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15 Commits
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master
| Author | SHA1 | Date | |
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 Kilian
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Kilian
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Kilian
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Kilian
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Kilian
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Kilian
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Kilian
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Kilian
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ec9facd4d9 |
@@ -0,0 +1,6 @@
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|||||||
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---
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||||||
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BasedOnStyle: LLVM
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||||||
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ColumnLimit: 130
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||||||
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IndentCaseLabels: true
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||||||
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AllowShortIfStatementsOnASingleLine: Always
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||||||
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AllowShortLoopsOnASingleLine: true
|
||||||
+367
-4
@@ -1,20 +1,383 @@
|
|||||||
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## Ignore Visual Studio temporary files, build results, and
|
||||||
|
## files generated by popular Visual Studio add-ons.
|
||||||
|
##
|
||||||
|
## Get latest from https://github.com/github/gitignore/blob/master/VisualStudio.gitignore
|
||||||
|
|
||||||
|
# User-specific files
|
||||||
|
*.rsuser
|
||||||
|
*.suo
|
||||||
|
*.user
|
||||||
|
*.userosscache
|
||||||
|
*.sln.docstates
|
||||||
|
|
||||||
|
# User-specific files (MonoDevelop/Xamarin Studio)
|
||||||
|
*.userprefs
|
||||||
|
|
||||||
|
# Mono auto generated files
|
||||||
|
mono_crash.*
|
||||||
|
|
||||||
|
# Build results
|
||||||
|
[Dd]ebug/
|
||||||
|
[Dd]ebugPublic/
|
||||||
|
[Rr]elease/
|
||||||
|
[Rr]eleases/
|
||||||
|
x64/
|
||||||
|
x86/
|
||||||
|
[Ww][Ii][Nn]32/
|
||||||
|
[Aa][Rr][Mm]/
|
||||||
|
[Aa][Rr][Mm]64/
|
||||||
|
bld/
|
||||||
|
[Bb]in/
|
||||||
|
[Oo]bj/
|
||||||
|
[Oo]ut/
|
||||||
|
[Ll]og/
|
||||||
|
[Ll]ogs/
|
||||||
|
|
||||||
|
# Visual Studio 2015/2017 cache/options directory
|
||||||
|
.vs/
|
||||||
|
# Uncomment if you have tasks that create the project's static files in wwwroot
|
||||||
|
#wwwroot/
|
||||||
|
|
||||||
|
# Visual Studio 2017 auto generated files
|
||||||
|
Generated\ Files/
|
||||||
|
|
||||||
|
# MSTest test Results
|
||||||
|
[Tt]est[Rr]esult*/
|
||||||
|
[Bb]uild[Ll]og.*
|
||||||
|
|
||||||
|
# NUnit
|
||||||
|
*.VisualState.xml
|
||||||
|
TestResult.xml
|
||||||
|
nunit-*.xml
|
||||||
|
|
||||||
|
# Build Results of an ATL Project
|
||||||
|
[Dd]ebugPS/
|
||||||
|
[Rr]eleasePS/
|
||||||
|
dlldata.c
|
||||||
|
|
||||||
|
# Benchmark Results
|
||||||
|
BenchmarkDotNet.Artifacts/
|
||||||
|
|
||||||
|
# .NET Core
|
||||||
|
project.lock.json
|
||||||
|
project.fragment.lock.json
|
||||||
|
artifacts/
|
||||||
|
|
||||||
|
# ASP.NET Scaffolding
|
||||||
|
ScaffoldingReadMe.txt
|
||||||
|
|
||||||
|
# StyleCop
|
||||||
|
StyleCopReport.xml
|
||||||
|
|
||||||
|
# Files built by Visual Studio
|
||||||
|
*_i.c
|
||||||
|
*_p.c
|
||||||
|
*_h.h
|
||||||
|
*.ilk
|
||||||
|
*.meta
|
||||||
|
*.obj
|
||||||
|
*.iobj
|
||||||
|
*.pch
|
||||||
|
*.pdb
|
||||||
|
*.ipdb
|
||||||
|
*.pgc
|
||||||
|
*.pgd
|
||||||
|
*.rsp
|
||||||
|
*.sbr
|
||||||
|
*.tlb
|
||||||
|
*.tli
|
||||||
|
*.tlh
|
||||||
|
*.tmp
|
||||||
|
*.tmp_proj
|
||||||
|
*_wpftmp.csproj
|
||||||
|
*.log
|
||||||
|
*.vspscc
|
||||||
|
*.vssscc
|
||||||
|
.builds
|
||||||
|
*.pidb
|
||||||
|
*.svclog
|
||||||
|
*.scc
|
||||||
|
|
||||||
|
# Chutzpah Test files
|
||||||
|
_Chutzpah*
|
||||||
|
|
||||||
|
# Visual C++ cache files
|
||||||
|
ipch/
|
||||||
|
*.aps
|
||||||
|
*.ncb
|
||||||
|
*.opendb
|
||||||
|
*.opensdf
|
||||||
|
*.sdf
|
||||||
|
*.cachefile
|
||||||
|
*.VC.db
|
||||||
|
*.VC.VC.opendb
|
||||||
|
|
||||||
|
# Visual Studio profiler
|
||||||
|
*.psess
|
||||||
|
*.vsp
|
||||||
|
*.vspx
|
||||||
|
*.sap
|
||||||
|
|
||||||
|
# Visual Studio Trace Files
|
||||||
|
*.e2e
|
||||||
|
|
||||||
|
# TFS 2012 Local Workspace
|
||||||
|
$tf/
|
||||||
|
|
||||||
|
# Guidance Automation Toolkit
|
||||||
|
*.gpState
|
||||||
|
|
||||||
|
# ReSharper is a .NET coding add-in
|
||||||
|
_ReSharper*/
|
||||||
|
*.[Rr]e[Ss]harper
|
||||||
|
*.DotSettings.user
|
||||||
|
|
||||||
|
# TeamCity is a build add-in
|
||||||
|
_TeamCity*
|
||||||
|
|
||||||
|
# DotCover is a Code Coverage Tool
|
||||||
