData.userData.isCargo ? (
|
||||
<Freighter WASMData={WASMData as WASMDataF} username={SBUsername} />
|
||||
) : (
|
||||
<Pax WASMData={WASMData as WASMDataPax} username={SBUsername} />
|
||||
)
|
||||
) : (
|
||||
<h1 className="text-sm font-medium">LOADING</h1>
|
||||
)}
|
||||
</div>
|
||||
</StrictMode>
|
||||
</div>
|
||||
);
|
||||
};
|
||||
|
||||
|
||||
@@ -1,10 +0,0 @@
|
||||
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 54 35">
|
||||
<path
|
||||
d="M17.08737 32.03408c-6.24 0-11.298-5.216-11.298-11.651 0-6.434 5.058-11.651 11.298-11.651s11.298 5.217 11.298 11.651c0 .679-.059 1.343-.167 1.989l1.052.29c.13-.741.202-1.502.202-2.281 0-7.082-5.579-12.823-12.46-12.823-6.881 0-12.46 5.741-12.46 12.823 0 7.081 5.579 12.822 12.46 12.822 4.524 0 8.485-2.482 10.668-6.196h-1.301c-2.039 3.037-5.439 5.027-9.292 5.027" />
|
||||
<path
|
||||
d="M43.10237.39308s-1.764 2.479-3.978 5.076c-2.212 2.595-4.01 4.393-4.01 4.393l-.166-.716-.766-.116s2.147-2.33 4.343-4.56c2.197-2.23 4.577-4.077 4.577-4.077" />
|
||||
<path
|
||||
d="M34.63157 9.42938s-.316 1.082-.732 1.547c-.416.466-.949.649-1.431 1.065-.483.417-1.964 2.031-1.964 2.031s-5.525 5.974-9.186 9.302c-3.661 3.329-8.058 7.009-11.183 8.837-3.129 1.831-5.675 2.912-7.805 2.147-2.13-.766-2.32-2.96-1.864-4.693.416-1.581 1.598-2.646 1.598-2.646s-1.698 1.88-1.664 3.977c.014.899.299 1.664.732 2.23.251.328 1.794 1.632 4.476.766 1.598-.516 4.015-1.526 6.84-3.695 5.875-4.51 7.805-6.174 13.696-12.131 3.277-3.314 5.375-5.642 5.375-5.642s.483-.432.665-.798c.184-.367.367-1.049.883-1.448s1.564-.849 1.564-.849" />
|
||||
<path
|
||||
d="M17.89017 18.03288h1.023s3.096 2.696 6.915 3.994 6.989 1.997 13.28 2.296c6.29.3 10.958.375 12.431.575 1.473.199 2.197.499 2.197.499s-13.056.424-17.224.599c-4.169.174-11.857.823-11.857.823l-.625-.299 5.592-1.598-6.964-.075z" />
|
||||
</svg>
|
||||
|
Before Width: | Height: | Size: 1.4 KiB |
@@ -1,202 +0,0 @@
|
||||
|
||||
Apache License
|
||||
Version 2.0, January 2004
|
||||
http://www.apache.org/licenses/
|
||||
|
||||
TERMS AND CONDITIONS FOR USE, REPRODUCTION, AND DISTRIBUTION
|
||||
|
||||
1. Definitions.
|
||||
|
||||
"License" shall mean the terms and conditions for use, reproduction,
|
||||
and distribution as defined by Sections 1 through 9 of this document.
|
||||
|
||||
"Licensor" shall mean the copyright owner or entity authorized by
|
||||
the copyright owner that is granting the License.
|
||||
|
||||
"Legal Entity" shall mean the union of the acting entity and all
|
||||
other entities that control, are controlled by, or are under common
|
||||
control with that entity. For the purposes of this definition,
|
||||
"control" means (i) the power, direct or indirect, to cause the
|
||||
direction or management of such entity, whether by contract or
|
||||
otherwise, or (ii) ownership of fifty percent (50%) or more of the
|
||||
outstanding shares, or (iii) beneficial ownership of such entity.
|
||||
|
||||
"You" (or "Your") shall mean an individual or Legal Entity
|
||||
exercising permissions granted by this License.
|
||||
|
||||
"Source" form shall mean the preferred form for making modifications,
|
||||
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|
||||
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|
||||
|
||||
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|
||||
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|
||||
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|
||||
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|
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|
||||
"Work" shall mean the work of authorship, whether in Source or
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|
||||
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|
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|
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|
||||
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|
||||
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|
||||
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Binary file not shown.
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@@ -1,44 +1,41 @@
|
||||
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
|
||||
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :----------- | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
|
||||
| kessler | stuff | @emotion/react | perpetual | material | MIT | git+https://github.com/emotion-js/emotion.git#main | 11.14.0 | 11.14.0 | ^11.11.1 | Emotion Contributors |
|
||||
| kessler | stuff | @emotion/styled | perpetual | material | MIT | git+https://github.com/emotion-js/emotion.git#main | 11.14.0 | 11.14.0 | ^11.11.0 | n/a |
|
||||
| kessler | stuff | @mui/icons-material | perpetual | material | MIT | git+https://github.com/mui/material-ui.git | 5.17.1 | 5.17.1 | ^5.14.16 | MUI Team |
|
||||
| kessler | stuff | @mui/material | perpetual | material | MIT | git+https://github.com/mui/material-ui.git | 5.17.1 | 5.17.1 | ^5.14.17 | MUI Team |
|
||||
| kessler | stuff | postcss-import | perpetual | material | MIT | git+https://github.com/postcss/postcss-import.git | 15.1.0 | 15.1.0 | ^15.1.0 | Maxime Thirouin |
|
||||
| kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 18.3.1 | 18.3.1 | ^18.2.0 | n/a |
|
||||
| kessler | stuff | react-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 18.3.1 | 18.3.1 | ^18.2.0 | n/a |
|
||||
| kessler | stuff | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 9.0.1 | 9.0.1 | ^9.0.1 | n/a |
|
||||
| kessler | stuff | @microsoft/msfs-types | perpetual | material | MIT | git+https://github.com/microsoft/msfs-avionics-mirror.git | 1.14.6 | 1.14.6 | ^1.14.6 | Asobo Studio / Working Title Simulations |
|
||||
| kessler | stuff | @rollup/plugin-commonjs | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 25.0.8 | 25.0.8 | ^25.0.0 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-json | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.1.0 | 6.1.0 | ^6.0.0 | rollup |
|
||||
| kessler | stuff | @rollup/plugin-node-resolve | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 15.3.1 | 15.3.1 | ^15.1.0 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-replace | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.0.2 | 6.0.2 | ^6.0.2 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-terser | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 0.4.4 | 0.4.4 | ^0.4.3 | Peter Placzek <peter.placzek1996@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 11.1.6 | 11.1.6 | ^11.1.1 | Oskar Segersvärd |
|
||||
| kessler | stuff | @types/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 18.3.23 | 18.3.23 | ^18.2.8 | n/a |
|
||||
| kessler | stuff | @types/react-dom | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 18.3.7 | 18.3.7 | ^18.2.4 | n/a |
|
||||
| kessler | stuff | @types/uuid | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 9.0.8 | 9.0.8 | ^9.0.7 | n/a |
|
||||
| kessler | stuff | @typescript-eslint/eslint-plugin | perpetual | material | MIT | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.10.0 | n/a |
|
||||
| kessler | stuff | @typescript-eslint/parser | perpetual | material | BSD-2-Clause | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.10.0 | n/a |
|
||||
| kessler | stuff | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.21 | 10.4.21 | ^10.4.14 | Andrey Sitnik <andrey@sitnik.ru> |
|
||||
| kessler | stuff | cross-env | perpetual | material | MIT | git+https://github.com/kentcdodds/cross-env.git | 7.0.3 | 7.0.3 | ^7.0.3 | Kent C. Dodds <me@kentcdodds.com> (https://kentcdodds.com) |
|
||||
| kessler | stuff | eslint | perpetual | material | MIT | git+https://github.com/eslint/eslint.git | 8.57.1 | 8.57.1 | ^8.42.0 | Nicholas C. Zakas <nicholas+npm@nczconsulting.com> |
|
||||
| kessler | stuff | eslint-plugin-import | perpetual | material | MIT | git+https://github.com/import-js/eslint-plugin-import.git | 2.31.0 | 2.31.0 | ^2.27.5 | Ben Mosher <me@benmosher.com> |
|
||||
| kessler | stuff | eslint-plugin-react | perpetual | material | MIT | git+https://github.com/jsx-eslint/eslint-plugin-react.git | 7.37.5 | 7.37.5 | ^7.32.2 | Yannick Croissant <yannick.croissant+npm@gmail.com> |
|
||||
| kessler | stuff | eslint-plugin-react-hooks | perpetual | material | MIT | git+https://github.com/facebook/react.git | 4.6.2 | 4.6.2 | ^4.6.0 | n/a |
|
||||
| kessler | stuff | license-report | perpetual | material | MIT | git+https://github.com/kessler/license-report.git | 6.7.2 | 6.7.2 | ^6.5.0 | Yaniv Kessler |
|
||||
| kessler | stuff | postcss | perpetual | material | MIT | git+https://github.com/postcss/postcss.git | 8.5.4 | 8.5.4 | ^8.4.24 | Andrey Sitnik <andrey@sitnik.ru> |
|
||||
| kessler | stuff | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.5.3 | 3.5.3 | ^3.0.3 | James Long |
|
||||
| kessler | stuff | prettier-plugin-organize-imports | perpetual | material | MIT | git+https://github.com/simonhaenisch/prettier-plugin-organize-imports.git | 3.2.4 | 3.2.4 | ^3.2.4 | Simon Haenisch (https://github.com/simonhaenisch) |
|
||||
| kessler | stuff | rimraf | perpetual | material | ISC | git://github.com/isaacs/rimraf.git | 5.0.10 | 5.0.10 | ^5.0.1 | Isaac Z. Schlueter <i@izs.me> (http://blog.izs.me/) |
|
||||
| kessler | stuff | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.41.1 | 4.41.1 | ^4.3.1 | Rich Harris |
|
||||
| kessler | stuff | rollup-plugin-copy | perpetual | material | MIT | git+https://github.com/vladshcherbin/rollup-plugin-copy.git | 3.5.0 | 3.5.0 | ^3.4.0 | Vlad Shcherbin <vlad.shcherbin@gmail.com> |
|
||||
| kessler | stuff | rollup-plugin-postcss | perpetual | material | MIT | git+https://github.com/egoist/rollup-plugin-postcss.git | 4.0.2 | 4.0.2 | ^4.0.2 | EGOIST <0x142857@gmail.com> |
|
||||
| kessler | stuff | rollup-plugin-react-svg | perpetual | material | MIT | git+https://github.com/boopathi/react-svg-loader.git | 3.0.3 | 3.0.3 | ^3.0.3 | boopathi |
|
||||
| kessler | stuff | rollup-plugin-version-injector | perpetual | material | ISC | git+https://github.com/djhouseknecht/rollup-plugin-version-injector.git | 1.3.3 | 1.3.3 | ^1.3.3 | David Houseknecht <david.j.houseknecht@gmail.com> |
|
||||
| kessler | stuff | sass | perpetual | material | MIT | git+https://github.com/sass/dart-sass.git | 1.89.1 | 1.89.1 | ^1.89.1 | Natalie Weizenbaum nweiz@google.com https://github.com/nex3 |
|
||||
| kessler | stuff | svg-slim | perpetual | material | MIT | git+https://github.com/benboba/svg-slim.git | 2.0.5 | 2.0.5 | ^2.0.5 | Wang Feng <benboba@gmail.com> |
|
||||
| kessler | stuff | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.5.3 | Microsoft Corp. |
|
||||
| kessler | stuff | typed-scss-modules | perpetual | material | MIT | git+https://github.com/skovy/typed-scss-modules.git | 7.1.4 | 7.1.4 | ^7.1.0 | Spencer Miskoviak <smiskoviak@gmail.com> |
|
||||
| kessler | stuff | typescript | perpetual | material | Apache-2.0 | git+https://github.com/Microsoft/TypeScript.git | 5.2.2 | 5.2.2 | 5.2.2 | Microsoft Corp. |
|
||||
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
|
||||
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :------------ | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
|
||||
| kessler | stuff | lucide-react | perpetual | material | ISC | git+https://github.com/lucide-icons/lucide.git | 0.555.0 | 0.555.0 | ^0.555.0 | Eric Fennis |
|
||||
| kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.4 | 19.2.4 | ^19.1.0 | n/a |
|
||||
| kessler | stuff | react-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.4 | 19.2.4 | ^19.1.0 | n/a |
|
||||
| kessler | stuff | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 11.1.0 | 11.1.0 | ^11.1.0 | n/a |
|
||||
| kessler | stuff | @microsoft/msfs-types | perpetual | material | MIT | git+https://github.com/microsoft/msfs-avionics-mirror.git | 1.14.6 | 1.14.6 | ^1.14.6 | Asobo Studio / Working Title Simulations |
|
||||
| kessler | stuff | @rollup/plugin-commonjs | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 28.0.9 | 28.0.9 | ^28.0.3 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-json | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.1.0 | 6.1.0 | ^6.1.0 | rollup |
|
||||
| kessler | stuff | @rollup/plugin-node-resolve | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 16.0.3 | 16.0.3 | ^16.0.1 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-replace | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.0.3 | 6.0.3 | ^6.0.2 | Rich Harris <richard.a.harris@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-terser | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 0.4.4 | 0.4.4 | ^0.4.4 | Peter Placzek <peter.placzek1996@gmail.com> |
|
||||
| kessler | stuff | @rollup/plugin-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 12.3.0 | 12.3.0 | ^12.1.2 | Oskar Segersvärd |
|
||||
| kessler | stuff | @types/node | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 24.12.2 | 24.12.0 | ^24.3.1 | n/a |
|
||||
| kessler | stuff | @types/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.14 | 19.2.14 | ^19.1.6 | n/a |
|
||||
| kessler | stuff | @types/react-dom | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.3 | 19.2.3 | ^19.1.6 | n/a |
|
||||
| kessler | stuff | @types/uuid | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 10.0.0 | 10.0.0 | ^10.0.0 | n/a |
|
||||
| kessler | stuff | @typescript-eslint/eslint-plugin | perpetual | material | MIT | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.21.0 | n/a |
|
||||
| kessler | stuff | @typescript-eslint/parser | perpetual | material | BSD-2-Clause | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.21.0 | n/a |
|
||||
| kessler | stuff | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.27 | 10.4.27 | ^10.4.21 | Andrey Sitnik <andrey@sitnik.ru> |
|
||||
| kessler | stuff | cross-env | perpetual | material | MIT | git+https://github.com/kentcdodds/cross-env.git | 7.0.3 | 7.0.3 | ^7.0.3 | Kent C. Dodds <me@kentcdodds.com> (https://kentcdodds.com) |
|
||||
| kessler | stuff | eslint | perpetual | material | MIT | git+https://github.com/eslint/eslint.git | 8.57.1 | 8.57.1 | ^8.57.1 | Nicholas C. Zakas <nicholas+npm@nczconsulting.com> |
|
||||
| kessler | stuff | eslint-plugin-import | perpetual | material | MIT | git+https://github.com/import-js/eslint-plugin-import.git | 2.32.0 | 2.32.0 | ^2.31.0 | Ben Mosher <me@benmosher.com> |
|
||||
| kessler | stuff | eslint-plugin-react | perpetual | material | MIT | git+https://github.com/jsx-eslint/eslint-plugin-react.git | 7.37.5 | 7.37.5 | ^7.37.5 | Yannick Croissant <yannick.croissant+npm@gmail.com> |
|
||||
| kessler | stuff | eslint-plugin-react-hooks | perpetual | material | MIT | git+https://github.com/facebook/react.git | 4.6.2 | 4.6.2 | ^4.6.2 | n/a |
|
||||
| kessler | stuff | license-report | perpetual | material | MIT | git+https://github.com/kessler/license-report.git | 6.8.2 | 6.8.2 | ^6.7.2 | Yaniv Kessler |
|
||||
| kessler | stuff | postcss | perpetual | material | MIT | git+https://github.com/postcss/postcss.git | 8.5.8 | 8.5.8 | ^8.5.4 | Andrey Sitnik <andrey@sitnik.ru> |
|
||||
| kessler | stuff | postcss-import | perpetual | material | MIT | git+https://github.com/postcss/postcss-import.git | 16.1.1 | 16.1.1 | ^16.1.0 | Maxime Thirouin |
|
||||
| kessler | stuff | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.8.1 | 3.8.1 | ^3.5.3 | James Long |
|
||||
| kessler | stuff | prettier-plugin-organize-imports | perpetual | material | MIT | git+https://github.com/simonhaenisch/prettier-plugin-organize-imports.git | 4.3.0 | 4.3.0 | ^4.1.0 | Simon Haenisch (https://github.com/simonhaenisch) |
|
||||
| kessler | stuff | rimraf | perpetual | material | BlueOak-1.0.0 | git+ssh://git@github.com/isaacs/rimraf.git | 6.1.3 | 6.1.3 | ^6.0.1 | Isaac Z. Schlueter <i@izs.me> (http://blog.izs.me/) |
|
||||
| kessler | stuff | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.60.1 | 4.60.0 | ^4.42.0 | Rich Harris |
|
||||
| kessler | stuff | rollup-plugin-copy | perpetual | material | MIT | git+https://github.com/vladshcherbin/rollup-plugin-copy.git | 3.5.0 | 3.5.0 | ^3.5.0 | Vlad Shcherbin <vlad.shcherbin@gmail.com> |
|
||||
| kessler | stuff | rollup-plugin-postcss | perpetual | material | MIT | git+https://github.com/egoist/rollup-plugin-postcss.git | 4.0.2 | 4.0.2 | ^4.0.2 | EGOIST <0x142857@gmail.com> |
|
||||
| kessler | stuff | rollup-plugin-react-svg | perpetual | material | MIT | git+https://github.com/boopathi/react-svg-loader.git | 3.0.3 | 3.0.3 | ^3.0.3 | boopathi |
|
||||
| kessler | stuff | rollup-plugin-version-injector | perpetual | material | ISC | git+https://github.com/djhouseknecht/rollup-plugin-version-injector.git | 1.3.3 | 1.3.3 | ^1.3.3 | David Houseknecht <david.j.houseknecht@gmail.com> |
|
||||
| kessler | stuff | sass | perpetual | material | MIT | git+https://github.com/sass/dart-sass.git | 1.99.0 | 1.98.0 | ^1.89.1 | Natalie Weizenbaum nweiz@google.com https://github.com/nex3 |
|
||||
| kessler | stuff | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.8.1 | Microsoft Corp. |
|
||||
| kessler | stuff | typed-scss-modules | perpetual | material | MIT | git+https://github.com/skovy/typed-scss-modules.git | 8.1.1 | 8.1.1 | ^8.1.1 | Spencer Miskoviak <smiskoviak@gmail.com> |
|
||||
| kessler | stuff | typescript | perpetual | material | Apache-2.0 | git+https://github.com/microsoft/TypeScript.git | 5.8.3 | 5.8.3 | 5.8.3 | Microsoft Corp. |
|
||||
|
||||
|
||||
@@ -0,0 +1,80 @@
|
||||
import { FC } from 'react';
|
||||
|
||||
interface CGSelectProps {
|
||||
minCG: number;
|
||||
maxCG: number;
|
||||
value: number;
|
||||
disabled: boolean;
|
||||
increase: () => void;
|
||||
decrease: () => void;
|
||||
}
|
||||
|
||||
const CGSelect: FC<CGSelectProps> = ({ minCG, maxCG, value, disabled, increase, decrease }) => {
|
||||
return (
|
||||
<div className="relative">
|
||||
<input
|
||||
disabled
|
||||
className="w-full rounded-lg border border-white bg-zinc-700 px-3 py-2 text-white shadow-sm focus:border-blue-600 focus:outline-none focus:ring-blue-600"
|
||||
value={value.toFixed(1)}
|
||||
/>
|
||||
<button
|
||||
disabled={disabled || value <= minCG}
|
||||
className="absolute right-2 top-0 -mt-[.5px] border-t bg-zinc-700 text-white disabled:text-zinc-400"
|
||||
onClick={increase}
|
||||
>
|
||||
{/* FIXME: FONTAWESOME IN EFB */}
|
||||
<svg
|
||||
aria-hidden="true"
|
||||
focusable="false"
|
||||
data-prefix="fas"
|
||||
data-icon="caret-up"
|
||||
className="svg-inline--fa fa-caret-up "
|
||||
role="img"
|
||||
xmlns="http://www.w3.org/2000/svg"
|
||||
viewBox="0 0 320 512"
|
||||
style={{
|
||||
height: '1em',
|
||||
verticalAlign: '-0.125em',
|
||||
display: 'inline-block',
|
||||
boxSizing: 'content-box',
|
||||
}}
|
||||
>
|
||||
<path
|
||||
fill="currentColor"
|
||||
d="M182.6 137.4c-12.5-12.5-32.8-12.5-45.3 0l-128 128c-9.2 9.2-11.9 22.9-6.9 34.9s16.6 19.8 29.6 19.8H288c12.9 0 24.6-7.8 29.6-19.8s2.2-25.7-6.9-34.9l-128-128z"
|
||||
></path>
|
||||
</svg>
|
||||
</button>
|
||||
<button
|
||||
disabled={disabled || value >= maxCG}
|
||||
className="absolute bottom-0 right-2 -mt-[.5px] border-b bg-zinc-700 text-white disabled:text-zinc-400"
|
||||
onClick={decrease}
|
||||
>
|
||||
{/* FIXME: FONTAWESOME IN EFB */}
|
||||
<svg
|
||||
aria-hidden="true"
|
||||
focusable="false"
|
||||
data-prefix="fas"
|
||||
data-icon="caret-down"
|
||||
className="svg-inline--fa fa-caret-down "
|
||||
role="img"
|
||||
xmlns="http://www.w3.org/2000/svg"
|
||||
viewBox="0 0 320 512"
|
||||
style={{
|
||||
height: '1em',
|
||||
verticalAlign: '-0.125em',
|
||||
display: 'inline-block',
|
||||
boxSizing: 'content-box',
|
||||
}}
|
||||
>
|
||||
<path
|
||||
fill="currentColor"
|
||||
d="M137.4 374.6c12.5 12.5 32.8 12.5 45.3 0l128-128c9.2-9.2 11.9-22.9 6.9-34.9s-16.6-19.8-29.6-19.8L32 192c-12.9 0-24.6 7.8-29.6 19.8s-2.2 25.7 6.9 34.9l128 128z"
|
||||
></path>
|
||||
</svg>
|
||||
</button>
|
||||
</div>
|
||||
);
|
||||
};
|
||||
|
||||
export default CGSelect;
|
||||
@@ -0,0 +1,216 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { WASMDataF } from '../../types/WASMData';
|
||||
import { LoadingState, SimBrief } from '../../types/general';
|
||||
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
||||
import { CoherentCallSBEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import CGSelect from '../CGSelect/CGSelect';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface SBEntryProps {
|
||||
WASMData: WASMDataF;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
const [SBInFlight, setSBInFlight] = useState(false);
|
||||
|
||||
// FROM EFB
|
||||
const simBrief = useSelector((state) => state.simbrief.plan);
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
|
||||
CoherentCallSBEntryF(CGTarget, _fuel ?? fuel, SBPlan);