|
*.dotCover
|
||||||
|
|
||||||
|
# AxoCover is a Code Coverage Tool
|
||||||
|
.axoCover/*
|
||||||
|
!.axoCover/settings.json
|
||||||
|
|
||||||
|
# Coverlet is a free, cross platform Code Coverage Tool
|
||||||
|
coverage*.json
|
||||||
|
coverage*.xml
|
||||||
|
coverage*.info
|
||||||
|
|
||||||
|
# Visual Studio code coverage results
|
||||||
|
*.coverage
|
||||||
|
*.coveragexml
|
||||||
|
|
||||||
|
# NCrunch
|
||||||
|
_NCrunch_*
|
||||||
|
.*crunch*.local.xml
|
||||||
|
nCrunchTemp_*
|
||||||
|
|
||||||
|
# MightyMoose
|
||||||
|
*.mm.*
|
||||||
|
AutoTest.Net/
|
||||||
|
|
||||||
|
# Web workbench (sass)
|
||||||
|
.sass-cache/
|
||||||
|
|
||||||
|
# Installshield output folder
|
||||||
|
[Ee]xpress/
|
||||||
|
|
||||||
|
# DocProject is a documentation generator add-in
|
||||||
|
DocProject/buildhelp/
|
||||||
|
DocProject/Help/*.HxT
|
||||||
|
DocProject/Help/*.HxC
|
||||||
|
DocProject/Help/*.hhc
|
||||||
|
DocProject/Help/*.hhk
|
||||||
|
DocProject/Help/*.hhp
|
||||||
|
DocProject/Help/Html2
|
||||||
|
DocProject/Help/html
|
||||||
|
|
||||||
|
# Click-Once directory
|
||||||
|
publish/
|
||||||
|
|
||||||
|
# Publish Web Output
|
||||||
|
*.[Pp]ublish.xml
|
||||||
|
*.azurePubxml
|
||||||
|
# Note: Comment the next line if you want to checkin your web deploy settings,
|
||||||
|
# but database connection strings (with potential passwords) will be unencrypted
|
||||||
|
*.pubxml
|
||||||
|
*.publishproj
|
||||||
|
|
||||||
|
# Microsoft Azure Web App publish settings. Comment the next line if you want to
|
||||||
|
# checkin your Azure Web App publish settings, but sensitive information contained
|
||||||
|
# in these scripts will be unencrypted
|
||||||
|
PublishScripts/
|
||||||
|
|
||||||
|
# NuGet Packages
|
||||||
|
*.nupkg
|
||||||
|
# NuGet Symbol Packages
|
||||||
|
*.snupkg
|
||||||
|
# The packages folder can be ignored because of Package Restore
|
||||||
|
**/[Pp]ackages/*
|
||||||
|
# except build/, which is used as an MSBuild target.
|
||||||
|
!**/[Pp]ackages/build/
|
||||||
|
# Uncomment if necessary however generally it will be regenerated when needed
|
||||||
|
#!**/[Pp]ackages/repositories.config
|
||||||
|
# NuGet v3's project.json files produces more ignorable files
|
||||||
|
*.nuget.props
|
||||||
|
*.nuget.targets
|
||||||
|
|
||||||
|
# Microsoft Azure Build Output
|
||||||
|
csx/
|
||||||
|
*.build.csdef
|
||||||
|
|
||||||
|
# Microsoft Azure Emulator
|
||||||
|
ecf/
|
||||||
|
rcf/
|
||||||
|
|
||||||
|
# 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*/
|
||||||
|
UpgradeLog*.XML
|
||||||
|
UpgradeLog*.htm
|
||||||
|
ServiceFabricBackup/
|
||||||
|
*.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/
|
||||||
|
|
||||||
|
# Fody - auto-generated XML schema
|
||||||
|
FodyWeavers.xsda
|
||||||
|
|
||||||
|
# Custom
|
||||||
|
|
||||||
Packages
|
Packages
|
||||||
_PackageInt
|
_PackageInt
|
||||||
PackagesMetadata
|
PackagesMetadata
|
||||||
PackageSources/js-bundle/__generated__
|
PackageSources/js-bundle/__generated__
|
||||||
PackageSources/js-bundle/.rollup.cache
|
PackageSources/js-bundle/.rollup.cache
|
||||||
PackageSources/js-bundle/node_modules
|
|
||||||
PackageSources/html_ui
|
PackageSources/html_ui
|
||||||
PackageSources/wasm-module/.vs
|
|
||||||
PackageSources/wasm-module/MSFS
|
PackageSources/wasm-module/MSFS
|
||||||
PackageSources/wasm-module/x64
|
|
||||||
|
|
||||||
node_modules
|
node_modules
|
||||||
|
|
||||||
*.blend1
|
*.blend1
|
||||||
*.tsbuildinfo
|
*.tsbuildinfo
|
||||||
|
|
||||||
PackageSources/SimObjects/Airplanes/**/panel/*.wasm
|
PackageSources/SimObjects/Airplanes/**/*.wasm
|
||||||
EFB/efb.css
|
EFB/efb.css
|
||||||
EFB/efb.js
|
EFB/efb.js
|
||||||
EFB/efb.html
|
EFB/efb.html
|
||||||
|
|||||||
Vendored
+29
@@ -0,0 +1,29 @@
|
|||||||
|
{
|
||||||
|
"configurations": [
|
||||||
|
{
|
||||||
|
"name": "Win32",
|
||||||
|
"includePath": [
|
||||||
|
"${workspaceFolder}/**",
|
||||||
|
"${workspaceFolder}/.vscode",
|
||||||
|
"C:\\MSFS 2024 SDK\\WASM\\wasi-sysroot\\include",
|
||||||
|
"C:\\MSFS 2024 SDK\\WASM\\wasi-sysroot\\include\\c++\\v1",
|
||||||
|
"C:\\MSFS 2024 SDK\\WASM\\include",
|
||||||
|
"C:\\MSFS 2024 SDK\\SimConnect SDK\\include"
|
||||||
|
],
|
||||||
|
"defines": [
|
||||||
|
"_DEBUG",
|
||||||
|
"UNICODE",
|
||||||
|
"_UNICODE"
|
||||||
|
],
|
||||||
|
"compilerArgs": [
|
||||||
|
"/Zc:__cplusplus"
|
||||||
|
],
|
||||||
|
"windowsSdkVersion": "10.0.26100.0",
|
||||||
|
"compilerPath": "cl.exe",
|
||||||
|
"cStandard": "c17",
|
||||||
|
"intelliSenseMode": "windows-msvc-x64",
|
||||||
|
"cppStandard": "c++14"
|
||||||
|
}
|
||||||
|
],
|
||||||
|
"version": 4
|
||||||
|
}
|
||||||
Vendored
+3
@@ -18,5 +18,8 @@
|
|||||||
},
|
},
|
||||||
"[xml]": {
|
"[xml]": {
|
||||||
"editor.defaultFormatter": "redhat.vscode-xml"
|
"editor.defaultFormatter": "redhat.vscode-xml"
|
||||||
|
},
|
||||||
|
"[typescriptreact]": {
|
||||||
|
"editor.defaultFormatter": "esbenp.prettier-vscode"
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
+1
-2
@@ -10,6 +10,5 @@ Index: EFB.html
|
|||||||
-<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/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>
|
+<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" />
|
<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.css" />
|
||||||
+<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/efb.css" />
|
|
||||||
+<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.css" />
|
+<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.css" />
|
||||||
|
|||||||
+16
-13
@@ -2,23 +2,26 @@ Index: EFB.js
|
|||||||
===================================================================
|
===================================================================
|
||||||
--- EFB.js
|
--- EFB.js
|
||||||
+++ EFB.js
|
+++ EFB.js
|
||||||
@@ -30203,9 +30203,9 @@
|
@@ -50833,11 +50833,11 @@
|
||||||
{
|
),
|
||||||
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",
|
/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
|
||||||
"data-ripple-light": "true",
|
"button",
|
||||||
onClick: () => getOutput(),
|
{
|
||||||
- children: "Set Payload"
|
- onClick: loadPayload,
|
||||||
+ children: "Manage Payload"
|
+ onClick: () => dispatch(setRoute({ path: "/payload" })),
|
||||||
}
|
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",
|
||||||
) }) })
|
- children: "Set payload & fuel"
|
||||||
] }) }) });
|
+ children: "Manage payload & fuel"
|
||||||
}
|
}
|
||||||
@@ -40556,8 +40556,27 @@
|
),
|
||||||
|
/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
|
||||||
|
"button",
|
||||||
|
@@ -51343,8 +51343,27 @@
|
||||||
] })
|
] })
|
||||||
] }) }) });
|
] }) }) });
|
||||||
}
|
}
|
||||||
|
|
||||||
+ // Exports for add. script
|
+// Exports for add. script
|
||||||
+ window.reactExports = __toESM(require_react());
|
+ window.reactExports = __toESM(require_react());
|
||||||
+ window.reactDomExports = __toESM(require_react_dom());
|
+ window.reactDomExports = __toESM(require_react_dom());
|
||||||
+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
|
+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
|
||||||
|
|||||||
@@ -1,5 +1,5 @@
|
|||||||
<?xml version="1.0" encoding="utf-8"?>
|
<?xml version="1.0" encoding="utf-8"?>
|
||||||
<AssetPackage Version="0.1.0">
|
<AssetPackage Version="1.3.0">
|
||||||
<ItemSettings>
|
<ItemSettings>
|
||||||
<ContentType>MISC</ContentType>
|
<ContentType>MISC</ContentType>
|
||||||
<Title>TFDi Design MD-11 Load Manager</Title>
|
<Title>TFDi Design MD-11 Load Manager</Title>
|
||||||
@@ -10,9 +10,10 @@
|
|||||||
<VisibleInStore>false</VisibleInStore>
|
<VisibleInStore>false</VisibleInStore>
|
||||||
<CanBeReferenced>false</CanBeReferenced>
|
<CanBeReferenced>false</CanBeReferenced>
|
||||||
</Flags>
|
</Flags>
|
||||||
|
<PackageOrderHint>CUSTOM_SIMOBJECTS_PATCH</PackageOrderHint>
|
||||||
<AssetGroups>
|
<AssetGroups>
|
||||||
<AssetGroup Name="ContentInfo">
|
<AssetGroup Name="ContentInfo">
|
||||||
<Type>ContentInfo</Type>
|
<Type Version="0">ContentInfo</Type>
|
||||||
<Flags>
|
<Flags>
|
||||||
<FSXCompatibility>false</FSXCompatibility>
|
<FSXCompatibility>false</FSXCompatibility>
|
||||||
</Flags>
|
</Flags>
|
||||||
@@ -20,7 +21,7 @@
|
|||||||
<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
|
<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
|
||||||
</AssetGroup>
|
</AssetGroup>
|
||||||
<AssetGroup Name="html-ui">
|
<AssetGroup Name="html-ui">
|
||||||
<Type>Copy</Type>
|
<Type Version="0">Copy</Type>
|
||||||
<Flags>
|
<Flags>
|
||||||
<FSXCompatibility>false</FSXCompatibility>
|
<FSXCompatibility>false</FSXCompatibility>
|
||||||
</Flags>
|
</Flags>
|
||||||
@@ -30,14 +31,16 @@
|
|||||||
<Exclude>vendor-*</Exclude>
|
<Exclude>vendor-*</Exclude>
|
||||||
</Config>
|
</Config>
|
||||||
</AssetGroup>
|
</AssetGroup>
|
||||||
<AssetGroup Name="md-11-panel-config">
|
<AssetGroup Name="wasm">
|
||||||
<Type>Copy</Type>
|
<Type Version="0">Copy</Type>
|
||||||
<Flags>
|
<Flags>
|
||||||
<FSXCompatibility>false</FSXCompatibility>
|
<FSXCompatibility>false</FSXCompatibility>
|
||||||
</Flags>
|
</Flags>
|
||||||
<AssetDir>PackageSources\SimObjects\Airplanes\</AssetDir>
|
<AssetDir>PackageSources\SimObjects\Airplanes\</AssetDir>
|
||||||
<OutputDir>SimObjects\Airplanes\</OutputDir>
|
<OutputDir>SimObjects\Airplanes\</OutputDir>
|
||||||
|
<Config>
|
||||||
|
<Exclude>.gitkeep</Exclude>
|
||||||
|
</Config>
|
||||||
</AssetGroup>
|
</AssetGroup>
|
||||||
</AssetGroups>
|
</AssetGroups>
|
||||||
</AssetPackage>
|
</AssetPackage>
|
||||||
|
|
||||||
|
|||||||
+11
-11
@@ -7,17 +7,17 @@ visible=1
|
|||||||
pixel_size=2048,2048
|
pixel_size=2048,2048
|
||||||
texture=vc1
|
texture=vc1
|
||||||
background_color=0,0,0
|
background_color=0,0,0
|
||||||
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core, 0,0,509,510
|
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=DU1,0,0,508,508
|