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [CGTarget, fuel]);
|
||||
useEffect(() => {
|
||||
if (!simBrief || gsxActive) return;
|
||||
|
||||
setSBInFlight(true);
|
||||
|
||||
const SBResponse = ImportFlightPlanKH(
|
||||
simBrief,
|
||||
WASMData.limits.maxZFW,
|
||||
WASMData.limits.maxTOW,
|
||||
WASMData.limits.maxFuel,
|
||||
WASMData.userData.isImperial
|
||||
);
|
||||
if (SBResponse.type === 'error') {
|
||||
console.error('TODO: ERROR', SBResponse.message);
|
||||
setSBInFlight(false);
|
||||
return;
|
||||
}
|
||||
|
||||
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
|
||||
|
||||
updateData(SBResponse.message as SimBrief, _fuel);
|
||||
|
||||
setFuel(_fuel);
|
||||
setSBInFlight(false);
|
||||
}, [simBrief, gsxActive]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Planned ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={WASMData.sbPlanned.ZFW}
|
||||
disabled
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Planned GW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={WASMData.sbPlanned.GW}
|
||||
disabled
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
|
||||
</label>
|
||||
<CGSelect
|
||||
minCG={WASMData.limits.minCG}
|
||||
maxCG={WASMData.limits.maxCG}
|
||||
value={CGTarget}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
increase={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev + 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
decrease={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev - 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!GWValid() || SBInFlight}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default SBEntryF;
|
||||
@@ -0,0 +1,219 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { WASMDataPax } from '../../types/WASMData';
|
||||
import { LoadingState, SimBrief } from '../../types/general';
|
||||
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
||||
import { CoherentCallSBEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import CGSelect from '../CGSelect/CGSelect';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface SBEntryProps {
|
||||
WASMData: WASMDataPax;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
const [SBInFlight, setSBInFlight] = useState(false);
|
||||
|
||||
// FROM EFB
|
||||
const simBrief = useSelector((state) => state.simbrief.plan);
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
|
||||
CoherentCallSBEntryPax(CGTarget, _fuel ?? fuel, SBPlan);
|
||||
};
|
||||
|
||||
useEffect(() => {
|
||||
if (!simBrief || gsxActive) return;
|
||||
|
||||
setSBInFlight(true);
|
||||
|
||||
const SBResponse = ImportFlightPlanKH(
|
||||
simBrief,
|
||||
WASMData.limits.maxZFW,
|
||||
WASMData.limits.maxTOW,
|
||||
WASMData.limits.maxFuel,
|
||||
WASMData.userData.isImperial
|
||||
);
|
||||
if (SBResponse.type === 'error') {
|
||||
console.error('TODO: ERROR', SBResponse.message);
|
||||
setSBInFlight(false);
|
||||
return;
|
||||
}
|
||||
|
||||
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
|
||||
|
||||
updateData(SBResponse.message as SimBrief, _fuel);
|
||||
|
||||
setFuel(_fuel);
|
||||
|
||||
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
|
||||
setSBInFlight(false);
|
||||
}, [simBrief, gsxActive]);
|
||||
|
||||
useEffect(() => updateData(), [CGTarget, fuel]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Planned ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={WASMData.sbPlanned.ZFW}
|
||||
disabled
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Planned GW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={WASMData.sbPlanned.GW}
|
||||
disabled
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="flex w-full items-center justify-between rounded-b-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
|
||||
</label>
|
||||
<CGSelect
|
||||
minCG={WASMData.limits.minCG}
|
||||
maxCG={WASMData.limits.maxCG}
|
||||
value={CGTarget}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
increase={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev + 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
decrease={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev - 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!GWValid() || SBInFlight}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default SBEntryPax;
|
||||
@@ -0,0 +1,38 @@
|
||||
import { FC } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
|
||||
interface ActionBarProps {
|
||||
loadingState: LoadingState;
|
||||
loadDisabled: boolean;
|
||||
GSXSync: boolean;
|
||||
load: () => void;
|
||||
unload: () => void;
|
||||
}
|
||||
|
||||
const ActionBar: FC<ActionBarProps> = ({ loadingState, loadDisabled, GSXSync, load, unload }) => {
|
||||
return (
|
||||
<div className="relative flex w-full items-center justify-start gap-x-6">
|
||||
{loadingState === 'preview' && !GSXSync && (
|
||||
<button
|
||||
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
|
||||
data-ripple-light="true"
|
||||
onClick={load}
|
||||
disabled={loadDisabled}
|
||||
>
|
||||
Load
|
||||
</button>
|
||||
)}
|
||||
{loadingState === 'loaded' && !GSXSync && (
|
||||
<button
|
||||
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
|
||||
data-ripple-light="true"
|
||||
onClick={unload}
|
||||
>
|
||||
Unload
|
||||
</button>
|
||||
)}
|
||||
</div>
|
||||
);
|
||||
};
|
||||
|
||||
export default ActionBar;
|
||||
@@ -1,9 +0,0 @@
|
||||
const Freight = () => {
|
||||
return (
|
||||
<div>
|
||||
<img src="assets/img/MD11_Profile.svg" style={{ width: '100%' }} />
|
||||
</div>
|
||||
);
|
||||
};
|
||||
|
||||
export default Freight;
|
||||
@@ -0,0 +1,162 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { GSXFuelingState, GSXLoadingState, WASMDataF } from '../../types/WASMData';
|
||||
import OptionsF from '../options/OptionsF';
|
||||
import Profile from '../profile/Profile';
|
||||
import SBEntryF from '../SBEntry/SBEntryF';
|
||||
import StationEntryF from '../stationEntry/StationEntryF';
|
||||
import Tabbar from '../tabbar/Tabbar';
|
||||
import ZFWEntryF from '../zfwEntry/ZFWEntryF';
|
||||
|
||||
interface FreighterProps {
|
||||
WASMData: WASMDataF;
|
||||
username?: string;
|
||||
}
|
||||
|
||||
const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
||||
const [selectedTab, setSelectedTab] = useState(0);
|
||||
const [loadingState, setLoadingState] = useState<LoadingState>('preview');
|
||||
|
||||
const upper1 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper1);
|
||||
|
||||
return Math.round(WASMData.livePayload.upper1);
|
||||
};
|
||||
const upper2 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper2);
|
||||
|
||||
return Math.round(WASMData.livePayload.upper2);
|
||||
};
|
||||
const upper3 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper3);
|
||||
|
||||
return Math.round(WASMData.livePayload.upper3);
|
||||
};
|
||||
const upper4 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper4);
|
||||
|
||||
return Math.round(WASMData.livePayload.upper4);
|
||||
};
|
||||
const lower1 = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.lowerForward);
|
||||
|
||||
return Math.round(WASMData.livePayload.lowerForward);
|
||||
};
|
||||
const lower2 = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.lowerRear);
|
||||
|
||||
return Math.round(WASMData.livePayload.lowerRear);
|
||||
};
|
||||
const OEW = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.empty);
|
||||
|
||||
return Math.round(WASMData.livePayload.empty);
|
||||
};
|
||||
const crew = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.crew);
|
||||
|
||||
return Math.round(WASMData.livePayload.crew);
|
||||
};
|
||||
|
||||
const GSXActive = () => {
|
||||
return (
|
||||
WASMData.GSX.couatlStarted &&
|
||||
WASMData.GSX.loadingState !== GSXLoadingState.IDLE &&
|
||||
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
||||
);
|
||||
};
|
||||
const GSXFuelActive = () => {
|
||||
return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
|
||||
};
|
||||
|
||||
const CGs = (): [string, boolean, string, boolean] => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) {
|
||||
return [
|
||||
WASMData.targetPayload.ZFWCG.toFixed(1),
|
||||
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.targetPayload.TOCG.toFixed(1),
|
||||
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
}
|
||||
|
||||
if (WASMData.options.GSXSync && GSXActive() && WASMData.GSX.loadingState === GSXLoadingState.BOARDING) {
|
||||
return [
|
||||
WASMData.targetPayload.ZFWCG.toFixed(1),
|
||||
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.targetPayload.TOCG.toFixed(1),
|
||||
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
}
|
||||
|
||||
return [
|
||||
WASMData.livePayload.ZFWCG.toFixed(1),
|
||||
WASMData.livePayload.ZFWCG < WASMData.limits.minCG || WASMData.livePayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.livePayload.TOCG.toFixed(1),
|
||||
WASMData.livePayload.TOCG < WASMData.limits.minCG || WASMData.livePayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
};
|
||||
|
||||
useEffect(() => {
|
||||
setLoadingState(WASMData.loaded ? 'loaded' : 'preview');
|
||||
}, [WASMData.loaded]);
|
||||
|
||||
return (
|
||||
<>
|
||||
<Profile
|
||||
type="F"
|
||||
isER={WASMData.userData.isER}
|
||||
upper1={`${upper1(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper2={`${upper2(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper3={`${upper3(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper4={`${upper4(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
lower1={`${lower1()}`}
|
||||
lower2={`${lower2()}`}
|
||||
OEW={`${OEW()}`}
|
||||
crew={`${crew()}`}
|
||||
unit={WASMData.userData.isImperial ? 'LBS' : 'KG'}
|
||||
inPreview={loadingState !== 'loaded' && !GSXActive()}
|
||||
CGs={CGs()}
|
||||
done={
|
||||
WASMData.options.GSXSync ? WASMData.GSX.loadingState === GSXLoadingState.BOARDED : loadingState !== 'preview'
|
||||
}
|
||||
/>
|
||||
<Tabbar
|
||||
tabs={username ? ['Simbrief', 'ZFW', 'Cargo', 'Options'] : ['ZFW', 'Cargo', 'Options']}
|
||||
selectedTab={selectedTab}
|
||||
setSelectedTab={setSelectedTab}
|
||||
/>
|
||||
{username && selectedTab === 0 && (
|
||||
<SBEntryF
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
||||
<ZFWEntryF
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
||||
<StationEntryF
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
||||
<OptionsF WASMData={WASMData} loadingState={loadingState} gsxActive={GSXActive()} />
|
||||
)}
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default Freighter;
|
||||
@@ -0,0 +1,102 @@
|
||||
import { useEffect, useRef, useState } from 'react';
|
||||
import { v4 } from 'uuid';
|
||||
import Keyboard from '../keyboard/Keyboard';
|
||||
|
||||
export default function Input(props: {
|
||||
type?: string;
|
||||
topKeyboard?: boolean;
|
||||
value: number | string;
|
||||
min?: number;
|
||||
max?: number;
|
||||
step?: number;
|
||||
placeholder?: string;
|
||||
className?: string;
|
||||
disabled?: boolean;
|
||||
onChange?: (value: string) => void;
|
||||
onBlur?: (value: string) => void;
|
||||
}) {
|
||||
const [guid] = useState(v4());
|
||||
const ref = useRef<HTMLInputElement>(null);
|
||||
const keyboardRef = useRef<HTMLDivElement>(null);
|
||||
const blurRef = useRef<boolean>(false);
|
||||
const [isFocused, setFocused] = useState(false);
|
||||
const [showKeyboard, setShowKeyboard] = useState(false);
|
||||
const [unfocusTimer, setUnfocusTimer] = useState<NodeJS.Timeout | null>(null);
|
||||
|
||||
useEffect(() => {
|
||||
if (unfocusTimer) {
|
||||
clearTimeout(unfocusTimer);
|
||||
setUnfocusTimer(null);
|
||||
}
|
||||
|
||||
if (isFocused) {
|
||||
setUnfocusTimer(setTimeout(() => ref.current?.blur(), 5e3));
|
||||
Coherent.trigger('FOCUS_INPUT_FIELD', guid, '', '', '', false);
|
||||
} else {
|
||||
console.log('UNFOCUS_INPUT_FIELD');
|
||||
Coherent.trigger('UNFOCUS_INPUT_FIELD', guid);
|
||||
}
|
||||
|
||||
return () => {
|
||||
if (unfocusTimer) {
|
||||
clearTimeout(unfocusTimer);
|
||||
setUnfocusTimer(null);
|
||||
}
|
||||
};
|
||||
}, [isFocused, guid]);
|
||||
|
||||
return (
|
||||
<>
|
||||
<input
|
||||
ref={ref}
|
||||
type={props.type ? props.type : 'text'}
|
||||
min={props.min}
|
||||
max={props.max}
|
||||
step={props.step}
|
||||
placeholder={props.placeholder}
|
||||
disabled={props.disabled}
|
||||
onFocus={() => {
|
||||
if (!isFocused) {
|
||||
setFocused(true);
|
||||
setShowKeyboard(true);
|
||||
ref.current?.select();
|
||||
}
|
||||
}}
|
||||
onBlur={(e) => {
|
||||
if (blurRef.current && isFocused) ref.current?.focus();
|
||||
else {
|
||||
props.onBlur?.(e.target.value);
|
||||
setShowKeyboard(false);
|
||||
setFocused(false);
|
||||
ref.current?.blur();
|
||||
}
|
||||
blurRef.current = false;
|
||||
}}
|
||||
onChange={(e) => {
|
||||
if (props.onChange) props.onChange(e.target.value);
|
||||
if (unfocusTimer) {
|
||||
clearTimeout(unfocusTimer);
|
||||
setUnfocusTimer(null);
|
||||
}
|
||||
if (isFocused) setUnfocusTimer(setTimeout(() => ref.current?.blur(), 5e3));
|
||||
}}
|
||||
value={props.value}
|
||||
className={props.className}
|
||||
/>
|
||||
{showKeyboard && (
|
||||
<Keyboard
|
||||
ref={keyboardRef}
|
||||
top={props.topKeyboard}
|
||||
value={String(props.value)}
|
||||
blurRef={blurRef}
|
||||
onInput={(value) => props.onChange && props.onChange(value)}
|
||||
onClose={() => {
|
||||
setShowKeyboard(false);
|
||||
setFocused(false);
|
||||
ref.current?.blur();
|
||||
}}
|
||||
/>
|
||||
)}
|
||||
</>
|
||||
);
|
||||
}
|
||||
@@ -0,0 +1,108 @@
|
||||
import { ArrowBigUp, Delete, Space, X } from 'lucide-react';
|
||||
import { forwardRef, RefObject, useState } from 'react';
|
||||
import { createPortal } from 'react-dom';
|
||||
|
||||
const defaultLayout = {
|
||||
default: [
|
||||
'1 2 3 4 5 6 7 8 9 0 {bksp}',
|
||||
'q w e r t y u i o p',
|
||||
'a s d f g h j k l',
|
||||
'{shift} z x c v b n m /',
|
||||
'{space} {close}',
|
||||
],
|
||||
shift: [
|
||||
'1 2 3 4 5 6 7 8 9 0 {bksp}',
|
||||
'Q W E R T Y U I O P',
|
||||
'A S D F G H J K L',
|
||||
'{shift} Z X C V B N M /',
|
||||
'{space} {close}',
|
||||
],
|
||||
};
|
||||
|
||||
const Keyboard = forwardRef<
|
||||
HTMLDivElement,
|
||||
{
|
||||
value: string;
|
||||
blurRef: RefObject<boolean>;
|
||||
top?: boolean;
|
||||
onInput: (value: string) => void;
|
||||
onClose: () => void;
|
||||
}
|
||||
>(({ value, top, blurRef, onInput, onClose }, ref) => {
|
||||
const [shift, setShift] = useState(false);
|
||||
|
||||
const layout = shift ? defaultLayout.shift : defaultLayout.default;
|
||||
|
||||
const handleKeyPress = (key: string) => {
|
||||
console.log('KEY PRESSED', key);
|
||||
|
||||
if (key === '{close}') {
|
||||
onClose();
|
||||
return;
|
||||
}
|
||||
|
||||
blurRef.current = true;
|
||||
|
||||
if (key === '{shift}') {
|
||||
setShift(!shift);
|
||||
return;
|
||||
}
|
||||
|
||||
let newValue = value;
|
||||
|
||||
if (key === '{bksp}') {
|
||||
newValue = value.slice(0, -1);
|
||||
} else if (key === '{space}') {
|
||||
newValue = value + ' ';
|
||||
} else if (key.length === 1) {
|
||||
newValue = value + key;
|
||||
}
|
||||
|
||||
onInput(newValue);
|
||||
};
|
||||
|
||||
return createPortal(
|
||||
<div
|
||||
ref={ref}
|
||||
className={`absolute ${top ? 'top-0' : 'bottom-0'} left-0 z-50 box-border w-full touch-manipulation select-none overflow-hidden bg-zinc-800 p-2 text-white`}
|
||||
>
|
||||
{layout.map((row, rowIndex) => (
|
||||
<div key={`row-${rowIndex}`} className="mb-1 flex w-full justify-center gap-1">
|
||||
{row.split(' ').map((key, keyIndex) => {
|
||||
let keyIdent = <>{key}</>;
|
||||
switch (key) {
|
||||
case '{shift}':
|
||||
keyIdent = <ArrowBigUp />;
|
||||
break;
|
||||
case '{bksp}':
|
||||
keyIdent = <Delete />;
|
||||
break;
|
||||
case '{close}':
|
||||
keyIdent = <X />;
|
||||
break;
|
||||
case '{space}':
|
||||
keyIdent = <Space />;
|
||||
break;
|
||||
}
|
||||
|
||||
return (
|
||||
<button
|
||||
key={`key-${rowIndex}-${keyIndex}`}
|
||||
className={`flex justify-center rounded-md p-4 ${
|
||||
key === '{close}' ? 'bg-zinc-700 px-12 focus:bg-zinc-600' : 'flex-1 bg-zinc-600'
|
||||
}`}
|
||||
onMouseDown={() => handleKeyPress(key)}
|
||||
>
|
||||
{keyIdent}
|
||||
</button>
|
||||
);
|
||||
})}
|
||||
</div>
|
||||
))}
|
||||
</div>,
|
||||
document.body
|
||||
);
|
||||
});
|
||||
Keyboard.displayName = "Keyboard"
|
||||
|
||||
export default Keyboard;
|
||||
@@ -0,0 +1,121 @@
|
||||
import { FC } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { WASMDataF } from '../../types/WASMData';
|
||||
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
|
||||
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
|
||||
|
||||
interface OptionsFProps {
|
||||
WASMData: WASMDataF;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
}
|
||||
|
||||
const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<ToggleComponentKH
|
||||
optionName="GSX Sync"
|
||||
value={WASMData.options.GSXSync}
|
||||
leftLabel={{ value: true }}
|
||||
rightLabel={{ value: false }}
|
||||
backgroundColor="bg-zinc-700"
|
||||
setValue={(value) => {
|
||||
CoherentCallOptionsSet(value);
|
||||
}}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
{WASMData.userData.isER ? (
|
||||
<>
|
||||
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - ER Variant</h2>
|
||||
<table className="text-xs">
|
||||
<tbody>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Passengers</td>
|
||||
<td className="p-1 px-2">0</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Passenger Weight</td>
|
||||
<td className="p-1 px-2">1 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Bag Weight</td>
|
||||
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249537 lbs' : '113188 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '451300 lbs' : '204706 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Takeoff Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '630500 lbs' : '285990 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Fuel Capacity</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '282619 lbs' : '128193 kg'}</td>
|
||||
</tr>
|
||||
</tbody>
|
||||
</table>
|
||||
</>
|
||||
) : (
|
||||
<>
|
||||
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - Normal variant</h2>
|
||||
<table className="text-xs">
|
||||
<tbody>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Passengers</td>
|
||||
<td className="p-1 px-2">0</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Passenger Weight</td>
|
||||
<td className="p-1 px-2">1 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Bag Weight</td>
|
||||
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249137 lbs' : '113006 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '451300 lbs' : '204706 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Takeoff Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '625500 lbs' : '283722 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Fuel Capacity</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '256207 lbs' : '116213 kg'}</td>
|
||||
</tr>
|
||||
</tbody>
|
||||
</table>
|
||||
</>
|
||||
)}
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<button
|
||||
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
|
||||
data-ripple-light="true"
|
||||
onClick={CoherentCallGSXReset}
|
||||
>
|
||||
Reset internal GSX state
|
||||
</button>
|
||||
</div>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default OptionsF;
|
||||
@@ -0,0 +1,182 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { WASMDataPax } from '../../types/WASMData';
|
||||
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
|
||||
import Input from '../input/Input';
|
||||
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
|
||||
|
||||
interface OptionsPaxProps {
|
||||
WASMData: WASMDataPax;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
}
|
||||
|
||||
const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive }) => {
|
||||
const [paxWeight, setPaxWeight] = useState(WASMData.options.paxWeight);
|
||||
const [bagWeight, setBagWeight] = useState(WASMData.options.bagWeight);
|
||||
|
||||
const updateData = () => {
|
||||
CoherentCallOptionsSet(undefined, paxWeight, bagWeight);
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [paxWeight, bagWeight]);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<ToggleComponentKH
|
||||
optionName="GSX Sync"
|
||||
value={WASMData.options.GSXSync}
|
||||
leftLabel={{ value: true }}
|
||||
rightLabel={{ value: false }}
|
||||
backgroundColor="bg-zinc-700"
|
||||
setValue={(value) => {
|
||||
CoherentCallOptionsSet(value);
|
||||
}}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Pax Weight ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={paxWeight}
|
||||