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=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=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=DU4,1539,0,510,508
|
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=DU5,0,513,511,509
|
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=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=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=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=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=ISFD,1032,519,544,505
|
htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core,0,0,1,1
|
||||||
//KH new gauge
|
//KH new gauge
|
||||||
htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
|
htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
|
||||||
|
|
||||||
+51
-51
@@ -1,15 +1,15 @@
|
|||||||
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25
|
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 1
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 283975
|
empty_weight = 283975
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@@ -24,21 +24,21 @@ 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.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.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.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, 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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 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, 0
|
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.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
|
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||||
//KH END
|
//KH END
|
||||||
@@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||||
LeftAux = 5.00, -2.00, -3.00, 1917.00, 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
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.1889
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@@ -265,7 +265,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@@ -319,19 +319,19 @@ max_gear_extended = 200
|
|||||||
|
|
||||||
[INTERACTIVE POINTS]
|
[INTERACTIVE POINTS]
|
||||||
number_of_interactive_points = 13
|
number_of_interactive_points = 13
|
||||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0
|
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
|
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
|
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,-7.180745,1,0,0,90,0,0,0,0,0,0,0
|
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,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
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,-29.85655,42.814491,0,0,0,0,0,0,0
|
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,-42.814491,0,0,0,0,0,0,0
|
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
|
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,-0.567,0,0,0,88,35,0,35,0,2,33,0
|
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,-90,35,0,35,0,2,33,0
|
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,-0.566572,0,0,0,90,35,0,35,0,2,33,0
|
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,-100,35,0,35,0,2,33,0
|
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,-0.565611,0,0,0,100,35,0,35,0,2,33,0
|
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]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@@ -348,8 +348,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -357,12 +357,12 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
@@ -370,8 +370,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 23
|
extending-time = 23
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -379,12 +379,12 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
@@ -392,8 +392,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.2
|
span-outboard = 0.2
|
||||||
extending-time = 8
|
extending-time = 8
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@@ -407,8 +407,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
+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
|
||||||
+54
-51
@@ -1,15 +1,18 @@
|
|||||||
//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25
|
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
|
||||||
|
|
||||||
|
[MODULAR_MERGE]
|
||||||
|
auto = true
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 1
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 283975
|
empty_weight = 283975
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@@ -24,21 +27,21 @@ 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.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.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.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, 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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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, 0
|
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.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
|
||||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 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, 0
|
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.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
|
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
|
||||||
//KH END
|
//KH END
|
||||||
@@ -59,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@@ -88,9 +91,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||||
LeftAux = 5.00, -2.00, -3.00, 1917.00, 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
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@@ -175,7 +178,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.1889
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@@ -265,7 +268,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@@ -319,19 +322,19 @@ max_gear_extended = 200
|
|||||||
|
|
||||||
[INTERACTIVE POINTS]
|
[INTERACTIVE POINTS]
|
||||||
number_of_interactive_points = 13
|
number_of_interactive_points = 13
|
||||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0
|
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
|
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
|
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,-7.180745,1,0,0,90,0,0,0,0,0,0,0
|
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,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
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,-29.85655,42.814491,0,0,0,0,0,0,0
|
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,-42.814491,0,0,0,0,0,0,0
|
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
|
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,-0.567,0,0,0,88,35,0,35,0,2,33,0
|
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,-90,35,0,35,0,2,33,0
|
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,-0.566572,0,0,0,90,35,0,35,0,2,33,0
|
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,-100,35,0,35,0,2,33,0
|
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,-0.565611,0,0,0,100,35,0,35,0,2,33,0
|
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]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@@ -348,8 +351,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -357,20 +360,20 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 23
|
extending-time = 23
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -378,20 +381,20 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.2
|
span-outboard = 0.2
|
||||||
extending-time = 8
|
extending-time = 8
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@@ -405,8 +408,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
+39
-35
@@ -1,15 +1,18 @@
|
|||||||
//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
|
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
|
||||||
|
|
||||||
|
[MODULAR_MERGE]
|
||||||
|
auto = true
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 1
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@@ -20,9 +23,9 @@ activate_mach_limit_based_on_cg = 0
|
|||||||
activate_cg_limit_based_on_mach = 0
|
activate_cg_limit_based_on_mach = 0
|
||||||
max_number_of_stations = 15
|
max_number_of_stations = 15
|
||||||
//KH START Empty default
|
//KH START Empty default
|
||||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
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.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.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.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||||
@@ -53,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@@ -82,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||||
LeftAux = 5.00, -2.00, -3.00, 1917.00, 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
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.1889
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@@ -259,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@@ -313,14 +316,14 @@ max_gear_extended = 200
|
|||||||
|
|
||||||
[INTERACTIVE POINTS]
|
[INTERACTIVE POINTS]
|
||||||
number_of_interactive_points = 8
|
number_of_interactive_points = 8
|
||||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0
|
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
|
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
|
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,-7.180745,1,0,0,90,0,0,0,0,0,0,0
|
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,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
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,-29.85655,42.814491,0,0,0,0,0,0,0
|
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,-42.814491,0,0,0,0,0,0,0
|
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,-0.003025,1,0,0,0,0,0,0,0,0,0,0
|
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]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@@ -337,8 +340,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -346,20 +349,21 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 23
|
extending-time = 23