onChange={(value) => handleInput(value, Number.MAX_VALUE, setPaxWeight)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Bag Weight ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={bagWeight}
|
||||
onChange={(value) => handleInput(value, Number.MAX_VALUE, setBagWeight)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
{WASMData.userData.isER ? (
|
||||
<>
|
||||
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - ER Variant</h2>
|
||||
<table className="text-xs">
|
||||
<tbody>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Passengers</td>
|
||||
<td className="p-1 px-2">313</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Passenger Weight</td>
|
||||
<td className="p-1 px-2">
|
||||
{WASMData.options.paxWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
|
||||
</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Bag Weight</td>
|
||||
<td className="p-1 px-2">
|
||||
{WASMData.options.bagWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
|
||||
</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286465 lbs' : '129937 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '400000 lbs' : '181437 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Takeoff Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '630500 lbs' : '285990 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Fuel Capacity</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '282619 lbs' : '128193 kg'}</td>
|
||||
</tr>
|
||||
</tbody>
|
||||
</table>
|
||||
</>
|
||||
) : (
|
||||
<>
|
||||
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - Normal variant</h2>
|
||||
<table className="text-xs">
|
||||
<tbody>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Passengers</td>
|
||||
<td className="p-1 px-2">313</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Passenger Weight</td>
|
||||
<td className="p-1 px-2">
|
||||
{WASMData.options.paxWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
|
||||
</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Bag Weight</td>
|
||||
<td className="p-1 px-2">
|
||||
{WASMData.options.bagWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
|
||||
</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286065 lbs' : '129755 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '400000 lbs' : '181437 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Takeoff Weight</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '625500 lbs' : '283722 kg'}</td>
|
||||
</tr>
|
||||
<tr>
|
||||
<td className="p-1 px-2">Max Fuel Capacity</td>
|
||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '256207 lbs' : '116213 kg'}</td>
|
||||
</tr>
|
||||
</tbody>
|
||||
</table>
|
||||
</>
|
||||
)}
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<button
|
||||
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
|
||||
data-ripple-light="true"
|
||||
onClick={CoherentCallGSXReset}
|
||||
>
|
||||
Reset internal GSX state & disable SYNC
|
||||
</button>
|
||||
</div>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default OptionsPax;
|
||||
@@ -1,51 +1,167 @@
|
||||
import { FC } from 'react';
|
||||
import {
|
||||
maxBusiness1StationCount,
|
||||
maxBusiness2StationCount,
|
||||
maxEconomy1StationCount,
|
||||
maxEconomy2StationCount,
|
||||
paxWeight,
|
||||
PayloadPax,
|
||||
} from '../../configs/pax';
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { GSXFuelingState, GSXLoadingState, WASMDataPax } from '../../types/WASMData';
|
||||
import OptionsPax from '../options/OptionsPax';
|
||||
import Profile from '../profile/Profile';
|
||||
import SBEntryPax from '../SBEntry/SBEntryPax';
|
||||
import StationEntryPax from '../stationEntry/StationEntryPax';
|
||||
import Tabbar from '../tabbar/Tabbar';
|
||||
import ZFWEntryPax from '../zfwEntry/ZFWEntryPax';
|
||||
|
||||
interface PaxProps {
|
||||
unit: 'kg' | 'lbs';
|
||||
payload: PayloadPax;
|
||||
WASMData: WASMDataPax;
|
||||
username?: string;
|
||||
}
|
||||
|
||||
const Pax: FC<PaxProps> = ({ unit, payload }) => {
|
||||
const upper1 = () => {
|
||||
return Math.round((payload.business1Left + payload.business1Center + payload.business1Right) / paxWeight[unit]);
|
||||
const Pax: FC<PaxProps> = ({ WASMData, username }) => {
|
||||
const [selectedTab, setSelectedTab] = useState(0);
|
||||
const [loadingState, setLoadingState] = useState<LoadingState>('preview');
|
||||
|
||||
const upper1 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return WASMData.targetPayload.business1;
|
||||
|
||||
return WASMData.livePayload.business1;
|
||||
};
|
||||
const upper2 = () => {
|
||||
return Math.round((payload.business2Left + payload.business2Center + payload.business2Right) / paxWeight[unit]);
|
||||
const upper2 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return WASMData.targetPayload.business2;
|
||||
|
||||
return WASMData.livePayload.business2;
|
||||
};
|
||||
const upper3 = () => {
|
||||
return Math.round((payload.economy1Left + payload.economy1Center + payload.economy1Right) / paxWeight[unit]);
|
||||
const upper3 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return WASMData.targetPayload.economy1;
|
||||
|
||||
return WASMData.livePayload.economy1;
|
||||
};
|
||||
const upper4 = () => {
|
||||
return Math.round((payload.economy2Left + payload.economy2Center + payload.economy2Right) / paxWeight[unit]);
|
||||
const upper4 = (overrideState: LoadingState = loadingState) => {
|
||||
if (overrideState !== 'loaded') return WASMData.targetPayload.economy2;
|
||||
|
||||
return WASMData.livePayload.economy2;
|
||||
};
|
||||
const lower1 = () => {
|
||||
return Math.round(payload.forwardCargo);
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.forwardCargo);
|
||||
|
||||
return Math.round(WASMData.livePayload.forwardCargo);
|
||||
};
|
||||
const lower2 = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.rearCargo);
|
||||
|
||||
return Math.round(WASMData.livePayload.rearCargo);
|
||||
};
|
||||
const OEW = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.empty);
|
||||
|
||||
return Math.round(WASMData.livePayload.empty);
|
||||
};
|
||||
const crew = () => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.crew);
|
||||
|
||||
return Math.round(WASMData.livePayload.crew);
|
||||
};
|
||||
|
||||
const lower2 = () => {
|
||||
return Math.round(payload.rearCargo);
|
||||
const GSXActive = () => {
|
||||
return (
|
||||
WASMData.GSX.couatlStarted &&
|
||||
WASMData.GSX.loadingState !== GSXLoadingState.IDLE &&
|
||||
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
||||
);
|
||||
};
|
||||
const GSXFuelActive = () => {
|
||||
return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
|
||||
};
|
||||
|
||||
const CGs = (): [string, boolean, string, boolean] => {
|
||||
if (loadingState !== 'loaded' && !GSXActive()) {
|
||||
return [
|
||||
WASMData.targetPayload.ZFWCG.toFixed(1),
|
||||
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.targetPayload.TOCG.toFixed(1),
|
||||
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
}
|
||||
|
||||
if (WASMData.options.GSXSync && GSXActive() && WASMData.GSX.loadingState === GSXLoadingState.BOARDING) {
|
||||
return [
|
||||
WASMData.targetPayload.ZFWCG.toFixed(1),
|
||||
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.targetPayload.TOCG.toFixed(1),
|
||||
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
}
|
||||
|
||||
return [
|
||||
WASMData.livePayload.ZFWCG.toFixed(1),
|
||||
WASMData.livePayload.ZFWCG < WASMData.limits.minCG || WASMData.livePayload.ZFWCG > WASMData.limits.maxCG,
|
||||
WASMData.livePayload.TOCG.toFixed(1),
|
||||
WASMData.livePayload.TOCG < WASMData.limits.minCG || WASMData.livePayload.TOCG > WASMData.limits.maxCG,
|
||||
];
|
||||
};
|
||||
|
||||
useEffect(() => {
|
||||
setLoadingState(WASMData.loaded ? 'loaded' : 'preview');
|
||||
}, [WASMData.loaded]);
|
||||
|
||||
return (
|
||||
<div style={{ position: 'relative' }}>
|
||||
<>
|
||||
<Profile
|
||||
upper1={`${upper1()}/${maxBusiness1StationCount}`}
|
||||
upper2={`${upper2()}/${maxBusiness2StationCount}`}
|
||||
upper3={`${upper3()}/${maxEconomy1StationCount}`}
|
||||
upper4={`${upper4()}/${maxEconomy2StationCount}`}
|
||||
type="PAX"
|
||||
isER={WASMData.userData.isER}
|
||||
upper1={`${upper1(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper1max={loadingState === 'loaded' || GSXActive() ? `${upper1('preview')}` : `${WASMData.limits.business1}`}
|
||||
upper2={`${upper2(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper2max={loadingState === 'loaded' || GSXActive() ? `${upper2('preview')}` : `${WASMData.limits.business2}`}
|
||||
upper3={`${upper3(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper3max={loadingState === 'loaded' || GSXActive() ? `${upper3('preview')}` : `${WASMData.limits.economy1}`}
|
||||
upper4={`${upper4(GSXActive() ? 'loaded' : loadingState)}`}
|
||||
upper4max={loadingState === 'loaded' || GSXActive() ? `${upper4('preview')}` : `${WASMData.limits.economy2}`}
|
||||
lower1={`${lower1()}`}
|
||||
lower2={`${lower2()}`}
|
||||
OEW={`${OEW()}`}
|
||||
crew={`${crew()}`}
|
||||
unit={WASMData.userData.isImperial ? 'LBS' : 'KG'}
|
||||
inPreview={loadingState !== 'loaded' && !GSXActive()}
|
||||
CGs={CGs()}
|
||||
done={
|
||||
WASMData.options.GSXSync ? WASMData.GSX.loadingState === GSXLoadingState.BOARDED : loadingState !== 'preview'
|
||||
}
|
||||
/>
|
||||
</div>
|
||||
<Tabbar
|
||||
tabs={
|
||||
username ? ['Simbrief', 'ZFW', 'Passengers & Cargo', 'Options'] : ['ZFW', 'Passengers & Cargo', 'Options']
|
||||
}
|
||||
selectedTab={selectedTab}
|
||||
setSelectedTab={setSelectedTab}
|
||||
/>
|
||||
{username && selectedTab === 0 && (
|
||||
<SBEntryPax
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
||||
<ZFWEntryPax
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
||||
<StationEntryPax
|
||||
WASMData={WASMData}
|
||||
loadingState={loadingState}
|
||||
setLoadingState={setLoadingState}
|
||||
gsxActive={GSXActive()}
|
||||
gsxFuelActive={GSXFuelActive()}
|
||||
/>
|
||||
)}
|
||||
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
||||
<OptionsPax WASMData={WASMData} loadingState={loadingState} gsxActive={GSXActive()} />
|
||||
)}
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
|
||||
@@ -0,0 +1,14 @@
|
||||
.stroke-zinc-600 {
|
||||
--tw-bg-opacity: 1;
|
||||
stroke: rgba(82, 82, 91, var(--tw-bg-opacity));
|
||||
}
|
||||
|
||||
.fill-neutral-500 {
|
||||
--tw-text-opacity: 1;
|
||||
fill: rgba(115, 115, 115, var(--tw-text-opacity));
|
||||
}
|
||||
|
||||
.fill-red-500 {
|
||||
--tw-bg-opacity: 1;
|
||||
fill: rgba(239, 68, 68, var(--tw-bg-opacity));
|
||||
}
|
||||
@@ -1,82 +1,144 @@
|
||||
import { FC } from 'react';
|
||||
|
||||
import styles from './Profile.module.scss';
|
||||
|
||||
interface ProfileProps {
|
||||
type: 'F' | 'PAX';
|
||||
isER: boolean;
|
||||
upper1: string;
|
||||
upper1max?: string;
|
||||
upper2: string;
|
||||
upper2max?: string;
|
||||
upper3: string;
|
||||
upper3max?: string;
|
||||
upper4: string;
|
||||
upper4max?: string;
|
||||
lower1: string;
|
||||
lower2: string;
|
||||
OEW: string;
|
||||
crew: string;
|
||||
CGs: [string, boolean, string, boolean];
|
||||
unit: string;
|
||||
inPreview: boolean;
|
||||
done: boolean;
|
||||
}
|
||||
|
||||
const Profile: FC<ProfileProps> = ({ upper1, upper2, upper3, upper4, lower1, lower2 }) => {
|
||||
const Profile: FC<ProfileProps> = ({
|
||||
type,
|
||||
isER,
|
||||
upper1,
|
||||
upper1max,
|
||||
upper2,
|
||||
upper2max,
|
||||
upper3,
|
||||
upper3max,
|
||||
upper4,
|
||||
upper4max,
|
||||
lower1,
|
||||
lower2,
|
||||
OEW,
|
||||
crew,
|
||||
CGs,
|
||||
unit,
|
||||
inPreview,
|
||||
done,
|
||||
}) => {
|
||||
const previewClass = inPreview ? styles['fill-neutral-500'] : undefined;
|
||||
const doneClass = done ? undefined : styles['fill-neutral-500'];
|
||||
const ZFWCGClass = CGs[1] ? styles['fill-red-500'] : doneClass;
|
||||
const TOCGClass = CGs[3] ? styles['fill-red-500'] : doneClass;
|
||||
|
||||
return (
|
||||
<svg
|
||||
width="4000"
|
||||
height="777"
|
||||
viewBox="0 0 4000 777"
|
||||
version="1.1"
|
||||
xmlns="http://www.w3.org/2000/svg"
|
||||
style={{ width: '100%', height: '100%' }}
|
||||
>
|
||||
<g transform="matrix(1.0068517,0,0,1.0069072,-24.265193,-12.003831)">
|
||||
<path
|
||||
style={{ fill: 'none', stroke: '#000000', strokeWidth: 2 }}
|
||||
d="M 680.84609,782.08906 C 549.70893,776.57617 458.39197,765.86739 324.268,740.27364 246.14504,725.36614 162.88028,702.65084 114.71005,683.10491 64.294422,662.64808 29.662286,634.19107 25.770394,610.02401 c -3.768309,-23.39909 7.45579,-38.27601 50.497871,-66.9322 6.041267,-4.02167 12.708198,-9.25866 14.816502,-11.63777 2.108011,-2.3791 4.524337,-4.47417 4.524337,-4.47417 0,0 45.054846,-44.16802 69.744156,-58.51947 72.48238,-42.13286 238.75805,-76.34072 425.62931,-87.56471 14.00364,-0.84087 33.99811,-2.06795 44.43237,-2.72604 26.21714,-1.65429 1973.23226,-2.44974 2062.35136,-0.84335 156.7308,2.8263 269.4991,7.73127 530.5484,23.07714 47.1492,2.77159 85.8529,4.90003 86.0115,4.72947 0.6463,-0.69343 3.1799,-46.29263 2.6116,-46.94111 -0.3392,-0.38556 -8.4798,-1.62861 -18.0916,-2.7617 -35.342,-4.16857 -67.3987,-11.80933 -77.0775,-18.373 -3.9158,-2.65461 -3.9645,-3.9457 -1.9416,-51.05288 2.108,-49.09699 3.1187,-81.38198 3.1285,-99.87491 0,-21.74527 -0.1657,-21.35031 11.1205,-24.91522 37.4056,-11.81592 117.8805,-11.055 171.1113,1.6182 15.227,3.62513 19.5889,3.51038 35.537,-0.93493 21.7,-6.04964 21.06,-5.5085 96.6369,-81.945831 C 3570.4998,46.436494 3606.118,14 3606.118,14 c 0,0 83.3791,-1.078541 169.2378,-1.078541 136.9775,0 171.6157,0.25301 171.2171,1.248541 -4.4107,10.98979 -56.581,125.3361 -58.6915,128.64097 -4.61,7.2154 -3.2138,7.87286 16.7587,7.89172 9.0621,0.008 22.5342,1.10149 37.2287,3.01945 4.1187,0.5379 15.3535,1.65128 24.9605,2.47427 9.6121,0.82315 19.8324,1.75527 22.7174,2.07148 5.068,0.5564 9.0513,198.14866 3.9933,198.1233 -3.6048,-0.0227 -31.7006,3.23162 -34.6989,4.01342 -1.9198,0.50096 -6.9751,1.19108 -11.2311,1.53277 -7.7386,0.62134 -7.7386,0.62134 -7.7386,8.40744 0,8.9212 0.045,8.96677 9.985,9.01912 7.5949,0.034 9.8123,1.6324 3.4137,2.45002 -2.7018,0.34529 -6.0356,0.83128 -7.4075,1.08125 -1.3721,0.24985 -13.4623,0.8929 -26.8656,1.4305 -13.401,0.53782 -28.9024,1.43993 -34.4461,2.0055 -15.6071,1.5929 -41.7206,3.00651 -55.6343,3.01162 -20.6343,0.008 -19.0304,-1.48657 -18.6619,17.39371 0.3714,18.99365 2.3135,23.83102 11.5516,28.75828 5.5848,2.97987 0.3035,2.54463 88.3394,7.28049 84.7137,4.55708 75.1577,-2.80725 75.1577,57.90224 0,54.0198 0.038,53.89862 -18.7911,59.76707 -20.408,6.36127 -118.4491,34.26355 -182.9035,52.0539 -74.4101,20.53866 -152.6313,42.46259 -160.2532,44.9152 -10.5871,3.40625 -57.116,16.36682 -105.4328,29.36671 -184.6218,49.67348 -402.045,89.66531 -516.1192,94.93296 -19.1653,0.88463 -2300.05965,1.25451 -2320.95791,0.37647 z M 2395.2284,766.17343 c 14.31,-1.72636 35.0044,-5.58482 45.9317,-8.56349 47.3731,-12.91382 34.3569,-20.54665 -70.3937,-41.28467 -9.3343,-1.84814 -21.9155,-4.52456 -27.9567,-5.94725 -119.2237,-28.08138 -135.9351,-31.12662 -227.3855,-41.43261 -32.4777,-3.66009 -84.0044,-11.38065 -126.5741,-18.96537 -77.5998,-13.826 -129.5464,-21.92668 -156.7612,-24.44667 -178.2006,-16.50013 -260.2484,38.63673 -109.1218,73.33233 7.2585,1.66581 18.9421,5.28886 25.9627,8.05145 39.3006,15.46148 111.0206,26.31652 233.4285,35.33072 97.5086,7.18033 247.1863,10.12384 247.9332,4.8756 0.6641,-4.65753 1.511,-4.79372 36.7152,-5.87802 22.9807,-0.70754 26.3782,-0.21453 26.3782,3.83336 0,2.58433 2.9594,14.00646 3.8761,14.95714 0.4007,0.41397 15.6685,2.27546 33.9287,4.13576 18.2638,1.86026 33.4271,3.60433 33.6979,3.87551 0.7657,0.76535 16.5437,-0.20885 30.3408,-1.87379 z"
|
||||
/>
|
||||
<path
|
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style={{ fill: 'none', stroke: '#000000', strokeWidth: 2, strokeLinecap: 'butt', strokeLinejoin: 'miter' }}
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d="m 699.36133,622.5332 v 160.30078 z m 1047.79487,83.25391 -0.023,76.82812 z"
|
||||
/>
|
||||
<path
|
||||
style={{
|
||||
fill: 'none',
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stroke: '#000000',
|
||||
strokeWidth: 2,
|
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strokeLinecap: 'butt',
|
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strokeLinejoin: 'miter',
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strokeDasharray: '2, 2',
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strokeDashoffset: 0,
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}}
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d="m 1747.1562,623.05078 v 83.23047 z m 653.1368,99.8086 v 43.08593 z"
|
||||
/>
|
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<path
|
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style={{ fill: 'none', stroke: '#000000', strokeWidth: 2, strokeLinecap: 'butt', strokeLinejoin: 'miter' }}
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d="M 3410.1875,600.50195 V 713.67188 Z M 2400.248,623.01367 v 99.26367 z m 0,142.40625 v 17.8418 z"
|
||||
/>
|
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<path
|
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style={{ fill: 'none', stroke: '#000000', strokeWidth: 2, strokeLinecap: 'butt', strokeLinejoin: 'miter' }}
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|
||||
/>
|
||||
<path
|
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style={{ fill: 'none', stroke: '#000000', strokeWidth: 2, strokeLinecap: 'butt', strokeLinejoin: 'round' }}
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d="m 365.87116,407.31944 -0.0244,215.69469 H 1641.4871 2916.6755 l 132.9514,-2.4633 132.9514,-2.46329 147.9234,-11.43029 147.9235,-11.43029 1.0235,-90.7622 1.0235,-90.7622 -83.301,-4.34855 -83.301,-4.34856"
|
||||
/>
|
||||
<path
|
||||
style={{ fill: 'none', stroke: '#000000', strokeWidth: 2, strokeLinecap: 'butt', strokeLinejoin: 'round' }}
|
||||
d="m 118.53125,572 h 128.07224 v 29.04076 h 119.14749"
|
||||
/>
|
||||
</g>
|
||||
<svg viewBox="0 0 4002 780" version="1.1" xmlns="http://www.w3.org/2000/svg" className="mb-4">
|
||||
<path
|
||||
style={{
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fill: 'none',
|
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strokeWidth: 4,
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strokeLinecap: 'butt',
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strokeLinejoin: 'miter',
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}}
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className={styles['stroke-zinc-600']}
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d="m 1748.2487,624.45529 v 83.5816 z m 653.1368,98.40409 v 43.08593 z"
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transform="matrix(1.0068517,0,0,1.0069072,-24.265193,-12.003831)"
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/>
|
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<path
|
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style={{
|
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fill: 'none',
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stroke: 'white',
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strokeWidth: 4,
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strokeLinecap: 'butt',
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strokeLinejoin: 'round',
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}}
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|
||||
transform="matrix(1.0068517,0,0,1.0069072,-24.265193,-12.003831)"
|
||||
/>
|
||||
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="725.61609" y="591.34473" textAnchor="middle" id="upper1">
|
||||
{upper1}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="725.61609" y="591.34473" textAnchor="middle">
|
||||
<tspan className={previewClass}>{upper1}</tspan>
|
||||
{upper1max && <tspan>/{upper1max}</tspan>}
|
||||
</text>
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="1509.024" y="591.34473" textAnchor="middle" id="upper2">
|
||||
{upper2}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1509.024" y="591.34473" textAnchor="middle">
|
||||
<tspan className={previewClass}>{upper2}</tspan>
|
||||
{upper2max && <tspan>/{upper2max}</tspan>}
|
||||
</text>
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="2292.3511" y="591.34473" textAnchor="middle" id="upper3">
|
||||
{upper3}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="2292.3511" y="591.34473" textAnchor="middle">
|
||||
<tspan className={previewClass}>{upper3}</tspan>
|
||||
{upper3max && <tspan>/{upper3max}</tspan>}
|
||||
</text>
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="3075.8955" y="591.34473" textAnchor="middle" id="upper4">
|
||||
{upper4}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="3075.8955" y="591.34473" textAnchor="middle">
|
||||
<tspan className={previewClass}>{upper4}</tspan>
|
||||
{upper4max && <tspan>/{upper4max}</tspan>}
|
||||
</text>
|
||||
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="1197.6641" y="754.35504" textAnchor="middle" id="lower1">
|
||||
{lower1}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1197.6641" y="754.35504" textAnchor="middle">
|
||||
<tspan className={previewClass}>{lower1}</tspan>
|
||||
</text>
|
||||
<text style={{ fill: '#000000', fontSize: '160px' }} x="2891.1475" y="754.35504" textAnchor="middle" id="lower2">
|
||||
{lower2}
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="2891.1475" y="754.35504" textAnchor="middle">
|
||||
<tspan className={previewClass}>{lower2}</tspan>
|
||||
</text>
|
||||
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="0" y="280.10175">
|
||||
{type === 'F' ? 'Pilots:' : 'Pilots & FAs:'}
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1476.2501" y="280.10175" textAnchor="end">
|
||||
<tspan className={previewClass}>{crew}</tspan>
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="0" y="130.625">
|
||||
OEW:
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1476.2501" y="130.625" textAnchor="end">
|
||||
{OEW}
|
||||
</text>
|
||||
|
||||
<text style={{ fill: 'white', fontSize: '100px' }} x="4002" y="778.24402" textAnchor="end">
|
||||
<tspan style={{ fontSize: '70px' }}>all in </tspan>
|
||||
<tspan>{unit}</tspan>
|
||||
</text>
|
||||
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="142.15625">
|
||||
TOCG:
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="142.15625">
|
||||
<tspan className={TOCGClass}>{CGs[2]}</tspan>
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="288.875">
|
||||
ZFWCG:
|
||||
</text>
|
||||
<text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="288.875">
|
||||
<tspan className={ZFWCGClass}>{CGs[0]}</tspan>
|
||||
</text>
|
||||
|
||||
<path
|
||||
style={{
|
||||
fill: 'none',
|
||||
stroke: 'white',
|
||||
strokeWidth: 8,
|
||||
strokeLinecap: 'butt',
|
||||
strokeLinejoin: 'round',
|
||||
opacity: isER ? 1 : 0,
|
||||
}}
|
||||
d="m 3616.1269,203.67131 -115.4682,116.32951 h 76.6132 l 13.6484,-13.75016 h -61.1499 l 42.8836,-43.20365 h 61.1499 l 13.6485,-13.75016 h -61.1499 l 31.6393,-31.87538 h 61.1499 l 13.6484,-13.75016 z m 101.1357,0 -115.4682,116.32951 h 15.4631 l 45.9082,-46.25055 h 21.7891 l -7.0158,46.25055 h 20.0709 l 6.7491,-50.85999 c 10.2365,-2.8646 20.2552,-7.10948 30.0559,-12.73452 9.8522,-5.67714 18.9402,-12.70852 27.2636,-21.09401 6.1521,-6.19797 10.0211,-11.30222 11.6068,-15.31268 1.6896,-4.06255 1.7441,-7.42197 0.1635,-10.07824 -1.4223,-2.34378 -4.0367,-3.95839 -7.8438,-4.84382 -3.7552,-0.93749 -9.1472,-1.40626 -16.176,-1.40625 z m 2.2801,13.2814 h 18.1967 c 4.165,0 7.4735,0.31252 9.9248,0.93751 2.5032,0.57292 4.1244,1.61462 4.8641,3.12503 0.9495,1.77087 0.7045,3.9584 -0.735,6.56258 -1.3356,2.55212 -3.6579,5.49487 -6.9666,8.82824 -4.3426,4.37505 -8.5084,7.9949 -12.4972,10.8595 -3.8849,2.81253 -8.0847,5.31258 -12.5989,7.50009 -4.8776,2.34378 -9.5781,3.95838 -14.1015,4.84381 -4.4716,0.83333 -9.1546,1.25002 -14.0487,1.25002 h -15.6194 z"
|
||||
/>
|
||||
</svg>
|
||||
);
|
||||
};
|
||||
|
||||
@@ -0,0 +1,221 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { WASMDataF } from '../../types/WASMData';
|
||||
import { CoherentCallStationEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface StationEntryProps {
|
||||
WASMData: WASMDataF;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||
const [upper1, setUpper1] = useState(WASMData.targetPayload.upper1);
|
||||
const [upper2, setUpper2] = useState(WASMData.targetPayload.upper2);
|
||||
const [upper3, setUpper3] = useState(WASMData.targetPayload.upper3);
|
||||
const [upper4, setUpper4] = useState(WASMData.targetPayload.upper4);
|
||||
const [lowerForward, setLowerForward] = useState(WASMData.targetPayload.lowerForward);
|
||||
const [lowerRear, setLowerRear] = useState(WASMData.targetPayload.lowerRear);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = () => {
|
||||
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel);
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Upper 1</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={upper1}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.upper1, setUpper1)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Upper 2</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={upper2}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.upper2, setUpper2)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Upper 3</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={upper3}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.upper3, setUpper3)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Upper 4</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={upper4}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.upper4, setUpper4)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Forward Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
topKeyboard
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={lowerForward}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.lowerForward, setLowerForward)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Aft Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
topKeyboard
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={lowerRear}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.lowerRear, setLowerRear)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!ZFWValid() || !GWValid()}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default StationEntryF;
|
||||
@@ -0,0 +1,227 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { WASMDataPax } from '../../types/WASMData';
|
||||
import { CoherentCallStationEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface StationEntryProps {
|
||||
WASMData: WASMDataPax;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const StationEntryPax: FC<StationEntryProps> = ({
|
||||
WASMData,
|
||||
loadingState,
|
||||
gsxActive,
|
||||
gsxFuelActive,
|
||||
setLoadingState,
|
||||
}) => {
|
||||
const [business1, setBusiness1] = useState(WASMData.targetPayload.business1);
|
||||
const [business2, setBusiness2] = useState(WASMData.targetPayload.business2);
|
||||
const [economy1, setEconomy1] = useState(WASMData.targetPayload.economy1);
|
||||
const [economy2, setEconomy2] = useState(WASMData.targetPayload.economy2);
|
||||
const [forwardCargo, setForwardCargo] = useState(WASMData.targetPayload.forwardCargo);
|
||||
const [rearCargo, setRearCargo] = useState(WASMData.targetPayload.rearCargo);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = () => {
|
||||
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel);
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Business</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={business1}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.business1, setBusiness1)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Premium Economy</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={business2}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.business2, setBusiness2)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Forward Economy</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={economy1}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.economy1, setEconomy1)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Aft Economy</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={economy2}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.economy2, setEconomy2)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Forward Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
topKeyboard
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={forwardCargo}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.forwardCargo, setForwardCargo)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Aft Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
topKeyboard
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={rearCargo}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.rearCargo, setRearCargo)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!ZFWValid() || !GWValid()}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default StationEntryPax;
|
||||
@@ -0,0 +1,27 @@
|
||||
import { FC } from 'react';
|
||||
|
||||
interface TabbarProps {
|
||||
tabs: string[];
|
||||
selectedTab: number;
|
||||
setSelectedTab: (tab: number) => void;
|
||||
}
|
||||
|
||||
const Tabbar: FC<TabbarProps> = ({ tabs, selectedTab, setSelectedTab }) => {
|
||||
return (
|
||||
<ul className="mb-4 flex list-none flex-row flex-wrap border-b-0 pl-0">
|
||||
{tabs.map((tab, i) => (
|
||||
<li key={`${tab}-${i}`}>
|
||||
<button
|
||||
key={i}
|
||||
className={`${selectedTab === i ? 'text-white underline' : 'text-neutral-500'} my-2 block border-x-0 border-b-2 border-t-0 border-slate-100 bg-zinc-900 px-7 text-sm font-medium uppercase`}
|
||||
onClick={() => setSelectedTab(i)}
|
||||
>
|
||||
{tab}
|
||||
</button>
|
||||
</li>
|
||||
))}
|
||||
</ul>
|
||||
);
|
||||
};
|
||||
|
||||
export default Tabbar;
|
||||
@@ -0,0 +1,51 @@
|
||||
interface ToggleComponentProps<T> {
|
||||
optionName: string;
|
||||
value: T;
|
||||
leftLabel: {
|
||||
value: T;
|
||||
label?: string;
|
||||
};
|
||||
rightLabel: {
|
||||
value: T;
|
||||
label?: string;
|
||||
};
|
||||
backgroundColor: string;
|
||||
disabled?: boolean;
|
||||
setValue: (value: T) => void;
|
||||
}
|
||||
|
||||
const ToggleComponentKH = <T,>({
|
||||
optionName,
|
||||
value,
|
||||
leftLabel,
|
||||
rightLabel,
|
||||
backgroundColor,
|
||||
disabled,
|
||||
setValue,
|
||||
}: ToggleComponentProps<T>) => {
|
||||
return (
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<span>{optionName}</span>
|
||||
<div className="inline-flex w-1/2 rounded-md shadow-sm">
|
||||
<button
|
||||
type="button"
|
||||
className={`${value === leftLabel.value ? 'bg-green-700' : backgroundColor} w-1/2 rounded-l-lg border border-white px-4 py-2 text-white disabled:pointer-events-none disabled:opacity-50`}
|
||||
onClick={() => setValue(leftLabel.value)}
|
||||
disabled={disabled}
|
||||
>
|
||||
{leftLabel.label || 'Enabled'}
|
||||
</button>
|
||||
<button
|
||||
type="button"
|
||||
className={`${value === rightLabel.value ? 'bg-green-700' : backgroundColor} w-1/2 rounded-r-md border border-white px-4 py-2 text-white disabled:pointer-events-none disabled:opacity-50`}
|
||||
onClick={() => setValue(rightLabel.value)}
|
||||
disabled={disabled}
|
||||
>
|
||||
{rightLabel.label || 'Disabled'}
|
||||
</button>
|
||||
</div>
|
||||
</div>
|
||||
);
|
||||
};
|
||||
|
||||
export default ToggleComponentKH;
|
||||
@@ -0,0 +1,206 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { WASMDataF } from '../../types/WASMData';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import CGSelect from '../CGSelect/CGSelect';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface ZFWEntryProps {
|
||||
WASMData: WASMDataF;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
const handleInputZFW = (input: string) => {
|
||||
if (!input) {
|
||||
setZFWTarget(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted <= 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
|
||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||
else setZFWTarget(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const handleBlurZFW = (input: string) => {
|
||||
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
||||
|
||||
if (!input) {
|
||||
setZFWTarget(minZFW);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < minZFW) setZFWTarget(minZFW);
|
||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||
else setZFWTarget(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = () => {
|
||||
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Target ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={ZFWTarget}
|
||||
onChange={(value) => handleInputZFW(value)}
|
||||
onBlur={(value) => handleBlurZFW(value)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
|
||||
</label>
|
||||
<CGSelect
|
||||
minCG={WASMData.limits.minCG}
|
||||
maxCG={WASMData.limits.maxCG}
|
||||
value={CGTarget}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
increase={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev + 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
decrease={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev - 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!GWValid()}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default ZFWEntryF;
|
||||
@@ -0,0 +1,206 @@
|
||||
import { FC, useEffect, useState } from 'react';
|
||||
import { WASMDataPax } from '../../types/WASMData';
|
||||
import { LoadingState } from '../../types/general';
|
||||
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||
import CGSelect from '../CGSelect/CGSelect';
|
||||
import ActionBar from '../actionbar/ActionBar';
|
||||
import Input from '../input/Input';
|
||||
|
||||
interface ZFWEntryProps {
|
||||
WASMData: WASMDataPax;
|
||||
loadingState: LoadingState;
|
||||
gsxActive: boolean;
|
||||
gsxFuelActive: boolean;
|
||||
setLoadingState: (newState: LoadingState) => void;
|
||||
}
|
||||
|
||||
const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
||||
|
||||
const ZFW = () => {
|
||||
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
||||
|
||||
return Math.round(WASMData.livePayload.total);
|
||||
};
|
||||
const ZFWValid = () => {
|
||||
return ZFW() <= WASMData.limits.maxZFW;
|
||||
};
|
||||
const GW = () => {
|
||||
return fuel + ZFW();
|
||||
};
|
||||
const GWValid = () => {
|
||||
return GW() <= WASMData.limits.maxTOW;
|
||||
};
|
||||
|
||||
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
|
||||
if (!input) {
|
||||
setter(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setter(0);
|
||||
else if (converted > maxValue) setter(maxValue);
|
||||
else setter(converted);
|
||||
}
|
||||
};
|
||||
const handleInputZFW = (input: string) => {
|
||||
if (!input) {
|
||||
setZFWTarget(0);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
|
||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||
else setZFWTarget(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const handleBlurZFW = (input: string) => {
|
||||
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
||||
|
||||
if (!input) {
|
||||
setZFWTarget(minZFW);
|
||||
return;
|
||||
}
|
||||
|
||||
const converted = parseInt(input);
|
||||
if (converted) {
|
||||
if (converted < minZFW) setZFWTarget(minZFW);
|
||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||
else setZFWTarget(converted);
|
||||
}
|
||||
};
|
||||
|
||||
const updateData = () => {
|
||||
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
|
||||
};
|
||||
|
||||
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
|
||||
useEffect(
|
||||
() =>
|
||||
setFuel((prev) => {
|
||||
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
|
||||
return prev;
|
||||
}),
|
||||
[WASMData.userData.isER]
|
||||
);
|
||||
|
||||
return (
|
||||
<>
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||
value={fuel}
|
||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>Target ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
|
||||
<Input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
|
||||
value={ZFWTarget}
|
||||
onChange={(value) => handleInputZFW(value)}
|
||||
onBlur={(value) => handleBlurZFW(value)}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
|
||||
</label>
|
||||
<CGSelect
|
||||
minCG={WASMData.limits.minCG}
|
||||
maxCG={WASMData.limits.maxCG}
|
||||
value={CGTarget}
|
||||
disabled={loadingState !== 'preview' || gsxActive}
|
||||
increase={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev + 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
decrease={() =>
|
||||
setCGTarget((prev) => {
|
||||
const _new = prev - 0.1;
|
||||
return _new;
|
||||
})
|
||||
}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
|
||||
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={ZFW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
|
||||
<div className="flex w-full items-center justify-between text-xs">
|
||||
<label>
|
||||
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
|
||||
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
|
||||
</label>
|
||||
<input
|
||||
type="text"
|
||||
placeholder=""
|
||||
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
|
||||
disabled
|
||||
value={GW()}
|
||||
/>
|
||||
</div>
|
||||
</div>
|
||||
</div>
|
||||
|
||||
<ActionBar
|
||||
loadingState={loadingState}
|
||||
loadDisabled={!GWValid()}
|
||||
GSXSync={WASMData.options.GSXSync}
|
||||
load={() => {
|
||||
setLoadingState('loaded');
|
||||
|
||||
loadAircraft();
|
||||
}}
|
||||
unload={() => {
|
||||
setLoadingState('preview');
|
||||
|
||||
unloadAircraft();
|
||||
}}
|
||||
/>
|
||||
</>
|
||||
);
|
||||
};
|
||||
|
||||
export default ZFWEntryPax;
|
||||
@@ -1,53 +0,0 @@
|
||||
export interface PayloadFreight {
|
||||
pilot: number;
|
||||
firstOfficer: number;
|
||||
engineer: number;
|
||||
upper1Left: number;
|
||||
upper1Right: number;
|
||||
upper2Left: number;
|
||||
upper2Right: number;
|
||||
upper3Left: number;
|
||||
upper3Right: number;
|
||||
upper4Left: number;
|
||||
upper4Right: number;
|
||||
lowerForward: number;
|
||||
lowerRear: number;
|
||||
leftAuxF: number;
|
||||
rightAuxF: number;
|
||||
}
|
||||
|
||||
// TODO: Extract from CFG at runtime.
|
||||
export const ArmsFreight = {
|
||||
pilot: 984,
|
||||
firstOfficer: 984,
|
||||
engineer: 960,
|
||||
upper1Left: 660,
|
||||
upper1Right: 660,
|
||||
upper2Left: 240,
|
||||
upper2Right: 240,
|
||||
upper3Left: -240,
|
||||
upper3Right: -240,
|
||||
upper4Left: -600,
|
||||
upper4Right: -600,
|
||||
lowerForward: 360,
|
||||
lowerRear: -360,
|
||||
leftAuxF: 60,
|
||||
rightAuxF: 60,
|
||||
};
|
||||
|
||||
//PMC pallet
|
||||
export const maxUpperStationWeight = {
|
||||
kg: (26 / 8) * 6804,
|
||||
lbs: (26 / 8) * 15000,
|
||||
};
|
||||
|
||||
export const baseWeightFreight = {
|
||||
pilot: {
|
||||
lbs: 190,
|
||||
kg: 86,
|
||||
},
|
||||
firstOfficer: {
|
||||
lbs: 190,
|
||||
kg: 86,
|
||||
},
|
||||
};
|
||||
@@ -1,82 +0,0 @@
|
||||
export interface PayloadPax {
|
||||
pilot: number;
|
||||
firstOfficer: number;
|
||||
engineer: number;
|
||||
cabinCrewFront: number;
|
||||
business1Left: number;
|
||||
business1Center: number;
|
||||
business1Right: number;
|
||||
business2Left: number;
|
||||
business2Center: number;
|
||||
business2Right: number;
|
||||
economy1Left: number;
|
||||
economy1Center: number;
|
||||
economy1Right: number;
|
||||
economy2Left: number;
|
||||
economy2Center: number;
|
||||
economy2Right: number;
|
||||
cabinCrewRear: number;
|
||||
forwardCargo: number;
|
||||
rearCargo: number;
|
||||
leftAuxPax: number;
|
||||
rightAuxPax: number;
|
||||
}
|
||||
|
||||
// TODO: Extract from CFG at runtime.
|
||||
export const ArmsPax = {
|
||||
pilot: 984,
|
||||
firstOfficer: 984,
|
||||
engineer: 960,
|
||||
cabinCrewFront: 792,
|
||||
business1Left: 540,
|
||||
business1Center: 540,
|
||||
business1Right: 540,
|
||||
business2Left: 300,
|
||||
business2Center: 300,
|
||||
business2Right: 300,
|
||||
economy1Left: -240,
|
||||
economy1Center: -240,
|
||||
economy1Right: -240,
|
||||
economy2Left: -600,
|
||||
economy2Center: -600,
|
||||
economy2Right: -600,
|
||||
cabinCrewRear: -660,
|
||||
forwardCargo: 360,
|
||||
rearCargo: -360,
|
||||
leftAuxPax: 60,
|
||||
rightAuxPax: 60,
|
||||
};
|
||||
|
||||
// TODO: Make user adjustable
|
||||
export const paxWeight = {
|
||||
kg: 86,
|
||||
lbs: 190,
|
||||
};
|
||||
|
||||
export const maxBusiness1StationCount = 30; // all Business rows
|
||||
export const maxBusiness2StationCount = 45; // first 5 "Economy" as "Premium Economy"
|
||||
export const maxEconomy1StationCount = 86; // up to and including the 5 seat Economy row
|
||||
export const maxEconomy2StationCount = 137; // rest of Economy rows
|
||||
|
||||
export const baseWeightPax = {
|
||||
pilot: {
|
||||
lbs: 190,
|
||||
kg: 86,
|
||||
},
|
||||
firstOfficer: {
|
||||
lbs: 190,
|
||||
kg: 86,
|
||||
},
|
||||
engineer: {
|
||||
lbs: 190,
|
||||
kg: 86,
|
||||
},
|
||||
cabinCrewFront: {
|
||||
lbs: 380,
|
||||
kg: 172,
|
||||
},
|
||||
cabinCrewRear: {
|
||||
lbs: 950,
|
||||
kg: 430,
|
||||
},
|
||||
};
|
||||
@@ -1,57 +0,0 @@
|
||||
export interface Fuel {
|
||||
main1: number;
|
||||
main3: number;
|
||||
main2: number;
|
||||
upperAux: number;
|
||||
lowerAux: number;
|
||||
main1Tip: number;
|
||||
main3Tip: number;
|
||||
tail: number;
|
||||
forwardAux1: number;
|
||||
forwardAux2: number;
|
||||
}
|
||||
|
||||
// TODO: Extract from CFG at runtime.
|
||||
export const EmptyArm = -159.6;
|
||||
|
||||
// TODO: Extract from CFG at runtime.