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -367,20 +371,20 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.2
|
span-outboard = 0.2
|
||||||
extending-time = 8
|
extending-time = 8
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@@ -394,8 +398,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
+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
|
||||||
+38
-35
@@ -1,15 +1,18 @@
|
|||||||
//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
|
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
|
||||||
|
|
||||||
|
[MODULAR_MERGE]
|
||||||
|
auto = true
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 1
|
minor = 8
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
empty_weight = 248567
|
empty_weight = 248567
|
||||||
reference_datum_position = 0, 0, 0
|
reference_datum_position = 0, 0, 0
|
||||||
empty_weight_CG_position = -13.3, 0, 0
|
empty_weight_CG_position = -10.0, 0, 0
|
||||||
CG_forward_limit = 0.12
|
CG_forward_limit = 0.12
|
||||||
CG_aft_limit = 0.34
|
CG_aft_limit = 0.34
|
||||||
empty_weight_pitch_MOI = 20897456
|
empty_weight_pitch_MOI = 20897456
|
||||||
@@ -20,9 +23,9 @@ activate_mach_limit_based_on_cg = 0
|
|||||||
activate_cg_limit_based_on_mach = 0
|
activate_cg_limit_based_on_mach = 0
|
||||||
max_number_of_stations = 15
|
max_number_of_stations = 15
|
||||||
//KH START Empty default
|
//KH START Empty default
|
||||||
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
||||||
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
|
station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
|
||||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
|
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.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.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.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
|
||||||
@@ -53,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
|
|||||||
emergency_extension_type = 2
|
emergency_extension_type = 2
|
||||||
hyd_need_power_to_function= 0
|
hyd_need_power_to_function= 0
|
||||||
min_castering_angle = 0.05236
|
min_castering_angle = 0.05236
|
||||||
max_castering_angle = 1.32645
|
max_castering_angle = 3.142
|
||||||
allow_stopped_steering = 1
|
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.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.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
|
||||||
@@ -82,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
|
|||||||
RightTip = -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
|
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
|
||||||
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
|
||||||
LeftAux = 5.00, -2.00, -3.00, 1917.00, 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
|
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
|
||||||
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
|
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
|
||||||
fuel_type = 2
|
fuel_type = 2
|
||||||
number_of_tank_selectors = 3
|
number_of_tank_selectors = 3
|
||||||
electric_pump = 0
|
electric_pump = 0
|
||||||
@@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
|
|||||||
lift_coef_flaps = 1
|
lift_coef_flaps = 1
|
||||||
lift_coef_spoilers = 0
|
lift_coef_spoilers = 0
|
||||||
drag_coef_zero_lift = 0.02539
|
drag_coef_zero_lift = 0.02539
|
||||||
drag_coef_flaps = 0.1889
|
drag_coef_flaps = 0.1339
|
||||||
drag_coef_gear = 0.0549
|
drag_coef_gear = 0.0549
|
||||||
drag_coef_spoilers = 0.05207
|
drag_coef_spoilers = 0.05207
|
||||||
side_force_slip_angle = -0.77392
|
side_force_slip_angle = -0.77392
|
||||||
@@ -259,7 +262,7 @@ cruise_lift_scalar = 1
|
|||||||
parasite_drag_scalar = 1
|
parasite_drag_scalar = 1
|
||||||
induced_drag_scalar = 1
|
induced_drag_scalar = 1
|
||||||
flap_induced_drag_scalar = 1
|
flap_induced_drag_scalar = 1
|
||||||
elevator_effectiveness = 1
|
elevator_effectiveness = 1.1
|
||||||
elevator_maxangle_scalar = 1
|
elevator_maxangle_scalar = 1
|
||||||
aileron_effectiveness = 1
|
aileron_effectiveness = 1
|
||||||
rudder_effectiveness = 1
|
rudder_effectiveness = 1
|
||||||
@@ -313,14 +316,14 @@ max_gear_extended = 200
|
|||||||
|
|
||||||
[INTERACTIVE POINTS]
|
[INTERACTIVE POINTS]
|
||||||
number_of_interactive_points = 8
|
number_of_interactive_points = 8
|
||||||
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0
|
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
|
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
|
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,-7.180745,1,0,0,90,0,0,0,0,0,0,0
|
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,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
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,-29.85655,42.814491,0,0,0,0,0,0,0
|
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,-42.814491,0,0,0,0,0,0,0
|
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,-0.003025,1,0,0,0,0,0,0,0,0,0,0
|