|
||||
export const ArmsFuel = {
|
||||
main1: -240,
|
||||
main3: -240,
|
||||
main2: 120,
|
||||
upperAux: 0,
|
||||
lowerAux: 0,
|
||||
main1Tip: -468,
|
||||
main3Tip: -468,
|
||||
tail: -840,
|
||||
forwardAux1: 60,
|
||||
forwardAux2: 60,
|
||||
};
|
||||
|
||||
// TODO: Extract following four from CFG at runtime
|
||||
const rootChord = 34.68;
|
||||
const wingSpan = 170.5;
|
||||
const wingArea = 3648;
|
||||
const quarterMAC = -165; //aero_center
|
||||
|
||||
const tipChord = (2 * wingArea) / wingSpan - rootChord;
|
||||
const taperRatio = tipChord / rootChord;
|
||||
|
||||
const MAC = (2 / 3) * rootChord * ((1 + taperRatio + taperRatio ** 2) / (1 + taperRatio)) * 12;
|
||||
const LEMAC = quarterMAC + (1 / 4) * MAC;
|
||||
|
||||
export const toPercentMAC = (positionInInches: number) => {
|
||||
return Math.abs(((positionInInches - LEMAC) / MAC) * 100);
|
||||
};
|
||||
|
||||
//PMC pallet due to 104in door
|
||||
export const maxForwardLowerStationWeight = {
|
||||
kg: 6 * 6804,
|
||||
lbs: 6 * 15000,
|
||||
};
|
||||
|
||||
//LD3s due to 70in door
|
||||
export const maxRearLowerStationWeight = {
|
||||
kg: 14 * 1588,
|
||||
lbs: 14 * 3500,
|
||||
};
|
||||
@@ -1,6 +1,3 @@
|
||||
export const COMMANDS = 'KHOFMANN_PDF_READER_COMMANDS';
|
||||
export const DATA = 'KHOFMANN_PDF_READER_DATA';
|
||||
export const LIST = 'LIST';
|
||||
export const LOAD = 'LOAD';
|
||||
export const SAVE = 'SAVE';
|
||||
export const MAX_LIST = 10;
|
||||
export const COHERENT_COMM_BUS_WASM_CALL = 'COMM_BUS_WASM_CALLBACK';
|
||||
|
||||
export const CG_ADJUST = 0.05;
|
||||
|
||||
@@ -1,7 +0,0 @@
|
||||
@font-face {
|
||||
font-family: 'Roboto';
|
||||
font-style: normal;
|
||||
font-display: swap;
|
||||
font-weight: 300;
|
||||
src: url(assets/fonts/Roboto-Light.ttf) format('truetype');
|
||||
}
|
||||
@@ -1,7 +0,0 @@
|
||||
@font-face {
|
||||
font-family: 'Roboto';
|
||||
font-style: normal;
|
||||
font-display: swap;
|
||||
font-weight: 400;
|
||||
src: url(assets/fonts/Roboto-Regular.ttf) format('truetype');
|
||||
}
|
||||
@@ -1,7 +0,0 @@
|
||||
@font-face {
|
||||
font-family: 'Roboto';
|
||||
font-style: normal;
|
||||
font-display: swap;
|
||||
font-weight: 500;
|
||||
src: url(assets/fonts/Roboto-Medium.ttf) format('truetype');
|
||||
}
|
||||
@@ -1,7 +0,0 @@
|
||||
@font-face {
|
||||
font-family: 'Roboto';
|
||||
font-style: normal;
|
||||
font-display: swap;
|
||||
font-weight: 700;
|
||||
src: url(assets/fonts/Roboto-Bold.ttf) format('truetype');
|
||||
}
|
||||
@@ -1,41 +0,0 @@
|
||||
<!doctype html>
|
||||
<html>
|
||||
<!-- prettier-ignore -->
|
||||
<head>
|
||||
<title></title>
|
||||
<meta charset="utf-8" />
|
||||
<meta name="viewport" content="width=device-width, initial-scale=1.0" />
|
||||
|
||||
<link rel="stylesheet" href="/SCSS/common.css" />
|
||||
<link rel="stylesheet" href="index.css" />
|
||||
|
||||
<script type="text/javascript" src="/JS/coherent.js"></script>
|
||||
<script type="text/javascript" src="/JS/common.js"></script>
|
||||
<script type="text/javascript" src="/Pages/VCockpit/Instruments/Shared/BaseInstrument.js"></script>
|
||||
<script type="text/javascript" src="/JS/dataStorage.js"></script>
|
||||
<script type="text/javascript" src="/JS/buttons.js"></script>
|
||||
<script type="text/javascript" src="/JS/Services/ToolBarPanels.js"></script>
|
||||
<script type="text/javascript" src="/JS/simvar.js"></script>
|
||||
|
||||
<link rel="import" href="/templates/NewPushButton/NewPushButton.html" />
|
||||
<link rel="import" href="/templates/ingameUi/ingameUi.html" />
|
||||
<link rel="import" href="/templates/ingameUiHeader/ingameUiHeader.html" />
|
||||
<link rel="import" href="/templates/virtualScroll/virtualScroll.html" />
|
||||
</head>
|
||||
<body class="border-box">
|
||||
<tfdidesign-md11-load-manager-panel>
|
||||
<ingame-ui
|
||||
id="tfdidesign-md11-load-manager"
|
||||
panel-id="TFDIDESIGN_MD11_LOAD_MANAGER_PANEL"
|
||||
title="TFDi Design MD-11 Load Manager"
|
||||
class="ingameUiFrame panelInvisible"
|
||||
content-fit="true"
|
||||
>
|
||||
<virtual-scroll direction="y">
|
||||
<div id="react" style="display: flex"></div>
|
||||
</virtual-scroll>
|
||||
</ingame-ui>
|
||||
</tfdidesign-md11-load-manager-panel>
|
||||
<script src="index.js" type="text/javascript"></script>
|
||||
</body>
|
||||
</html>
|
||||
@@ -1,30 +0,0 @@
|
||||
import { createElement } from 'react';
|
||||
import { createRoot } from 'react-dom/client';
|
||||
import App from './App';
|
||||
|
||||
class TFDiDesignMD11LoadManagerPanel extends TemplateElement {
|
||||
dataListener?: ViewListener.ViewListener;
|
||||
|
||||
constructor() {
|
||||
super();
|
||||
}
|
||||
|
||||
connectedCallback() {
|
||||
super.connectedCallback();
|
||||
|
||||
this.dataListener = RegisterViewListener('JS_LISTENER_COMM_BUS');
|
||||
|
||||
const container = document.getElementById('react');
|
||||
if (container) {
|
||||
const root = createRoot(container);
|
||||
root.render(createElement(App, { dataListener: this.dataListener }));
|
||||
}
|
||||
}
|
||||
|
||||
disconnectedCallback() {
|
||||
super.disconnectedCallback();
|
||||
}
|
||||
}
|
||||
|
||||
window.customElements.define('tfdidesign-md11-load-manager-panel', TFDiDesignMD11LoadManagerPanel);
|
||||
checkAutoload();
|
||||
@@ -0,0 +1,115 @@
|
||||
interface WASMData {
|
||||
GSX: GSX;
|
||||
userData: UserData;
|
||||
options: Options;
|
||||
sbPlanned: {
|
||||
ZFW: number;
|
||||
GW: number;
|
||||
fuel: number;
|
||||
};
|
||||
loaded: boolean;
|
||||
}
|
||||
|
||||
export interface WASMDataPax extends WASMData {
|
||||
livePayload: LivePayloadPax;
|
||||
targetPayload: TargetPayloadPax;
|
||||
limits: LimitsPax;
|
||||
}
|
||||
|
||||
export interface WASMDataF extends WASMData {
|
||||
livePayload: LivePayloadF;
|
||||
targetPayload: TargetPayloadF;
|
||||
limits: LimitsF;
|
||||
}
|
||||
|
||||
interface TargetPayload {
|
||||
CGTarget: number;
|
||||
ZFWCG: number;
|
||||
TOCG: number;
|
||||
total: number;
|
||||
fuel: number;
|
||||
}
|
||||
|
||||
interface TargetPayloadPax extends TargetPayload {
|
||||
empty: number;
|
||||
crew: number;
|
||||
business1: number;
|
||||
business2: number;
|
||||
economy1: number;
|
||||
economy2: number;
|
||||
forwardCargo: number;
|
||||
rearCargo: number;
|
||||
}
|
||||
|
||||
type LivePayloadPax = TargetPayloadPax;
|
||||
|
||||
interface TargetPayloadF extends TargetPayload {
|
||||
empty: number;
|
||||
crew: number;
|
||||
upper1: number;
|
||||
upper2: number;
|
||||
upper3: number;
|
||||
upper4: number;
|
||||
lowerForward: number;
|
||||
lowerRear: number;
|
||||
}
|
||||
|
||||
type LivePayloadF = TargetPayloadF;
|
||||
|
||||
interface GSX {
|
||||
couatlStarted: boolean;
|
||||
loadingState: GSXLoadingState;
|
||||
fuelingState: GSXFuelingState;
|
||||
}
|
||||
|
||||
interface Limits {
|
||||
minCG: number;
|
||||
maxCG: number;
|
||||
maxFuel: number;
|
||||
maxTOW: number;
|
||||
maxZFW: number;
|
||||
minZFW: number;
|
||||
}
|
||||
|
||||
interface LimitsPax extends Limits {
|
||||
business1: number;
|
||||
business2: number;
|
||||
economy1: number;
|
||||
economy2: number;
|
||||
forwardCargo: number;
|
||||
rearCargo: number;
|
||||
}
|
||||
|
||||
interface LimitsF extends Limits {
|
||||
upper1: number;
|
||||
upper2: number;
|
||||
upper3: number;
|
||||
upper4: number;
|
||||
lowerForward: number;
|
||||
lowerRear: number;
|
||||
}
|
||||
|
||||
interface UserData {
|
||||
isCargo: boolean;
|
||||
isER: boolean;
|
||||
isImperial: boolean;
|
||||
}
|
||||
|
||||
interface Options {
|
||||
GSXSync: boolean;
|
||||
paxWeight: number;
|
||||
bagWeight: number;
|
||||
}
|
||||
|
||||
export enum GSXLoadingState {
|
||||
IDLE = 0,
|
||||
BOARDING = 1,
|
||||
BOARDED = 2,
|
||||
DEBOARDING = 3,
|
||||
DEBOARDED = 4,
|
||||
}
|
||||
|
||||
export enum GSXFuelingState {
|
||||
IDLE = 0,
|
||||
FUELING = 1,
|
||||
}
|
||||
@@ -0,0 +1,29 @@
|
||||
export type LoadingState = 'preview' | 'loaded';
|
||||
|
||||
export interface SimBrief {
|
||||
plannedZFW: number;
|
||||
plannedGW: number;
|
||||
pax: number;
|
||||
cargo: number;
|
||||
fuel: number;
|
||||
}
|
||||
|
||||
export enum CallMode {
|
||||
SB_SET = 0,
|
||||
ZFW_SET = 1,
|
||||
STATION_SET = 2,
|
||||
LOAD_SET = 3,
|
||||
UNLOAD_SET = 4,
|
||||
OPTIONS_SET = 5,
|
||||
GSX_RESET = 6,
|
||||
}
|
||||
|
||||
export enum CommBusCall {
|
||||
TFDI_SIMBRIEF_USERNAME = 'requestSimBriefUsername',
|
||||
}
|
||||
|
||||
export enum CommBusEvent {
|
||||
TFDI_SIMBRIEF_USERNAME = 'receiveSimBriefUsername',
|
||||
LIVE_DATA = 'khofmann_tfdi_md-11_load_manager_live_data',
|
||||
UPDATE_TARGET = 'khofmann_tfdi_md-11_load_manager_update_target',
|
||||
}
|
||||
-10
@@ -1,10 +0,0 @@
|
||||
import '@mui/material';
|
||||
|
||||
declare module '@mui/material/styles' {
|
||||
interface Theme {
|
||||
screenHeight: number;
|
||||
}
|
||||
interface ThemeOptions {
|
||||
screenHeight: number;
|
||||
}
|
||||
}
|
||||
@@ -1,11 +0,0 @@
|
||||
import { CSSProperties, DOMAttributes, ReactNode } from 'react';
|
||||
|
||||
type CustomElement<T> = Partial<T & DOMAttributes<T> & { children: ReactNode }>;
|
||||
|
||||
declare global {
|
||||
namespace JSX {
|
||||
interface IntrinsicElements {
|
||||
['virtual-scroll']: CustomElement<{ class?: string; direction: 'x' | 'y'; style?: CSSProperties }>;
|
||||
}
|
||||
}
|
||||
}
|
||||
@@ -0,0 +1,41 @@
|
||||
import { SimBrief } from '../types/general';
|
||||
|
||||
type Plan = {
|
||||
params: {
|
||||
units: 'kgs' | 'lbs';
|
||||
};
|
||||
weights: {
|
||||
est_zfw: number;
|
||||
est_ramp: number;
|
||||
pax_count_actual: number;
|
||||
freight_added: number;
|
||||
};
|
||||
fuel: {
|
||||
plan_ramp: number;
|
||||
};
|
||||
};
|
||||
|
||||
export const ImportFlightPlanKH = (
|
||||
plan: Plan,
|
||||
maxZFW: number,
|
||||
maxTOW: number,
|
||||
maxFuel: number,
|
||||
isImperial: boolean
|
||||
) => {
|
||||
if (!plan) return { type: 'error', message: 'Empty plan' };
|
||||
|
||||
let convFactor = 1;
|
||||
if (plan.params.units === 'kgs' && isImperial) convFactor = 2.20462262185;
|
||||
if (plan.params.units === 'lbs' && !isImperial) convFactor = 1 / 2.20462262185;
|
||||
|
||||
return {
|
||||
type: 'data',
|
||||
message: {
|
||||
plannedZFW: Math.min(maxZFW, Math.round(plan.weights.est_zfw * convFactor)),
|
||||
plannedGW: Math.min(maxTOW, Math.round(plan.weights.est_ramp * convFactor)),
|
||||
pax: plan.weights.pax_count_actual,
|
||||
cargo: Math.round(plan.weights.freight_added * convFactor),
|
||||
fuel: Math.min(maxFuel, Math.round(plan.fuel.plan_ramp * convFactor)),
|
||||
} as SimBrief,
|
||||
};
|
||||
};
|
||||
@@ -0,0 +1,143 @@
|
||||
import { COHERENT_COMM_BUS_WASM_CALL } from '../constants';
|
||||
import { CallMode, CommBusEvent, SimBrief } from '../types/general';
|
||||
|
||||
export const loadAircraft = () => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.LOAD_SET,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const unloadAircraft = () => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.UNLOAD_SET,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const inRangeOf = (value: number, target: number, tolerance: number = 10) => {
|
||||
return Math.abs(value - target) < tolerance;
|
||||
};
|
||||
|
||||
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number, fuelTarget: number) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.ZFW_SET,
|
||||
ZFWTarget: ZFWTarget,
|
||||
CGTarget: CGTarget,
|
||||
fuelTarget: fuelTarget,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallStationEntryPax = (
|
||||
business1: number,
|
||||
business2: number,
|
||||
economy1: number,
|
||||
economy2: number,
|
||||
forwardCargo: number,
|
||||
rearCargo: number,
|
||||
fuelTarget: number
|
||||
) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.STATION_SET,
|
||||
business1,
|
||||
business2,
|
||||
economy1,
|
||||
economy2,
|
||||
forwardCargo,
|
||||
rearCargo,
|
||||
fuelTarget,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallStationEntryF = (
|
||||
upper1: number,
|
||||
upper2: number,
|
||||
upper3: number,
|
||||
upper4: number,
|
||||
lowerForward: number,
|
||||
lowerRear: number,
|
||||
fuelTarget: number
|
||||
) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.STATION_SET,
|
||||
upper1,
|
||||
upper2,
|
||||
upper3,
|
||||
upper4,
|
||||
lowerForward,
|
||||
lowerRear,
|
||||
fuelTarget,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallSBEntryPax = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.SB_SET,
|
||||
cargo: SBPlan?.cargo,
|
||||
numPax: SBPlan ? parseInt(SBPlan.pax as unknown as string) : undefined,
|
||||
CGTarget: CGTarget,
|
||||
plannedZFW: SBPlan?.plannedZFW,
|
||||
plannedGW: SBPlan?.plannedGW,
|
||||
fuel: fuel,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallSBEntryF = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.SB_SET,
|
||||
cargo: SBPlan?.cargo,
|
||||
CGTarget: CGTarget,
|
||||
plannedZFW: SBPlan?.plannedZFW,
|
||||
plannedGW: SBPlan?.plannedGW,
|
||||
fuel: SBPlan?.fuel,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallOptionsSet = (GSXSync?: boolean, paxWeight?: number, bagWeight?: number) => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.OPTIONS_SET,
|
||||
GSXSync,
|
||||
paxWeight,
|
||||
bagWeight,
|
||||
})
|
||||
);
|
||||
};
|
||||
|
||||
export const CoherentCallGSXReset = () => {
|
||||
Coherent.call(
|
||||
COHERENT_COMM_BUS_WASM_CALL,
|
||||
CommBusEvent.UPDATE_TARGET,
|
||||
JSON.stringify({
|
||||
mode: CallMode.GSX_RESET,
|
||||
})
|
||||
);
|
||||
};
|
||||
@@ -65,7 +65,7 @@
|
||||
// "sourceMap": true, /* Create source map files for emitted JavaScript files. */
|
||||
// "inlineSourceMap": true, /* Include sourcemap files inside the emitted JavaScript. */
|
||||
// "outFile": "./", /* Specify a file that bundles all outputs into one JavaScript file. If 'declaration' is true, also designates a file that bundles all .d.ts output. */
|
||||
"outDir": "../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel",
|
||||
// "outDir": "../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel",
|
||||
/* Specify an output folder for all emitted files. */
|
||||
// "removeComments": true, /* Disable emitting comments. */
|
||||
// "noEmit": true, /* Disable emitting files from a compilation. */
|
||||
|
||||
File diff suppressed because it is too large
Load Diff
@@ -1,17 +0,0 @@
|
||||
<SimBase.Document Type="InGamePanels" version="1,0">
|
||||
<Filename>tfdidesign-md11-load-manager.spb</Filename>
|
||||
<InGamePanels.InGamePanelDefinition
|
||||
id="TFDIDESIGN_MD11_LOAD_MANAGER_PANEL"
|
||||
Name="tfdidesign-md11-load-manager"
|
||||
url="html_UI/InGamePanels/tfdidesign-md11-load-manager-panel/index.html"
|
||||
resizeDirections="both"
|
||||
minWidth="100"
|
||||
minHeight="70"
|
||||
defaultWidth="100"
|
||||
defaultHeight="70"
|
||||
defaultTop="10"
|
||||
defaultLeft="10"
|
||||
icon="ICON_TFDIDESIGN_MD11_LOAD_MANAGER"
|
||||
buttonVisible="true">
|
||||
</InGamePanels.InGamePanelDefinition>
|
||||
</SimBase.Document>
|
||||
@@ -0,0 +1,119 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
/********************************* Headers *********************************/
|
||||
// MSFS headers
|
||||
#include <MSFS/MSFS_WindowsTypes.h>
|
||||
#include <SimConnect.h>
|
||||
// C headers
|
||||
#include <math.h>
|
||||
// C++ headers
|
||||
#include <algorithm>
|
||||
// Own headers
|
||||
#include "fuel.h"
|
||||
#include "log.h"
|
||||
#include "shared.h"
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
// PMC pallet due to 104in door
|
||||
#define MAX_UPPER_CARGO(IS_IMPERIAL) ((IS_IMPERIAL) ? (6.5 * 15000.0) : (6.5 * 6804.0))
|
||||
// Max ZFW
|
||||
#define MAX_F_ZFW(IS_IMPERIAL) ((IS_IMPERIAL) ? (451300) : (204706))
|
||||
// Arms
|
||||
#define ARM_F_UPPER1_LEFT 660
|
||||
#define ARM_F_UPPER1_RIGHT 660
|
||||
#define ARM_F_UPPER2_LEFT 240
|
||||
#define ARM_F_UPPER2_RIGHT 240
|
||||
#define ARM_F_UPPER3_LEFT -240
|
||||
#define ARM_F_UPPER3_RIGHT -240
|
||||
#define ARM_F_UPPER4_LEFT -600
|
||||
#define ARM_F_UPPER4_RIGHT -600
|
||||
|
||||
/***************************** Data structures *****************************/
|
||||
typedef struct {
|
||||
// SimConnect mapped
|
||||
double pilot;
|
||||
double firstOfficer;
|
||||
double engineer;
|
||||
double upper1Left;
|
||||
double upper1Right;
|
||||
double upper2Left;
|
||||
double upper2Right;
|
||||
double upper3Left;
|
||||
double upper3Right;
|
||||
double upper4Left;
|
||||
double upper4Right;
|
||||
double lowerForward;
|
||||
double lowerRear;
|
||||
double leftAux;
|
||||
double rightAux;
|
||||
double _ZFWCG; // DO NOT USE
|
||||
|
||||
// Additional properties
|
||||
double empty;
|
||||
double total;
|
||||
double CGTarget;
|
||||
double ZFWCG;
|
||||
double TOCG;
|
||||
struct stations {
|
||||
unsigned int upper1;
|
||||
unsigned int upper2;
|
||||
unsigned int upper3;
|
||||
unsigned int upper4;
|
||||
unsigned int total;
|
||||
} stations;
|
||||
struct sbPlanned {
|
||||
double ZFW;
|
||||
double GW;
|
||||
double fuel;
|
||||
unsigned int cargo;
|
||||
} sbPlanned;
|
||||
} fPayloadData_t;
|
||||
|
||||
typedef struct {
|
||||
// SimConnect mapped
|
||||
double pilot;
|
||||
double firstOfficer;
|
||||
double engineer;
|
||||
double upper1Left;
|
||||
double upper1Right;
|
||||
double upper2Left;
|
||||
double upper2Right;
|
||||
double upper3Left;
|
||||
double upper3Right;
|
||||
double upper4Left;
|
||||
double upper4Right;
|
||||
double lowerForward;
|
||||
double lowerRear;
|
||||
double leftAux;
|
||||
double rightAux;
|
||||
double ZFWCG;
|
||||
} fPayloadDataSet_t;
|
||||
|
||||
/******************************** Functions ********************************/
|
||||
// ZFW Entry
|
||||
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
|
||||
const UserData_t *const userData);
|
||||
// SimBrief Entry
|
||||
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned int cargo,
|
||||
const UserData_t *const userData);
|
||||
// Updates pax stations with their respective weights
|
||||
// Used internally and used for Station Entry (pax only, cargo is ste directly)
|
||||
// STATION WEIGHTS ARE NOT NORMALISED TO POUNDS
|
||||
void generatePayload(fPayloadData_t *const targetPayload);
|
||||
// Normalise to Pounds
|
||||
// For Station Entry: CALL AFTER `generatePayload`
|
||||
void normalisePayload(fPayloadData_t *const targetPayload, const bool isImperial);
|
||||
void calculateCGs(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial);
|
||||
void load(const fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
|
||||
const bool isImperial);
|
||||
void unloadF(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER);
|
||||
@@ -0,0 +1,94 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
/********************************* Headers *********************************/
|
||||
// MSFS headers
|
||||
#include <MSFS/MSFS_WindowsTypes.h>
|
||||
#include <SimConnect.h>
|
||||
// C headers
|
||||
#include <math.h>
|
||||
// C++ headers
|
||||
#include <algorithm>
|
||||
// Own headers
|
||||
#include "shared.h"
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
|
||||
// Pounds to gallons conversion
|
||||
#define LBS_PER_GAL 6.699999809
|
||||
// Fueling rate
|
||||
#define FUELING_RATE ((LBS_PER_GAL * 1000) / 60)
|
||||
// Max tank capacity gallons
|
||||
#define MAX_TANK_1_3_MAIN_GAL 5167.907
|
||||
#define MAX_TANK_1_3_TIP_GAL 874.5
|
||||
#define MAX_TANK_1_3_GAL (5167.907 + 874.5)
|
||||
#define MAX_TANK_2_GAL 9556.95
|
||||
#define MAX_UPR_AUX_GAL 12998.58
|
||||
#define MAX_LWR_AUX_GAL 1641.82
|
||||
#define MAX_TAIL_GAL 1957.779
|
||||
#define MAX_FWD_AUX_GAL 1970.8
|
||||
// Max tank capacity pounds
|
||||
#define MAX_TANK_1_3_MAIN_LBS (LBS_PER_GAL * MAX_TANK_1_3_MAIN_GAL)
|
||||
#define MAX_TANK_1_3_TIP_LBS (LBS_PER_GAL * MAX_TANK_1_3_TIP_GAL)
|
||||
#define MAX_TANK_1_3_LBS (LBS_PER_GAL * MAX_TANK_1_3_GAL)
|
||||
#define MAX_TANK_2_LBS (LBS_PER_GAL * MAX_TANK_2_GAL)
|
||||
#define MAX_UPR_AUX_LBS (LBS_PER_GAL * MAX_UPR_AUX_GAL)
|
||||
#define MAX_LWR_AUX_LBS (LBS_PER_GAL * MAX_LWR_AUX_GAL)
|
||||
#define MAX_TAIL_LBS (LBS_PER_GAL * MAX_TAIL_GAL)
|
||||
#define MAX_FWD_AUX_LBS (LBS_PER_GAL * MAX_FWD_AUX_GAL)
|
||||
// Max Fuel
|
||||
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
|
||||
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
|
||||
// Arms Fuel
|
||||
#define ARM_MAIN1 -240.0
|
||||
#define ARM_MAIN3 -240.0
|
||||
#define ARM_MAIN2 120.0
|
||||
#define ARM_UPPER_AUX 0.0
|
||||
#define ARM_LOWER_AUX 0.0
|
||||
#define ARM_MAIN1_TIP -468.0
|
||||
#define ARM_MAIN3_TIP -468.0
|
||||
#define ARM_TAIL -840.0
|
||||
#define ARM_FORWARD_AUX1 60.0
|
||||
#define ARM_FORWARD_AUX2 60.0
|
||||
|
||||
/***************************** Data structures *****************************/
|
||||
typedef struct {
|
||||
// SimConnect mapped
|
||||
double main1;
|
||||
double main3;
|
||||
double main2;
|
||||
double upperAux;
|
||||
double lowerAux;
|
||||
double main1Tip;
|
||||
double main3Tip;
|
||||
double tail;
|
||||
double forwardAux1;
|
||||
double forwardAux2;
|
||||
// Additional properties
|
||||
double total;
|
||||
} FuelData_t;
|
||||
|
||||
typedef struct {
|
||||
double main1;
|
||||
double main3;
|
||||
double main2;
|
||||
double upperAux;
|
||||
double lowerAux;
|
||||
double tail;
|
||||
double forwardAux1;
|
||||
double forwardAux2;
|
||||
} FuelDataSet_t;
|
||||
|
||||
/******************************** Functions ********************************/
|
||||
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const bool isImperial, const bool isER);
|
||||
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const UserData_t *const userData);
|
||||
void fuel(const FuelData_t *const targetFuel, const HANDLE simConnect);
|
||||
@@ -0,0 +1,43 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
/********************************* Headers *********************************/
|
||||
// MSFS headers
|
||||
#include "rapidjson/filewritestream.h"
|
||||
#include <MSFS/MSFS.h>
|
||||
#include <MSFS/MSFS_CommBus.h>
|
||||
#include <MSFS/MSFS_Core.h>
|
||||
#include <MSFS/MSFS_GaugeContext.h>
|
||||
#include <MSFS/MSFS_WindowsTypes.h>
|
||||
#include <SimConnect.h>
|
||||
#include <rapidjson/document.h>
|
||||
#include <rapidjson/filereadstream.h>
|
||||
#include <rapidjson/writer.h>
|
||||
|
||||
// Own headers
|
||||
#include "freighter.h"
|
||||
#include "fuel.h"
|
||||
#include "log.h"
|
||||
#include "pax.h"
|
||||
#include "shared.h"
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
// Module identification
|
||||
// COMM BUS
|
||||
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
||||
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
||||
|
||||
/******************************** Functions ********************************/
|
||||
void commBusUpdateTargetCallback(const char *args, unsigned int size, void *ctx);
|
||||
int receiveData(const char *buf);
|
||||
void sendData();
|
||||
void CALLBACK MyDispatchProc(SIMCONNECT_RECV *pData, DWORD cbData, void *pContext);
|
||||
@@ -0,0 +1,25 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
// C headers
|
||||
#include <stdio.h>
|
||||
#include <stdlib.h>
|
||||
#include <string.h>
|
||||
// C++ headers
|
||||
#include <ctime>
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
// Module identification
|
||||
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
|
||||
#define VERSION_STRING "2.40"
|
||||
|
||||
void toLog(FILE *file, const char *format, double *optional = nullptr);
|
||||
@@ -0,0 +1,156 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
/********************************* Headers *********************************/
|
||||
// MSFS headers
|
||||
#include <MSFS/MSFS_WindowsTypes.h>
|
||||
#include <SimConnect.h>
|
||||
// C headers
|
||||
#include <math.h>
|
||||
// C++ headers
|
||||
#include <algorithm>
|
||||
// Own headers
|
||||
#include "fuel.h"
|
||||
#include "log.h"
|
||||
#include "shared.h"
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
// 2x 190lbs default
|
||||
#define FRONT_CREW_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (760.0) : (344.0))
|
||||
// 2x 190lbs default
|
||||
#define REAR_CREW_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (760.0) : (344.0))
|
||||
// All actual Business seats
|
||||
#define MAX_BUSINESS_1 18
|
||||
// First 5 rows of economy
|
||||
#define MAX_BUSINESS_2 45
|
||||
// Next 10 rows
|
||||
#define MAX_ECONOMY_1 86
|
||||
// Remaining rows
|
||||
// 12 x 9
|
||||
// 6 x 8
|
||||
// 4 x 2
|
||||
#define MAX_ECONOMY_2 164
|
||||
// Total
|
||||
#define MAX_PAX 313
|
||||
// Max ZFW
|
||||
#define MAX_PAX_ZFW(IS_IMPERIAL) ((IS_IMPERIAL) ? (400000) : (181437))
|
||||
// Arms
|
||||
#define ARM_PAX_CABIN_CREW_FRONT 792.0
|
||||
#define ARM_PAX_BUSINESS1_LEFT 540.0
|
||||
#define ARM_PAX_BUSINESS1_CENTER 540.0
|
||||
#define ARM_PAX_BUSINESS1_RIGHT 540.0
|
||||
#define ARM_PAX_BUSINESS2_LEFT 300.0
|
||||
#define ARM_PAX_BUSINESS2_CENTER 300.0
|
||||
#define ARM_PAX_BUSINESS2_RIGHT 300.0
|
||||
#define ARM_PAX_ECONOMY1_LEFT -240.0
|
||||
#define ARM_PAX_ECONOMY1_CENTER -240.0
|
||||
#define ARM_PAX_ECONOMY1_RIGHT -240.0
|
||||
#define ARM_PAX_ECONOMY2_LEFT -600.0
|
||||
#define ARM_PAX_ECONOMY2_CENTER -600.0
|
||||
#define ARM_PAX_ECONOMY2_RIGHT -600.0
|
||||
#define ARM_PAX_CABIN_CREW_REAR -660.0
|
||||
|
||||
/***************************** Data structures *****************************/
|
||||
typedef struct {
|
||||
// SimConnect mapped
|
||||
double pilot;
|
||||
double firstOfficer;
|
||||
double engineer;
|
||||
double cabinCrewFront;
|
||||
double business1Left;
|
||||
double business1Center;
|
||||
double business1Right;
|
||||
double business2Left;
|
||||
double business2Center;
|
||||
double business2Right;
|
||||
double economy1Left;
|
||||
double economy1Center;
|
||||
double economy1Right;
|
||||
double economy2Left;
|
||||
double economy2Center;
|
||||
double economy2Right;
|
||||
double cabinCrewRear;
|
||||
double forwardCargo;
|
||||
double rearCargo;
|
||||
double leftAux;
|
||||
double rightAux;
|
||||
double _ZFWCG; // DO NOT USE
|
||||
|
||||
// Additional properties
|
||||
double empty;
|
||||
double total;
|
||||
double CGTarget;
|
||||
double ZFWCG;
|
||||
double TOCG;
|
||||
struct paxCount {
|
||||
unsigned char business1;
|
||||
unsigned char business2;
|
||||
unsigned char economy1;
|
||||
unsigned char economy2;
|
||||
unsigned short total;
|
||||
} paxCount;
|
||||
struct sbPlanned {
|
||||
double ZFW;
|
||||
double GW;
|
||||
double fuel;
|
||||
unsigned short pax;
|
||||
unsigned int cargo;
|
||||
} sbPlanned;
|
||||
} paxPayloadData_t;
|
||||
|
||||
typedef struct {
|
||||
double pilot;
|
||||
double firstOfficer;
|
||||
double engineer;
|
||||
double cabinCrewFront;
|
||||
double business1Left;
|
||||
double business1Center;
|
||||
double business1Right;
|
||||
double business2Left;
|
||||
double business2Center;
|
||||
double business2Right;
|
||||
double economy1Left;
|
||||
double economy1Center;
|
||||
double economy1Right;
|
||||
double economy2Left;
|
||||
double economy2Center;
|
||||
double economy2Right;
|
||||
double cabinCrewRear;
|
||||
double forwardCargo;
|
||||
double rearCargo;
|
||||
double leftAux;
|
||||
double rightAux;
|
||||
double ZFWCG;
|
||||
} paxPayloadDataSet_t;
|
||||
|
||||
/******************************** Functions ********************************/
|
||||
// ZFW Entry, fill pax first (pax+bag), rest is cargo
|
||||
void distribute(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
|
||||
const UserData_t *const userData, const UserOptions_t *const userOptions);
|
||||
// SimBrief Entry, SB pax count and total cargo
|
||||
void distribute(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned short numPax, unsigned int cargo,
|
||||
const UserData_t *const userData, const UserOptions_t *const userOptions);
|
||||
// Updates pax stations with their respective weights
|
||||
// Used internally and used for Station Entry (pax only, cargo is ste directly)
|
||||
// STATION WEIGHTS ARE NOT NORMALISED TO POUNDS
|
||||
void generatePayload(paxPayloadData_t *const targetPayload, const bool isImperial, const UserOptions_t *const userOptions);
|
||||
// Normalise to Pounds
|
||||
// For Station Entry: CALL AFTER `generatePayload`
|
||||
void normalisePayload(paxPayloadData_t *const targetPayload, const bool isImperial);
|
||||
void calculateCGs(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial);
|
||||
void load(const paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
|
||||
const bool isImperial);
|
||||
void unload(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER);
|
||||
// Based on ICAO/LH findings
|
||||
double PAX_WEIGHT(const bool isImperial, const UserOptions_t *const options);
|
||||
// Based on ICAO/LH findings
|
||||
double BAG_WEIGHT(const bool isImperial, const UserOptions_t *const options);
|
||||
@@ -0,0 +1,131 @@
|
||||
#pragma once
|
||||
|
||||
#ifndef __INTELLISENSE__
|
||||
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||
#else
|
||||
#define MODULE_EXPORT
|
||||
#define MODULE_WASM_MODNAME(mod)
|
||||
#define __attribute__(x)
|
||||
#define __restrict__
|
||||
#endif
|
||||
|
||||
/******************************** Constants ********************************/
|
||||
// 190lbs default
|
||||
#define PILOT_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (190.0) : (86.0))
|
||||
// 200lbs per tank (one LD3)
|
||||
#define AUX_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (200.0) : (91.0))
|
||||
// PMC pallet due to 104in door
|
||||
#define MAX_FRONT_CARGO(IS_IMPERIAL) ((IS_IMPERIAL) ? (6.0 * 15000.0) : (6.0 * 6804.0))
|
||||
// LD3s due to 70in door, ER option takes up two slots
|
||||
#define MAX_REAR_CARGO(IS_IMPERIAL, IS_ER) ((IS_IMPERIAL) ? ((IS_ER ? 12.0 : 14.0) * 3500.0) : ((IS_ER ? 12.0 : 14.0) * 1588.0))
|
||||
// Max TOW
|
||||
#define MAX_TOW(IS_IMPERIAL) ((IS_IMPERIAL) ? (625500) : (283722))
|
||||
#define MAX_TOW_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (630500) : (285990))
|
||||
// Arms Shared
|
||||
#define ARM_EMPTY -120.0
|
||||
#define ARM_PILOT 984.0
|
||||
#define ARM_FIRST_OFFICER 984.0
|
||||
#define ARM_ENGINEER 960.0
|
||||
#define ARM_FORWARD_CARGO 360.0
|
||||
#define ARM_REAR_CARGO -360.0
|
||||
#define ARM_LEFT_AUX 60.0
|
||||
#define ARM_RIGHT_AUX 60.0
|
||||
// MAC
|
||||
#define ROOT_CHORD 34.68
|
||||
#define WING_SPAN 170.5
|
||||
#define WING_AREA 3648.0
|
||||
#define QUARTER_MAC -165.0 // aero_center
|
||||
#define TIP_CHORD ((2.0 * WING_AREA) / WING_SPAN - ROOT_CHORD)
|
||||
#define TAPER_RATIO (TIP_CHORD / ROOT_CHORD)
|
||||
#define MAC ((2.0 / 3.0) * ROOT_CHORD * ((1.0 + TAPER_RATIO + (TAPER_RATIO * TAPER_RATIO)) / (1.0 + TAPER_RATIO)) * 12.0)
|
||||
#define LEMAC (QUARTER_MAC + (1.0 / 4.0) * MAC)
|
||||
// CG Limits
|
||||
#define MIN_CG 12.0
|
||||
#define MAX_CG 34.0
|
||||
#define CG_TOLERANCE 0.05
|
||||
// GSX States
|
||||
#define GSX_SERVICE_IDLE 1
|
||||
#define GSX_SERVICE_CALLED 4
|
||||
#define GSX_SERVICE_ACTIVE 5
|
||||
#define GSX_SERVICE_FINISHED 6
|
||||
|
||||
/********************************* Macros **********************************/
|
||||
// Conversions
|
||||
#define TO_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE)*2.20462262185)
|
||||
#define FROM_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE) * (1.0 / 2.20462262185))
|
||||
// MAC
|
||||
#define TO_PERCENT_MAC(POS) ((((POS)-LEMAC) / MAC) * -100.0)
|
||||
|
||||
/********************************** ENUMS **********************************/
|
||||
enum DATA_DEFINITIONS {
|
||||
DATA_DEFINITION_EMPTY_WEIGHT,
|
||||
DATA_DEFINITION_PAYLOAD_PAX,
|
||||
DATA_DEFINITION_PAYLOAD_F,
|
||||
DATA_DEFINITION_FUEL,
|
||||
DATA_DEFINITION_FUEL_SET,
|
||||
DATA_DEFINITION_GSX,
|
||||
DATA_DEFINITION_USER_DATA,
|
||||
};
|
||||
|
||||
enum DATA_REQUESTS {
|
||||
DATA_REQUEST_EMPTY_WEIGHT,
|
||||
DATA_REQUEST_PAYLOAD_PAX,
|
||||
DATA_REQUEST_PAYLOAD_F,
|
||||
DATA_REQUEST_FUEL,
|
||||
DATA_REQUEST_FUEL_SET,
|
||||
DATA_REQUEST_GSX,
|
||||
DATA_REQUEST_USER_DATA,
|
||||
};
|
||||
|
||||
enum LOADING_STATES {
|
||||
LOADING_STATE_IDLE,
|
||||
LOADING_STATE_BOARDING,
|
||||
LOADING_STATE_BOARDED,
|
||||
LOADING_STATE_DEBOARDING,
|
||||
LOADING_STATE_DEBOARDED,
|
||||
};
|
||||
|
||||
enum FUELING_STATES { FUELING_STATE_IDLE, FUELING_STATE_CALLED, FUELING_STATE_FUELING, FUELING_STATE_FUELED };
|
||||
|
||||
enum CALL_MODES {
|
||||
CALL_MODE_SB_SET,
|
||||
CALL_MODE_ZFW_SET,
|
||||
CALL_MODE_STATION_SET,
|
||||
CALL_MODE_LOAD_SET,
|
||||
CALL_MODE_UNLOAD_SET,
|
||||
CALL_MODE_OPTIONS_SET,
|
||||
CALL_MODE_GSX_RESET,
|
||||
};
|
||||
|
||||
/***************************** Data structures *****************************/
|
||||
typedef struct {
|
||||
double isCargo;
|
||||
double isER;
|
||||
double isImperial;
|
||||
} UserData_t;
|
||||
|
||||
typedef struct {
|
||||
// SimConnect mapped
|
||||
double couatlStarted; // boolean
|
||||
double boardingState; // See manual, 5 => active
|
||||
double deboardingState; // See manual, 5 => active
|
||||
double refuelingState; // See manual, 5 => active
|
||||
double passengersBoarded; // Num pax
|
||||
double passengersDeboarded; // Num pax
|
||||
double cargoBoarded; // In percent
|
||||
double cargoDeboarded; // In percent
|
||||
double fuelConnected; // boolean
|
||||
|
||||
// Additional properties
|
||||
enum LOADING_STATES loadingState;
|
||||
enum FUELING_STATES fuelingState;
|
||||
} GSXData_t;
|
||||
|
||||
typedef struct {
|
||||
bool GSXSync;
|
||||
double paxWeightKG;
|
||||
double bagWeightKG;
|
||||
double paxWeightLBS;
|
||||
double bagWeightLBS;
|
||||
} UserOptions_t;
|
||||
@@ -0,0 +1,25 @@
|
||||
|
||||
Microsoft Visual Studio Solution File, Format Version 12.00
|
||||
# Visual Studio Version 17
|
||||
VisualStudioVersion = 17.13.36105.23
|
||||
MinimumVisualStudioVersion = 10.0.40219.1
|
||||
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager", "load-manager.vcxproj", "{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}"
|
||||
EndProject
|
||||
Global
|
||||
GlobalSection(SolutionConfigurationPlatforms) = preSolution
|
||||
Debug|MSFS = Debug|MSFS
|
||||
Release|MSFS = Release|MSFS
|
||||
EndGlobalSection
|
||||
GlobalSection(ProjectConfigurationPlatforms) = postSolution
|
||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|MSFS.ActiveCfg = Debug|MSFS
|
||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|MSFS.Build.0 = Debug|MSFS
|
||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.ActiveCfg = Release|MSFS
|
||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.Build.0 = Release|MSFS
|
||||
EndGlobalSection
|
||||
GlobalSection(SolutionProperties) = preSolution
|
||||
HideSolutionNode = FALSE
|
||||
EndGlobalSection
|
||||
GlobalSection(ExtensibilityGlobals) = postSolution
|
||||
SolutionGuid = {835CA9EE-0C67-4B32-B910-3F3A40943047}
|
||||
EndGlobalSection
|
||||
EndGlobal
|
||||
@@ -0,0 +1,4 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<Project ToolsVersion="Current" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
||||
<PropertyGroup />
|
||||
</Project>
|
||||
@@ -0,0 +1,174 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<Project DefaultTargets="Build" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
||||
<ItemGroup Label="ProjectConfigurations">
|
||||
<ProjectConfiguration Include="Debug|MSFS">
|
||||
<Configuration>Debug</Configuration>
|
||||
<Platform>MSFS</Platform>
|
||||
</ProjectConfiguration>
|
||||
<ProjectConfiguration Include="Release|MSFS">
|
||||
<Configuration>Release</Configuration>
|
||||
<Platform>MSFS</Platform>
|
||||
</ProjectConfiguration>
|
||||
</ItemGroup>
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||||
<PropertyGroup Label="Globals">
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||||
<VCProjectVersion>16.0</VCProjectVersion>
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||||
<ProjectGuid>{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}</ProjectGuid>
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||||
<RootNamespace>Module</RootNamespace>
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||||
<WindowsTargetPlatformVersion>10.0</WindowsTargetPlatformVersion>
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||||
<ProjectName>load-manager</ProjectName>
|
||||
</PropertyGroup>
|
||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.Default.props" />
|
||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="Configuration">
|
||||
<ConfigurationType>Application</ConfigurationType>
|
||||
<UseDebugLibraries>true</UseDebugLibraries>
|
||||
<PlatformToolset>MSFS2024</PlatformToolset>
|
||||
<CharacterSet>MultiByte</CharacterSet>
|
||||
</PropertyGroup>
|
||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="Configuration">
|
||||
<ConfigurationType>Application</ConfigurationType>
|
||||
<UseDebugLibraries>false</UseDebugLibraries>
|
||||
<PlatformToolset>MSFS2024</PlatformToolset>
|
||||
<WholeProgramOptimization>true</WholeProgramOptimization>
|
||||
<CharacterSet>MultiByte</CharacterSet>
|
||||
</PropertyGroup>
|
||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.props" />
|
||||
<ImportGroup Label="ExtensionSettings">
|
||||
</ImportGroup>
|
||||
<ImportGroup Label="Shared">
|
||||
</ImportGroup>
|
||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="PropertySheets">
|
||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
||||
</ImportGroup>
|
||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="PropertySheets">
|
||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
||||
</ImportGroup>
|
||||
<PropertyGroup Label="UserMacros" />
|
||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
|
||||
<TargetExt>.wasm</TargetExt>
|
||||
<GenerateManifest />
|
||||
<LinkIncremental />
|
||||
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
|
||||
<TargetName>$(ProjectName)</TargetName>
|
||||
</PropertyGroup>
|
||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
||||
<TargetExt>.wasm</TargetExt>
|
||||
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
|
||||
</PropertyGroup>
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||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
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||||
<ClCompile>
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||||
<WarningLevel>Level3</WarningLevel>
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||||
<Optimization>Disabled</Optimization>
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||||
<SDLCheck>
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||||
</SDLCheck>
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||||
<ConformanceMode>true</ConformanceMode>
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||||
<BufferSecurityCheck>false</BufferSecurityCheck>
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||||
<AdditionalIncludeDirectories>
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||||
</AdditionalIncludeDirectories>
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||||
<PreprocessorDefinitions>__wasi__;_STRING_H_CPLUSPLUS_98_CONFORMANCE_;_WCHAR_H_CPLUSPLUS_98_CONFORMANCE_;_LIBCPP_HAS_NO_THREADS;_WINDLL;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
||||
<ShowIncludes>false</ShowIncludes>
|
||||
<ExceptionHandling>false</ExceptionHandling>
|
||||
<RuntimeTypeInfo>
|
||||
</RuntimeTypeInfo>
|
||||
<SupportJustMyCode>
|
||||
</SupportJustMyCode>
|
||||
<DebugInformationFormat>ProgramDatabase</DebugInformationFormat>
|
||||
<BasicRuntimeChecks>
|
||||
</BasicRuntimeChecks>
|
||||
<LanguageStandard>stdcpp14</LanguageStandard>
|
||||
<MultiProcessorCompilation>true</MultiProcessorCompilation>
|
||||
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
|
||||
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
||||
</ClCompile>
|
||||
<Link>
|
||||
<SubSystem>
|
||||
</SubSystem>
|
||||
<AdditionalDependencies>
|
||||
</AdditionalDependencies>
|
||||
<IgnoreAllDefaultLibraries>
|
||||
</IgnoreAllDefaultLibraries>
|
||||
<NoEntryPoint>true</NoEntryPoint>
|
||||
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
|
||||
<RandomizedBaseAddress>
|
||||
</RandomizedBaseAddress>
|
||||
<DataExecutionPrevention>
|
||||
</DataExecutionPrevention>
|
||||
<GenerateDebugInformation>true</GenerateDebugInformation>
|
||||
<ProgramDatabaseFile>
|
||||
</ProgramDatabaseFile>
|
||||
<ImportLibrary>
|
||||
</ImportLibrary>
|
||||
<ProfileGuidedDatabase>
|
||||
</ProfileGuidedDatabase>
|
||||
<AdditionalLibraryDirectories>
|
||||
</AdditionalLibraryDirectories>
|
||||
</Link>
|
||||
<PostBuildEvent>
|
||||
<Command>cd $(SolutionDir)..\..\
|
||||
Powershell.exe -File .\copy-debug.ps1</Command>
|
||||
</PostBuildEvent>
|
||||
</ItemDefinitionGroup>
|
||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
||||
<ClCompile>
|
||||
<WarningLevel>Level3</WarningLevel>
|
||||
<Optimization>MaxSpeed</Optimization>
|
||||
<FunctionLevelLinking>true</FunctionLevelLinking>
|
||||
<IntrinsicFunctions>true</IntrinsicFunctions>
|
||||
<SDLCheck>true</SDLCheck>
|
||||
<ConformanceMode>true</ConformanceMode>
|
||||
<AdditionalIncludeDirectories>
|
||||
</AdditionalIncludeDirectories>
|
||||
<PreprocessorDefinitions>__wasi__;__wasm32__;_STRING_H_CPLUSPLUS_98_CONFORMANCE_;_WCHAR_H_CPLUSPLUS_98_CONFORMANCE_;_LIBCPP_NO_EXCEPTIONS;_LIBCPP_HAS_NO_THREADS;_LIBCPP_STD_VER=14;_WINDLL;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
||||
<BufferSecurityCheck>false</BufferSecurityCheck>
|
||||
<ExceptionHandling>false</ExceptionHandling>
|
||||
<DebugInformationFormat>false</DebugInformationFormat>
|
||||
<SupportJustMyCode>