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]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@@ -337,8 +340,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -346,20 +349,20 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.1]
|
[FLAPS.1]
|
||||||
type = 1
|
type = 1
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 23
|
extending-time = 23
|
||||||
damaging-speed = 250
|
damaging-speed = 280
|
||||||
blowout-speed = 300
|
blowout-speed = 310
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@@ -367,20 +370,20 @@ pitch_scalar = 1
|
|||||||
max_on_ground_position = 7
|
max_on_ground_position = 7
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 0, -1, 0
|
flaps-position.1 = 0, -1, 0
|
||||||
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.28, 1.0, 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.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
|
||||||
flaps-position.6 = 35, 160, 0.32, 1
|
flaps-position.6 = 35, 160, 0.32, 1
|
||||||
flaps-position.7 = 50, 150, 0.33, 1
|
flaps-position.7 = 50, 155, 0.43, 1
|
||||||
|
|
||||||
[FLAPS.2]
|
[FLAPS.2]
|
||||||
type = 2
|
type = 2
|
||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.2
|
span-outboard = 0.2
|
||||||
extending-time = 8
|
extending-time = 8
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@@ -394,8 +397,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 250
|
damaging-speed = 300
|
||||||
blowout-speed = 300
|
blowout-speed = 330
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
+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
|
||||||
@@ -1,6 +1,6 @@
|
|||||||
{
|
{
|
||||||
"name": "tfdidesign-md11-load-manager",
|
"name": "js-bundle",
|
||||||
"version": "0.1.186",
|
"version": "0.2.34",
|
||||||
"description": "",
|
"description": "",
|
||||||
"main": "index.js",
|
"main": "index.js",
|
||||||
"type": "module",
|
"type": "module",
|
||||||
|
|||||||
@@ -1,40 +1,41 @@
|
|||||||
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
|
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
|
||||||
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :----------- | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
|
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :------------ | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
|
||||||
| kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.0 | 19.1.0 | ^19.1.0 | n/a |
|
| 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-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.0 | 19.1.0 | ^19.1.0 | n/a |
|
| 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 | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 11.1.0 | 11.1.0 | ^11.1.0 | 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 | @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 | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 11.1.0 | 11.1.0 | ^11.1.0 | n/a |
|
||||||
| kessler | stuff | @rollup/plugin-commonjs | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 28.0.9 | 28.0.3 | ^28.0.3 | Rich Harris <richard.a.harris@gmail.com> |
|
| 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-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-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-node-resolve | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 16.0.3 | 16.0.1 | ^16.0.1 | 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-replace | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.0.3 | 6.0.2 | ^6.0.2 | Rich Harris <richard.a.harris@gmail.com> |
|
| 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-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-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-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 12.3.0 | 12.1.2 | ^12.1.2 | Oskar Segersvärd |
|
| 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 | @types/node | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 24.10.1 | 24.3.1 | ^24.3.1 | n/a |
|
| 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/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.7 | 19.1.6 | ^19.1.6 | n/a |
|
| 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-dom | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.3 | 19.1.6 | ^19.1.6 | 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/uuid | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 10.0.0 | 10.0.0 | ^10.0.0 | 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 | @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 | @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/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 | @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 | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.22 | 10.4.21 | ^10.4.21 | Andrey Sitnik <andrey@sitnik.ru> |
|