|
||||
</SupportJustMyCode>
|
||||
<LanguageStandard>stdcpp14</LanguageStandard>
|
||||
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
|
||||
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
||||
</ClCompile>
|
||||
<Link>
|
||||
<SubSystem>
|
||||
</SubSystem>
|
||||
<AdditionalDependencies>%(AdditionalDependencies)</AdditionalDependencies>
|
||||
<IgnoreAllDefaultLibraries>
|
||||
</IgnoreAllDefaultLibraries>
|
||||
<NoEntryPoint>true</NoEntryPoint>
|
||||
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
|
||||
<RandomizedBaseAddress>
|
||||
</RandomizedBaseAddress>
|
||||
<DataExecutionPrevention>
|
||||
</DataExecutionPrevention>
|
||||
<GenerateDebugInformation>false</GenerateDebugInformation>
|
||||
<ProgramDatabaseFile>
|
||||
</ProgramDatabaseFile>
|
||||
<ImportLibrary>
|
||||
</ImportLibrary>
|
||||
<ProfileGuidedDatabase>
|
||||
</ProfileGuidedDatabase>
|
||||
<AdditionalLibraryDirectories>$(OutDir)</AdditionalLibraryDirectories>
|
||||
</Link>
|
||||
<PostBuildEvent>
|
||||
<Command>cd $(SolutionDir)..\..\
|
||||
Powershell.exe -File .\copy-release.ps1</Command>
|
||||
</PostBuildEvent>
|
||||
</ItemDefinitionGroup>
|
||||
<ItemGroup>
|
||||
<ClCompile Include="src/freighter.cpp" />
|
||||
<ClCompile Include="src/load-manager.cpp" />
|
||||
<ClCompile Include="src/log.cpp" />
|
||||
<ClCompile Include="src/pax.cpp" />
|
||||
<ClCompile Include="src/fuel.cpp" />
|
||||
</ItemGroup>
|
||||
<ItemGroup>
|
||||
<ClInclude Include="include/freighter.h" />
|
||||
<ClInclude Include="include/load-manager.h" />
|
||||
<ClInclude Include="include/log.h" />
|
||||
<ClInclude Include="include/pax.h" />
|
||||
<ClInclude Include="include/shared.h" />
|
||||
<ClInclude Include="include/fuel.h" />
|
||||
</ItemGroup>
|
||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
|
||||
<ImportGroup Label="ExtensionTargets">
|
||||
</ImportGroup>
|
||||
</Project>
|
||||
@@ -0,0 +1,50 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<Project ToolsVersion="4.0" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
||||
<ItemGroup>
|
||||
<ClCompile Include="src/freighter.cpp">
|
||||
<Filter>Source Files</Filter>
|
||||
</ClCompile>
|
||||
<ClCompile Include="src/load-manager.cpp">
|
||||
<Filter>Source Files</Filter>
|
||||
</ClCompile>
|
||||
<ClCompile Include="src/log.cpp">
|
||||
<Filter>Source Files</Filter>
|
||||
</ClCompile>
|
||||
<ClCompile Include="src/pax.cpp">
|
||||
<Filter>Source Files</Filter>
|
||||
</ClCompile>
|
||||
<ClCompile Include="src/fuel.cpp">
|
||||
<Filter>Source Files</Filter>
|
||||
</ClCompile>
|
||||
</ItemGroup>
|
||||
<ItemGroup>
|
||||
<ClInclude Include="include/freighter.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
<ClInclude Include="include/load-manager.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
<ClInclude Include="include/log.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
<ClInclude Include="include/pax.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
<ClInclude Include="include/shared.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
<ClInclude Include="include/fuel.h">
|
||||
<Filter>Header Files</Filter>
|
||||
</ClInclude>
|
||||
</ItemGroup>
|
||||
<ItemGroup>
|
||||
<Filter Include="Header Files">
|
||||
<UniqueIdentifier>{93995380-89BD-4b04-88EB-625FBE52EBFB}</UniqueIdentifier>
|
||||
<Extensions>h;hh;hpp;hxx;h++;hm;inl;inc;ipp;xsd</Extensions>
|
||||
</Filter>
|
||||
<Filter Include="Source Files">
|
||||
<UniqueIdentifier>{4FC737F1-C7A5-4376-A066-2A32D752A2FF}</UniqueIdentifier>
|
||||
<Extensions>cpp;c;cc;cxx;c++;cppm;ixx;def;odl;idl;hpj;bat;asm;asmx</Extensions>
|
||||
</Filter>
|
||||
</ItemGroup>
|
||||
</Project>
|
||||
@@ -0,0 +1,4 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<Project ToolsVersion="Current" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
||||
<PropertyGroup />
|
||||
</Project>
|
||||
@@ -0,0 +1,15 @@
|
||||
{
|
||||
"name": "wasm-module",
|
||||
"version": "0.0.16",
|
||||
"description": "Load Manager WASM module",
|
||||
"scripts": {
|
||||
"clean": "rimraf ../SimObjects/Airplanes/TFDi_Design_MD-11/panel/load-manager.wasm && rimraf MSFS",
|
||||
"build": "MSBuild.exe ./load-manager.sln /p:Platform=MSFS",
|
||||
"build:rel": "MSBuild.exe ./load-manager.sln /p:Platform=MSFS /p:Configuration=Release",
|
||||
"release": "pnpm clean && npm version patch && pnpm build:rel && node stack-analysis"
|
||||
},
|
||||
"keywords": [],
|
||||
"author": "Kilian Kurt Hofmann",
|
||||
"license": "MIT",
|
||||
"packageManager": "pnpm@10.25.0"
|
||||
}
|
||||
@@ -0,0 +1,307 @@
|
||||
#include "freighter.h"
|
||||
|
||||
// ZFW Entry
|
||||
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
|
||||
const UserData_t *const userData) {
|
||||
// Find payload, num pax and extra cargo
|
||||
double payload = ZFWTarget - targetPayload->empty - targetPayload->pilot - targetPayload->firstOfficer -
|
||||
targetPayload->engineer - targetPayload->leftAux - targetPayload->rightAux;
|
||||
unsigned int cargo = round(payload);
|
||||
|
||||
distribute(targetPayload, fuel, cargo, userData);
|
||||
}
|
||||
|
||||
// SimBrief Entry
|
||||
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned int cargo,
|
||||
const UserData_t *const userData) {
|
||||
// Clear
|
||||
targetPayload->stations.upper1 = targetPayload->stations.upper2 = targetPayload->stations.upper3 =
|
||||
targetPayload->stations.upper4 = targetPayload->stations.total = 0;
|
||||
targetPayload->lowerForward = targetPayload->lowerRear = 0;
|
||||
|
||||
unsigned short _cargo = 0;
|
||||
unsigned int count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
|
||||
MAX_REAR_CARGO(userData->isImperial, userData->isER);
|
||||
// Initial distribution
|
||||
while (cargo > 0 && count > 0) {
|
||||
if (cargo >= 6) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper4++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
|
||||
targetPayload->lowerForward++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->lowerRear < MAX_REAR_CARGO(userData->isImperial, userData->isER)) {
|
||||
targetPayload->lowerRear++;
|
||||
_cargo++;
|
||||
}
|
||||
} else if (cargo == 5) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper4++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
|
||||
targetPayload->lowerForward++;
|
||||
_cargo++;
|
||||
}
|
||||
} else if (cargo == 4) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper4++;
|
||||
_cargo++;
|
||||
}
|
||||
} else if (cargo == 3) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
_cargo++;
|
||||
}
|
||||
} else if (cargo == 2) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
_cargo++;
|
||||
}
|
||||
} else if (cargo == 1) {
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
_cargo++;
|
||||
}
|
||||
}
|
||||
cargo -= _cargo;
|
||||
targetPayload->stations.total += _cargo;
|
||||
|
||||
_cargo = 0;
|
||||
|
||||
count--;
|
||||
}
|
||||
// Refinement
|
||||
count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
|
||||
MAX_REAR_CARGO(userData->isImperial, userData->isER);
|
||||
while (count > 0) {
|
||||
generatePayload(targetPayload);
|
||||
calculateCGs(targetPayload, fuel, userData->isImperial);
|
||||
|
||||
// in front of target
|
||||
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
|
||||
if (targetPayload->stations.upper1 > 0) {
|
||||
targetPayload->stations.upper1--;
|
||||
} else if (targetPayload->stations.upper2 > 0) {
|
||||
targetPayload->stations.upper2--;
|
||||
} else if (targetPayload->stations.upper3 > 0) {
|
||||
targetPayload->stations.upper3--;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper4++;
|
||||
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
} else {
|
||||
targetPayload->stations.upper1++;
|
||||
}
|
||||
}
|
||||
// behind target
|
||||
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
|
||||
if (targetPayload->stations.upper4 > 0) {
|
||||
targetPayload->stations.upper4--;
|
||||
} else if (targetPayload->stations.upper3 > 0) {
|
||||
targetPayload->stations.upper3--;
|
||||
} else if (targetPayload->stations.upper2 > 0) {
|
||||
targetPayload->stations.upper2--;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper1++;
|
||||
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper2++;
|
||||
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
|
||||
targetPayload->stations.upper3++;
|
||||
} else {
|
||||
targetPayload->stations.upper4++;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
count--;
|
||||
}
|
||||
// Refinement cargo
|
||||
count = MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
|
||||
while (count > 0) {
|
||||
generatePayload(targetPayload);
|
||||
calculateCGs(targetPayload, fuel, userData->isImperial);
|
||||
|
||||
// in front of target
|
||||
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
|
||||
if (targetPayload->lowerForward > 0 && targetPayload->lowerRear < MAX_REAR_CARGO(userData->isImperial, userData->isER)) {
|
||||
targetPayload->lowerForward--;
|
||||
targetPayload->lowerRear++;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
}
|
||||
// behind target
|
||||
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
|
||||
if (targetPayload->lowerRear > 0 && targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
|
||||
targetPayload->lowerRear--;
|
||||
targetPayload->lowerForward++;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
count--;
|
||||
}
|
||||
}
|
||||
|
||||
// Updates pax stations with their respective weights
|
||||
// Used internally and used for Station Entry (pax only, cargo is set directly)
|
||||
void generatePayload(fPayloadData_t *const targetPayload) {
|
||||
targetPayload->upper1Left = targetPayload->upper1Right = (targetPayload->stations.upper1 / 2.0);
|
||||
targetPayload->upper2Left = targetPayload->upper2Right = (targetPayload->stations.upper2 / 2.0);
|
||||
targetPayload->upper3Left = targetPayload->upper3Right = (targetPayload->stations.upper3 / 2.0);
|
||||
targetPayload->upper4Left = targetPayload->upper4Right = (targetPayload->stations.upper4 / 2.0);
|
||||
targetPayload->total = targetPayload->empty + targetPayload->pilot + targetPayload->firstOfficer + targetPayload->engineer +
|
||||
targetPayload->upper1Left + targetPayload->upper1Right + targetPayload->upper2Left +
|
||||
targetPayload->upper2Right + targetPayload->upper3Left + targetPayload->upper3Right +
|
||||
targetPayload->upper4Left + targetPayload->upper4Right + targetPayload->lowerForward +
|
||||
targetPayload->lowerRear + targetPayload->leftAux + targetPayload->rightAux;
|
||||
}
|
||||
|
||||
// Normalise to Pounds
|
||||
// MANDATORY BEFORE SETTING WEIGHTS
|
||||
// USE ON COPY OF GLOBAL STATE ONLY
|
||||
void normalisePayload(fPayloadData_t *const targetPayload, const bool isImperial) {
|
||||
targetPayload->empty = TO_POUNDS(isImperial, targetPayload->empty);
|
||||
targetPayload->pilot = TO_POUNDS(isImperial, targetPayload->pilot);
|
||||
targetPayload->firstOfficer = TO_POUNDS(isImperial, targetPayload->firstOfficer);
|
||||
targetPayload->engineer = TO_POUNDS(isImperial, targetPayload->engineer);
|
||||
targetPayload->upper1Left = TO_POUNDS(isImperial, targetPayload->upper1Left);
|
||||
targetPayload->upper1Right = TO_POUNDS(isImperial, targetPayload->upper1Right);
|
||||
targetPayload->upper2Left = TO_POUNDS(isImperial, targetPayload->upper2Left);
|
||||
targetPayload->upper2Right = TO_POUNDS(isImperial, targetPayload->upper2Right);
|
||||
targetPayload->upper3Left = TO_POUNDS(isImperial, targetPayload->upper3Left);
|
||||
targetPayload->upper3Right = TO_POUNDS(isImperial, targetPayload->upper3Right);
|
||||
targetPayload->upper4Left = TO_POUNDS(isImperial, targetPayload->upper4Left);
|
||||
targetPayload->upper4Right = TO_POUNDS(isImperial, targetPayload->upper4Right);
|
||||
targetPayload->lowerForward = TO_POUNDS(isImperial, targetPayload->lowerForward);
|
||||
targetPayload->lowerRear = TO_POUNDS(isImperial, targetPayload->lowerRear);
|
||||
targetPayload->leftAux = TO_POUNDS(isImperial, targetPayload->leftAux);
|
||||
targetPayload->rightAux = TO_POUNDS(isImperial, targetPayload->rightAux);
|
||||
}
|
||||
|
||||
void calculateCGs(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial) {
|
||||
fPayloadData_t localPayload = {};
|
||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
||||
normalisePayload(&localPayload, isImperial);
|
||||
|
||||
double totalMoment = localPayload.empty * ARM_EMPTY + localPayload.pilot * ARM_PILOT +
|
||||
localPayload.firstOfficer * ARM_FIRST_OFFICER + localPayload.engineer * ARM_ENGINEER +
|
||||
localPayload.upper1Left * ARM_F_UPPER1_LEFT + localPayload.upper1Right * ARM_F_UPPER1_RIGHT +
|
||||
localPayload.upper2Left * ARM_F_UPPER2_LEFT + localPayload.upper2Right * ARM_F_UPPER2_RIGHT +
|
||||
localPayload.upper3Left * ARM_F_UPPER3_LEFT + localPayload.upper3Right * ARM_F_UPPER3_RIGHT +
|
||||
localPayload.upper4Left * ARM_F_UPPER4_LEFT + localPayload.upper4Right * ARM_F_UPPER4_RIGHT +
|
||||
localPayload.lowerForward * ARM_FORWARD_CARGO + localPayload.lowerRear * ARM_REAR_CARGO +
|
||||
localPayload.leftAux * ARM_LEFT_AUX + localPayload.rightAux * ARM_RIGHT_AUX;
|
||||
|
||||
double totalWeight = localPayload.empty + localPayload.pilot + localPayload.firstOfficer + localPayload.engineer +
|
||||
localPayload.upper1Left + localPayload.upper1Right + localPayload.upper2Left + localPayload.upper2Right +
|
||||
localPayload.upper3Left + localPayload.upper3Right + localPayload.upper4Left + localPayload.upper4Right +
|
||||
localPayload.lowerForward + localPayload.lowerRear + localPayload.leftAux + localPayload.rightAux;
|
||||
|
||||
targetPayload->ZFWCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
||||
|
||||
totalMoment += fuel->main1 * ARM_MAIN1 + fuel->main3 * ARM_MAIN3 + fuel->main2 * ARM_MAIN2 + fuel->upperAux * ARM_UPPER_AUX +
|
||||
fuel->lowerAux * ARM_LOWER_AUX + fuel->main1Tip * ARM_MAIN1_TIP + fuel->main3Tip * ARM_MAIN3_TIP +
|
||||
fuel->tail * ARM_TAIL + fuel->forwardAux1 * ARM_FORWARD_AUX1 + fuel->forwardAux2 * ARM_FORWARD_AUX2;
|
||||
|
||||
totalWeight += fuel->total;
|
||||
|
||||
targetPayload->TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
||||
}
|
||||
|
||||
void load(const fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
|
||||
const bool isImperial) {
|
||||
fPayloadData_t localPayload = {};
|
||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
||||
normalisePayload(&localPayload, isImperial);
|
||||
|
||||
calculateCGs(&localPayload, fuel, isImperial);
|
||||
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
|
||||
|
||||
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
|
||||
|
||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
|
||||
sizeof(fPayloadDataSet_t), &localPayload);
|
||||
}
|
||||
|
||||
void unloadF(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER) {
|
||||
fPayloadData_t localPayload = {};
|
||||
|
||||
localPayload.empty = empty;
|
||||
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
|
||||
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
|
||||
|
||||
calculateCGs(&localPayload, fuel, true);
|
||||
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
|
||||
|
||||
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
|
||||
|
||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
|
||||
sizeof(fPayloadDataSet_t), &localPayload);
|
||||
}
|
||||
@@ -0,0 +1,138 @@
|
||||
#include "fuel.h"
|
||||
|
||||
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const bool isImperial, const bool isER) {
|
||||
double fuelLbs = TO_POUNDS(isImperial, fuelTarget);
|
||||
|
||||
// Equal mains
|
||||
if (fuelLbs <= MAX_TANK_1_3_LBS * 3) {
|
||||
double tanks = fuelLbs / 3;
|
||||
// Only main
|
||||
if (tanks <= MAX_TANK_1_3_TIP_LBS) {
|
||||
targetFuel->main1 = tanks;
|
||||
targetFuel->main3 = tanks;
|
||||
targetFuel->main1Tip = 0;
|
||||
targetFuel->main3Tip = 0;
|
||||
}
|
||||
// Tips
|
||||
else if (tanks <= MAX_TANK_1_3_TIP_LBS * 2) {
|
||||
double tips = tanks - MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main1 = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main1Tip = tips;
|
||||
targetFuel->main3Tip = tips;
|
||||
}
|
||||
// Max tip
|
||||
else {
|
||||
double mains = tanks - MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main1 = mains;
|
||||
targetFuel->main3 = mains;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
}
|
||||
|
||||
targetFuel->main2 = tanks;
|
||||
|
||||
targetFuel->upperAux = 0;
|
||||
targetFuel->lowerAux = 0;
|
||||
targetFuel->tail = 0;
|
||||
targetFuel->forwardAux1 = 0;
|
||||
targetFuel->forwardAux2 = 0;
|
||||
}
|
||||
// No Aux
|
||||
else if (fuelLbs <= MAX_TANK_1_3_LBS * 2 + MAX_TANK_2_LBS) {
|
||||
targetFuel->main1 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
|
||||
targetFuel->main2 = fuelLbs - MAX_TANK_1_3_LBS * 2;
|
||||
|
||||
targetFuel->upperAux = 0;
|
||||
targetFuel->lowerAux = 0;
|
||||
targetFuel->tail = 0;
|
||||
targetFuel->forwardAux1 = 0;
|
||||
targetFuel->forwardAux2 = 0;
|
||||
}
|
||||
// UPR AUX
|
||||
else if (fuelLbs <= MAX_TANK_1_3_LBS * 2 + MAX_TANK_2_LBS + MAX_UPR_AUX_LBS) {
|
||||
targetFuel->main1 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main2 = MAX_TANK_2_LBS;
|
||||
|
||||
targetFuel->upperAux = fuelLbs - MAX_TANK_1_3_LBS * 2 - MAX_TANK_2_LBS;
|
||||
|
||||
targetFuel->lowerAux = 0;
|
||||
targetFuel->tail = 0;
|
||||
targetFuel->forwardAux1 = 0;
|
||||
targetFuel->forwardAux2 = 0;
|
||||
}
|
||||
// LWR AUX
|
||||
else if (fuelLbs <= MAX_TANK_1_3_LBS * 2 + MAX_TANK_2_LBS + MAX_UPR_AUX_LBS + MAX_LWR_AUX_LBS) {
|
||||
targetFuel->main1 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main2 = MAX_TANK_2_LBS;
|
||||
targetFuel->upperAux = MAX_UPR_AUX_LBS;
|
||||
|
||||
targetFuel->lowerAux = fuelLbs - MAX_TANK_1_3_LBS * 2 - MAX_TANK_2_LBS - MAX_UPR_AUX_LBS;
|
||||
|
||||
targetFuel->tail = 0;
|
||||
targetFuel->forwardAux1 = 0;
|
||||
targetFuel->forwardAux2 = 0;
|
||||
}
|
||||
// Tail
|
||||
else if (fuelLbs <= MAX_TANK_1_3_LBS * 2 + MAX_TANK_2_LBS + MAX_UPR_AUX_LBS + MAX_LWR_AUX_LBS + MAX_TAIL_LBS) {
|
||||
targetFuel->main1 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main2 = MAX_TANK_2_LBS;
|
||||
targetFuel->upperAux = MAX_UPR_AUX_LBS;
|
||||
targetFuel->lowerAux = MAX_LWR_AUX_LBS;
|
||||
|
||||
targetFuel->tail = fuelLbs - MAX_TANK_1_3_LBS * 2 - MAX_TANK_2_LBS - MAX_UPR_AUX_LBS - MAX_LWR_AUX_LBS;
|
||||
|
||||
targetFuel->forwardAux1 = 0;
|
||||
targetFuel->forwardAux2 = 0;
|
||||
} else if (isER) {
|
||||
targetFuel->main1 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main3 = MAX_TANK_1_3_MAIN_LBS;
|
||||
targetFuel->main1Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main3Tip = MAX_TANK_1_3_TIP_LBS;
|
||||
targetFuel->main2 = MAX_TANK_2_LBS;
|
||||
targetFuel->upperAux = MAX_UPR_AUX_LBS;
|
||||
targetFuel->lowerAux = MAX_LWR_AUX_LBS;
|
||||
targetFuel->tail = MAX_TAIL_LBS;
|
||||
|
||||
fuelLbs = fuelLbs - MAX_TANK_1_3_LBS * 2 - MAX_TANK_2_LBS - MAX_UPR_AUX_LBS - MAX_LWR_AUX_LBS - MAX_TAIL_LBS;
|
||||
targetFuel->forwardAux1 = min(fuelLbs / 2, MAX_FWD_AUX_LBS);
|
||||
targetFuel->forwardAux2 = min(fuelLbs / 2, MAX_FWD_AUX_LBS);
|
||||
}
|
||||
|
||||
targetFuel->total = targetFuel->main1 + targetFuel->main3 + targetFuel->main2 + targetFuel->upperAux + targetFuel->lowerAux +
|
||||
targetFuel->main1Tip + targetFuel->main3Tip + targetFuel->tail + targetFuel->forwardAux1 +
|
||||
targetFuel->forwardAux2;
|
||||
}
|
||||
|
||||
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const UserData_t *const userData) {
|
||||
distribute(targetFuel, fuelTarget, userData->isImperial, userData->isER);
|
||||
}
|
||||
|
||||
void fuel(const FuelData_t *const targetFuel, const HANDLE simConnect) {
|
||||
FuelDataSet_t localFuel = {};
|
||||
|
||||
localFuel.main1 = min(MAX_TANK_1_3_GAL, (targetFuel->main1 + targetFuel->main1Tip) / LBS_PER_GAL);
|
||||
localFuel.main2 = min(MAX_TANK_2_GAL, targetFuel->main2 / LBS_PER_GAL);
|
||||
localFuel.main3 = min(MAX_TANK_1_3_GAL, (targetFuel->main3 + targetFuel->main3Tip) / LBS_PER_GAL);
|
||||
localFuel.upperAux = min(MAX_UPR_AUX_GAL, targetFuel->upperAux / LBS_PER_GAL);
|
||||
localFuel.lowerAux = min(MAX_LWR_AUX_GAL, targetFuel->lowerAux / LBS_PER_GAL);
|
||||
localFuel.tail = min(MAX_TAIL_GAL, targetFuel->tail / LBS_PER_GAL);
|
||||
localFuel.forwardAux1 = min(MAX_FWD_AUX_GAL, targetFuel->forwardAux1 / LBS_PER_GAL);
|
||||
localFuel.forwardAux2 = min(MAX_FWD_AUX_GAL, targetFuel->forwardAux2 / LBS_PER_GAL);
|
||||
|
||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_FUEL_SET, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
|
||||
sizeof(FuelDataSet_t), &localFuel);
|
||||
}
|
||||
File diff suppressed because it is too large
Load Diff
@@ -0,0 +1,49 @@
|
||||
#include "log.h"
|
||||
|
||||
void toLog(FILE *file, const char *format, double *optional) {
|
||||
static FILE *logFile;
|
||||
static bool logFileFailed = false;
|
||||
|
||||
if (logFile == NULL) {
|
||||
logFile = fopen("\\work\\toLog.txt", "w");
|
||||
if (logFile == NULL) {
|
||||
logFileFailed = true;
|
||||
|
||||
toLog(stderr, "Error creating logfile.\n");
|
||||
} else {
|
||||
toLog(stdout, "Logfile created.\n");
|
||||
}
|
||||
}
|
||||
|
||||
if (!logFileFailed) {
|
||||
time_t rawtime;
|
||||
time(&rawtime);
|
||||
|
||||
char *_new = (char *)calloc(strlen(format) + 24 + 1, sizeof(char));
|
||||
if (_new == NULL) {
|
||||
fprintf(stderr, MODULE_NAME "Failed to allocate string for toLog.\n");
|
||||
return;
|
||||
}
|
||||
|
||||
strftime(_new, 24, "%FT%TZ | ", gmtime(&rawtime));
|
||||
strncat(_new, format, strlen(format));
|
||||
if (optional != nullptr) fprintf(logFile, _new, *optional);
|
||||
else
|
||||
fprintf(logFile, _new);
|
||||
fflush(logFile);
|
||||
free(_new);
|
||||
}
|
||||
|
||||
char *_new = (char *)calloc(strlen(format) + strlen(MODULE_NAME) + 1, sizeof(char));
|
||||
if (_new == NULL) {
|
||||
fprintf(stderr, MODULE_NAME "Failed to allocate string for internal console.\n");
|
||||
return;
|
||||
}
|
||||
|
||||
strncpy(_new, MODULE_NAME, strlen(MODULE_NAME));
|
||||
strncat(_new, format, strlen(format));
|
||||
if (optional != nullptr) fprintf(file, _new, *optional);
|
||||
else
|
||||
fprintf(file, _new);
|
||||
free(_new);
|
||||
}
|
||||
@@ -0,0 +1,333 @@
|
||||
#include "pax.h"
|
||||
|
||||
// ZFW Entry, fill pax first (pax+bag), rest is cargo
|
||||
void distribute(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
|
||||
const UserData_t *const userData, const UserOptions_t *const userOptions) {
|
||||
// Find payload, num pax and extra cargo
|
||||
double payload = ZFWTarget - targetPayload->empty - targetPayload->pilot - targetPayload->firstOfficer -
|
||||
targetPayload->engineer - targetPayload->cabinCrewFront - targetPayload->cabinCrewRear -
|
||||
targetPayload->leftAux - targetPayload->rightAux;
|
||||
unsigned short numPax = max(0.0, min((double)MAX_PAX, floor(payload / (PAX_WEIGHT(userData->isImperial, userOptions) +
|
||||
BAG_WEIGHT(userData->isImperial, userOptions)))));
|
||||
unsigned int cargo = round(payload - numPax * PAX_WEIGHT(userData->isImperial, userOptions) -
|
||||
numPax * BAG_WEIGHT(userData->isImperial, userOptions));
|
||||
|
||||
distribute(targetPayload, fuel, numPax, cargo, userData, userOptions);
|
||||
}
|
||||
|
||||
// SimBrief Entry, SB pax count and extra cargo
|
||||
void distribute(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned short numPax, unsigned int cargo,
|
||||
const UserData_t *const userData, const UserOptions_t *const userOptions) {
|
||||
// Clear
|
||||
targetPayload->paxCount.business1 = targetPayload->paxCount.business2 = targetPayload->paxCount.economy1 =
|
||||
targetPayload->paxCount.economy2 = targetPayload->paxCount.total = 0;
|
||||
targetPayload->forwardCargo = targetPayload->rearCargo = 0;
|
||||
|
||||
unsigned short _numPax = 0;
|
||||
unsigned int count = MAX_PAX;
|
||||
// Initial distribution pax + bags
|
||||
while (numPax > 0 && count > 0) {
|
||||
if (numPax >= 4) {
|
||||
if (targetPayload->paxCount.business1 < MAX_BUSINESS_1) {
|
||||
targetPayload->paxCount.business1++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
|
||||
targetPayload->paxCount.business2++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
|
||||
targetPayload->paxCount.economy1++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
|
||||
targetPayload->paxCount.economy2++;
|
||||
_numPax++;
|
||||
}
|
||||
} else if (numPax == 3) {
|
||||
if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
|
||||
targetPayload->paxCount.business2++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
|
||||
targetPayload->paxCount.economy1++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
|
||||
targetPayload->paxCount.economy2++;
|
||||
_numPax++;
|
||||
}
|
||||
} else if (numPax == 2) {
|
||||
if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
|
||||
targetPayload->paxCount.economy1++;
|
||||
_numPax++;
|
||||
}
|
||||
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
|
||||
targetPayload->paxCount.economy2++;
|
||||
_numPax++;
|
||||
}
|
||||
} else if (numPax == 1) {
|
||||
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
|
||||
targetPayload->paxCount.economy2++;
|
||||
_numPax++;
|
||||
}
|
||||
}
|
||||
numPax -= _numPax;
|
||||
targetPayload->paxCount.total += _numPax;
|
||||
|
||||
if (_numPax % 2 == 0) {
|
||||
targetPayload->forwardCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
targetPayload->rearCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
} else {
|
||||
_numPax--;
|
||||
targetPayload->forwardCargo += (_numPax / 2 + 1) * BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
targetPayload->rearCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
}
|
||||
|
||||
_numPax = 0;
|
||||
|
||||
count--;
|
||||
}
|
||||
count = MAX_FRONT_CARGO(userData->isImperial);
|
||||
// Initial distribution of remaining cargo
|
||||
while (cargo > 0 && count > 0) {
|
||||
if (targetPayload->forwardCargo < MAX_FRONT_CARGO(userData->isImperial)) {
|
||||
targetPayload->forwardCargo++;
|
||||
cargo--;
|
||||
}
|
||||
if (targetPayload->rearCargo < MAX_REAR_CARGO(userData->isImperial, userData->isER) && cargo > 0) {
|
||||
targetPayload->rearCargo++;
|
||||
cargo--;
|
||||
}
|
||||
|
||||
count--;
|
||||
}
|
||||
// Refinement pax
|
||||
count = MAX_PAX;
|
||||
|
||||
unsigned char minBusiness1 = round(targetPayload->paxCount.business1 / 3);
|
||||
unsigned char minBusiness2 = round(targetPayload->paxCount.business2 / 3);
|
||||
unsigned char minEconomy1 = round(targetPayload->paxCount.economy1 / 3);
|
||||
unsigned char minEconomy2 = round(targetPayload->paxCount.economy2 / 3);
|
||||
|
||||
while (count > 0) {
|
||||
generatePayload(targetPayload, userData->isImperial, userOptions);
|
||||
calculateCGs(targetPayload, fuel, userData->isImperial);
|
||||
|
||||
// in front of target
|
||||
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
|
||||
if (targetPayload->paxCount.business1 > minBusiness1) {
|
||||
targetPayload->paxCount.business1--;
|
||||
} else if (targetPayload->paxCount.business2 > minBusiness2) {
|
||||
targetPayload->paxCount.business2--;
|
||||
} else if (targetPayload->paxCount.economy1 > minEconomy1) {
|
||||
targetPayload->paxCount.economy1--;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
|
||||
targetPayload->paxCount.economy2++;
|
||||
} else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
|
||||
targetPayload->paxCount.economy1++;
|
||||
} else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
|
||||
targetPayload->paxCount.business2++;
|
||||
} else {
|
||||
targetPayload->paxCount.business1++;
|
||||
}
|
||||
}
|
||||
// behind target
|
||||
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
|
||||
if (targetPayload->paxCount.economy2 > minEconomy2) {
|
||||
targetPayload->paxCount.economy2--;
|
||||
} else if (targetPayload->paxCount.economy1 > minEconomy1) {
|
||||
targetPayload->paxCount.economy1--;
|
||||
} else if (targetPayload->paxCount.business2 > minBusiness2) {
|
||||
targetPayload->paxCount.business2--;
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
if (targetPayload->paxCount.business1 < MAX_BUSINESS_1) {
|
||||
targetPayload->paxCount.business1++;
|
||||
} else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
|
||||
targetPayload->paxCount.business2++;
|
||||
} else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
|
||||
targetPayload->paxCount.economy1++;
|
||||
} else {
|
||||
targetPayload->paxCount.economy2++;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
count--;
|
||||
}
|
||||
// Refinement cargo
|
||||
count = MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
|
||||
while (count > 0) {
|
||||
generatePayload(targetPayload, userData->isImperial, userOptions);
|
||||
calculateCGs(targetPayload, fuel, userData->isImperial);
|
||||
|
||||
// in front of target
|
||||
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
|
||||
if (targetPayload->forwardCargo > 0 && targetPayload->rearCargo < MAX_REAR_CARGO(userData->isImperial, userData->isER)) {
|
||||
if (targetPayload->forwardCargo > BAG_WEIGHT(userData->isImperial, userOptions) &&
|
||||
targetPayload->rearCargo < MAX_FRONT_CARGO(userData->isImperial) - BAG_WEIGHT(userData->isImperial, userOptions)) {
|
||||
targetPayload->forwardCargo -= BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
targetPayload->rearCargo += BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
} else {
|
||||
targetPayload->forwardCargo--;
|
||||
targetPayload->rearCargo++;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
}
|
||||
// behind target
|
||||
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
|
||||
if (targetPayload->rearCargo > 0 && targetPayload->forwardCargo < MAX_FRONT_CARGO(userData->isImperial)) {
|
||||
if (targetPayload->rearCargo > BAG_WEIGHT(userData->isImperial, userOptions) &&
|
||||
targetPayload->forwardCargo <
|
||||
MAX_REAR_CARGO(userData->isImperial, userData->isER) - BAG_WEIGHT(userData->isImperial, userOptions)) {
|
||||
targetPayload->rearCargo -= BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
targetPayload->forwardCargo += BAG_WEIGHT(userData->isImperial, userOptions);
|
||||
} else {
|
||||
targetPayload->rearCargo--;
|
||||
targetPayload->forwardCargo++;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
} else {
|
||||
break;
|
||||
}
|
||||
|
||||
count--;
|
||||
}
|
||||
}
|
||||
|
||||
// Updates pax stations with their respective weights
|
||||
// Used internally and used for Station Entry (pax only, cargo is set directly)
|
||||
void generatePayload(paxPayloadData_t *const targetPayload, const bool isImperial, const UserOptions_t *const userOptions) {
|
||||
targetPayload->business1Left = targetPayload->business1Center = targetPayload->business1Right =
|
||||
(targetPayload->paxCount.business1 / 3.0) * PAX_WEIGHT(isImperial, userOptions);
|
||||
targetPayload->business2Left = targetPayload->business2Center = targetPayload->business2Right =
|
||||
(targetPayload->paxCount.business2 / 3.0) * PAX_WEIGHT(isImperial, userOptions);
|
||||
targetPayload->economy1Left = targetPayload->economy1Center = targetPayload->economy1Right =
|
||||
(targetPayload->paxCount.economy1 / 3.0) * PAX_WEIGHT(isImperial, userOptions);
|
||||
targetPayload->economy2Left = targetPayload->economy2Center = targetPayload->economy2Right =
|
||||
(targetPayload->paxCount.economy2 / 3.0) * PAX_WEIGHT(isImperial, userOptions);
|
||||
targetPayload->total = targetPayload->empty + targetPayload->pilot + targetPayload->firstOfficer + targetPayload->engineer +
|
||||
targetPayload->cabinCrewFront + targetPayload->business1Left + targetPayload->business1Center +
|
||||
targetPayload->business1Right + targetPayload->business2Left + targetPayload->business2Center +
|
||||
targetPayload->business2Right + targetPayload->economy1Left + targetPayload->economy1Center +
|
||||
targetPayload->economy1Right + targetPayload->economy2Left + targetPayload->economy2Center +
|
||||
targetPayload->economy2Right + targetPayload->cabinCrewRear + targetPayload->forwardCargo +
|
||||
targetPayload->rearCargo + targetPayload->leftAux + targetPayload->rightAux;
|
||||
}
|
||||
|
||||
// Normalise to Pounds
|
||||
// MANDATORY BEFORE SETTING WEIGHTS
|
||||
// USE ON COPY OF GLOBAL STATE ONLY
|
||||
void normalisePayload(paxPayloadData_t *const targetPayload, const bool isImperial) {
|
||||
targetPayload->empty = TO_POUNDS(isImperial, targetPayload->empty);
|
||||
targetPayload->pilot = TO_POUNDS(isImperial, targetPayload->pilot);
|
||||
targetPayload->firstOfficer = TO_POUNDS(isImperial, targetPayload->firstOfficer);
|
||||
targetPayload->engineer = TO_POUNDS(isImperial, targetPayload->engineer);
|
||||
targetPayload->cabinCrewFront = TO_POUNDS(isImperial, targetPayload->cabinCrewFront);
|
||||
targetPayload->business1Left = TO_POUNDS(isImperial, targetPayload->business1Left);
|
||||
targetPayload->business1Center = TO_POUNDS(isImperial, targetPayload->business1Center);
|
||||
targetPayload->business1Right = TO_POUNDS(isImperial, targetPayload->business1Right);
|
||||
targetPayload->business2Left = TO_POUNDS(isImperial, targetPayload->business2Left);
|
||||
targetPayload->business2Center = TO_POUNDS(isImperial, targetPayload->business2Center);
|
||||
targetPayload->business2Right = TO_POUNDS(isImperial, targetPayload->business2Right);
|
||||
targetPayload->economy1Left = TO_POUNDS(isImperial, targetPayload->economy1Left);
|
||||
targetPayload->economy1Center = TO_POUNDS(isImperial, targetPayload->economy1Center);
|
||||
targetPayload->economy1Right = TO_POUNDS(isImperial, targetPayload->economy1Right);
|
||||
targetPayload->economy2Left = TO_POUNDS(isImperial, targetPayload->economy2Left);
|
||||
targetPayload->economy2Center = TO_POUNDS(isImperial, targetPayload->economy2Center);
|
||||
targetPayload->economy2Right = TO_POUNDS(isImperial, targetPayload->economy2Right);
|
||||
targetPayload->cabinCrewRear = TO_POUNDS(isImperial, targetPayload->cabinCrewRear);
|
||||
targetPayload->forwardCargo = TO_POUNDS(isImperial, targetPayload->forwardCargo);
|
||||
targetPayload->rearCargo = TO_POUNDS(isImperial, targetPayload->rearCargo);
|
||||
targetPayload->leftAux = TO_POUNDS(isImperial, targetPayload->leftAux);
|
||||
targetPayload->rightAux = TO_POUNDS(isImperial, targetPayload->rightAux);
|
||||
}
|
||||
|
||||
void calculateCGs(paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial) {
|
||||
paxPayloadData_t localPayload = {};
|
||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
||||
normalisePayload(&localPayload, isImperial);
|
||||
|
||||
double totalMoment =
|
||||
localPayload.empty * ARM_EMPTY + localPayload.pilot * ARM_PILOT + localPayload.firstOfficer * ARM_FIRST_OFFICER +
|
||||
localPayload.engineer * ARM_ENGINEER + localPayload.cabinCrewFront * ARM_PAX_CABIN_CREW_FRONT +
|
||||
localPayload.business1Left * ARM_PAX_BUSINESS1_LEFT + localPayload.business1Center * ARM_PAX_BUSINESS1_CENTER +
|
||||
localPayload.business1Right * ARM_PAX_BUSINESS1_RIGHT + localPayload.business2Left * ARM_PAX_BUSINESS2_LEFT +
|
||||
localPayload.business2Center * ARM_PAX_BUSINESS2_CENTER + localPayload.business2Right * ARM_PAX_BUSINESS2_RIGHT +
|
||||
localPayload.economy1Left * ARM_PAX_ECONOMY1_LEFT + localPayload.economy1Center * ARM_PAX_ECONOMY1_CENTER +
|
||||
localPayload.economy1Right * ARM_PAX_ECONOMY1_RIGHT + localPayload.economy2Left * ARM_PAX_ECONOMY2_LEFT +
|
||||
localPayload.economy2Center * ARM_PAX_ECONOMY2_CENTER + localPayload.economy2Right * ARM_PAX_ECONOMY2_RIGHT +
|
||||
localPayload.cabinCrewRear * ARM_PAX_CABIN_CREW_REAR + localPayload.forwardCargo * ARM_FORWARD_CARGO +
|
||||
localPayload.rearCargo * ARM_REAR_CARGO + localPayload.leftAux * ARM_LEFT_AUX + localPayload.rightAux * ARM_RIGHT_AUX;
|
||||
|
||||
double totalWeight = localPayload.empty + localPayload.pilot + localPayload.firstOfficer + localPayload.engineer +
|
||||
localPayload.cabinCrewFront + localPayload.business1Left + localPayload.business1Center +
|
||||
localPayload.business1Right + localPayload.business2Left + localPayload.business2Center +
|
||||
localPayload.business2Right + localPayload.economy1Left + localPayload.economy1Center +
|
||||
localPayload.economy1Right + localPayload.economy2Left + localPayload.economy2Center +
|
||||
localPayload.economy2Right + localPayload.cabinCrewRear + localPayload.forwardCargo +
|
||||
localPayload.rearCargo + localPayload.leftAux + localPayload.rightAux;
|
||||
|
||||
targetPayload->ZFWCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
||||
|
||||
totalMoment += fuel->main1 * ARM_MAIN1 + fuel->main3 * ARM_MAIN3 + fuel->main2 * ARM_MAIN2 + fuel->upperAux * ARM_UPPER_AUX +
|
||||
fuel->lowerAux * ARM_LOWER_AUX + fuel->main1Tip * ARM_MAIN1_TIP + fuel->main3Tip * ARM_MAIN3_TIP +
|
||||
fuel->tail * ARM_TAIL + fuel->forwardAux1 * ARM_FORWARD_AUX1 + fuel->forwardAux2 * ARM_FORWARD_AUX2;
|
||||
|
||||
totalWeight += fuel->total;
|
||||
|
||||
targetPayload->TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
||||
}
|
||||
|
||||
void load(const paxPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
|
||||
const bool isImperial) {
|
||||
paxPayloadData_t localPayload = {};
|
||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
||||
normalisePayload(&localPayload, isImperial);
|
||||
|
||||
calculateCGs(&localPayload, fuel, isImperial);
|
||||
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
|
||||
|
||||
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
|
||||
|
||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
|
||||
sizeof(paxPayloadDataSet_t), &localPayload);
|
||||
}
|
||||
|
||||
void unload(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER) {
|
||||
paxPayloadData_t localPayload = {};
|
||||
|
||||
localPayload.empty = empty;
|
||||
localPayload.cabinCrewFront = FRONT_CREW_WEIGHT(true);
|
||||
localPayload.cabinCrewRear = REAR_CREW_WEIGHT(true);
|
||||
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
|
||||
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
|
||||
|
||||
calculateCGs(&localPayload, fuel, true);
|
||||
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
|
||||
|
||||
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
|
||||
|
||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
|
||||
sizeof(paxPayloadDataSet_t), &localPayload);
|
||||
}
|
||||
|
||||
double PAX_WEIGHT(const bool isImperial, const UserOptions_t *const options) {
|
||||
return (isImperial) ? (options->paxWeightLBS) : (options->paxWeightKG);
|
||||
}
|
||||
|
||||
double BAG_WEIGHT(const bool isImperial, const UserOptions_t *const options) {
|
||||
return (isImperial) ? (options->bagWeightLBS) : (options->bagWeightKG);
|
||||
}
|
||||
@@ -0,0 +1,64 @@
|
||||
const fs = require('fs');
|
||||
const path = require('path');
|
||||
|
||||
const BASE_DIRS = ['.'];
|
||||
|
||||
let THRESHOLD = parseInt(process.argv.at(-1) ?? 2048);
|
||||
THRESHOLD = isNaN(THRESHOLD) ? 2048 : THRESHOLD;
|
||||
console.log(`Threshold at ${THRESHOLD} bytes`);
|
||||
let LEVEL =
|
||||
process.argv.includes('--level') ? process.argv[process.argv.findIndex((p) => p === '--level') + 1] : undefined;
|
||||
if (LEVEL !== 'info') LEVEL = undefined;
|
||||
console.log(`Log level ${LEVEL ?? 'default'}`);
|
||||
|
||||
BASE_DIRS.forEach((BASE_DIR) => {
|
||||
console.log(`Analysis for ${BASE_DIR}`);
|
||||
|
||||
const output = fs.openSync(path.join(BASE_DIR, 'stack-analysis.log'), 'w');
|
||||
|
||||
let functions = [];
|
||||
|
||||
let files = fs.readdirSync(BASE_DIR);
|
||||
files = files.filter((file) => file.endsWith('.su'));
|
||||
files.forEach((file) => {
|
||||
const content = fs.readFileSync(path.join(BASE_DIR, file), {
|
||||
encoding: 'utf8',
|
||||
});
|
||||
|
||||
const _functions = content.split('\n');
|
||||
_functions.forEach((_function) => {
|
||||
const fields = _function.split('\t');
|
||||
|
||||
if (fields.length != 3) return;
|
||||
|
||||
functions.push({
|
||||
name: fields[0],
|
||||
cost: parseInt(fields[1]),
|
||||
type: fields[2],
|
||||
});
|
||||
});
|
||||
|
||||
fs.unlinkSync(path.join(BASE_DIR, file));
|
||||
});
|
||||
|
||||
functions = functions.sort((a, b) => b.cost - a.cost);
|
||||
functions.forEach((_function) => {
|
||||
if (_function.cost === THRESHOLD) {
|
||||
console.warn(
|
||||
`\x1b[33mFunction \x1b[1m${_function.name}\x1b[0m \x1b[33mat threshold (\x1b[1m${_function.cost}\x1b[0m\x1b[33m)\x1b[0m`
|
||||
);
|
||||
} else if (_function.cost >= THRESHOLD) {
|
||||
console.error(
|
||||
`\x1b[31mFunction \x1b[1m${_function.name}\x1b[0m \x1b[31mexceeds threshold (\x1b[1m${_function.cost}\x1b[0m\x1b[31m)\x1b[0m`
|
||||
);
|
||||
} else if (LEVEL === 'info') {
|
||||
console.error(
|
||||
`\x1b[32mFunction \x1b[1m${_function.name}\x1b[0m \x1b[32mbelow threshold (\x1b[1m${_function.cost}\x1b[0m\x1b[32m)\x1b[0m`
|
||||
);
|
||||
}
|
||||
|
||||
fs.writeSync(output, `${_function.cost}\t${_function.type}\t${_function.name}\n`, null, { encoding: 'utf8' });
|
||||
});
|
||||
|
||||
fs.closeSync(output);
|
||||
});
|
||||
@@ -1,6 +1,12 @@
|
||||
# How to build
|
||||
|
||||
Build WASM module from VS
|
||||
`pnpm build` from `js-bundle`
|
||||
Build in sim
|
||||
|
||||
# Sources
|
||||
|
||||
- https://www.boeing.com/content/dam/boeing/boeingdotcom/company/about_bca/startup/pdf/freighters/MD11BCF.pdf
|
||||
- LAMM
|
||||
- https://www.satco-inc.com/product-pallet/?part_number=31086-595
|
||||
- https://www.satco-inc.com/product-container/?part_number=34124-901
|
||||
- https://www.satco-inc.com/product-container/?part_number=34124-901
|
||||
|
||||
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Reference in New Issue
Block a user