| 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 | 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 | 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 | 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 | 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-plugin-import | perpetual | material | MIT | git+https://github.com/import-js/eslint-plugin-import.git | 2.32.0 | 2.31.0 | ^2.31.0 | Ben Mosher <me@benmosher.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-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-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-hooks | perpetual | material | MIT | git+https://github.com/facebook/react.git | 4.6.2 | 4.6.2 | ^4.6.2 | n/a |
|
| 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 | license-report | perpetual | material | MIT | git+https://github.com/kessler/license-report.git | 6.8.1 | 6.7.2 | ^6.7.2 | Yaniv Kessler |
|
| 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 | postcss | perpetual | material | MIT | git+https://github.com/postcss/postcss.git | 8.5.6 | 8.5.4 | ^8.5.4 | Andrey Sitnik <andrey@sitnik.ru> |
|
| 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-import | perpetual | material | MIT | git+https://github.com/postcss/postcss-import.git | 16.1.1 | 16.1.0 | ^16.1.0 | Maxime Thirouin |
|
| 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 | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.7.3 | 3.5.3 | ^3.5.3 | James Long |
|
| 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-plugin-organize-imports | perpetual | material | MIT | git+https://github.com/simonhaenisch/prettier-plugin-organize-imports.git | 4.3.0 | 4.1.0 | ^4.1.0 | Simon Haenisch (https://github.com/simonhaenisch) |
|
| 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 | rimraf | perpetual | material | ISC | git+ssh://git@github.com/isaacs/rimraf.git | 6.1.2 | 6.0.1 | ^6.0.1 | Isaac Z. Schlueter <i@izs.me> (http://blog.izs.me/) |
|
| 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 | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.53.3 | 4.42.0 | ^4.42.0 | Rich Harris |
|
| 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-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 | 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-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-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-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-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-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 | 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 | sass | perpetual | material | MIT | git+https://github.com/sass/dart-sass.git | 1.94.2 | 1.89.1 | ^1.89.1 | Natalie Weizenbaum nweiz@google.com https://github.com/nex3 |
|
| 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 | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.8.1 | Microsoft Corp. |
|
| 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 | 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 | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.8.1 | Microsoft Corp. |
|
||||||
| 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. |
|
| 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. |
|
||||||
|
|
||||||
|
|||||||
@@ -2,7 +2,7 @@ import { FC, useEffect, useState } from 'react';
|
|||||||
import { WASMDataF } from '../../types/WASMData';
|
import { WASMDataF } from '../../types/WASMData';
|
||||||
import { LoadingState, SimBrief } from '../../types/general';
|
import { LoadingState, SimBrief } from '../../types/general';
|
||||||
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
||||||
import { CoherentCallSBEntryF, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallSBEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import CGSelect from '../CGSelect/CGSelect';
|
import CGSelect from '../CGSelect/CGSelect';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
@@ -11,13 +11,13 @@ interface SBEntryProps {
|
|||||||
WASMData: WASMDataF;
|
WASMData: WASMDataF;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
const [SBInFlight, setSBInFlight] = useState(false);
|
const [SBInFlight, setSBInFlight] = useState(false);
|
||||||
|
|
||||||
// FROM EFB
|
// FROM EFB
|
||||||
@@ -52,6 +52,11 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
|
|||||||
}
|
}
|
||||||
};
|
};
|
||||||
|
|
||||||
|
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
|
||||||
|
CoherentCallSBEntryF(CGTarget, _fuel ?? fuel, SBPlan);
|
||||||
|
};
|
||||||
|
|
||||||
|
useEffect(() => updateData(), [CGTarget, fuel]);
|
||||||
useEffect(() => {
|
useEffect(() => {
|
||||||
if (!simBrief || gsxActive) return;
|
if (!simBrief || gsxActive) return;
|
||||||
|
|
||||||
@@ -70,12 +75,13 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
|
|||||||
return;
|
return;
|
||||||
}
|
}
|
||||||
|
|
||||||
updateData(undefined, SBResponse.message as SimBrief);
|
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
|
||||||
|
|
||||||
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
|
updateData(SBResponse.message as SimBrief, _fuel);
|
||||||
|
|
||||||
|
setFuel(_fuel);
|
||||||
setSBInFlight(false);
|
setSBInFlight(false);
|
||||||
}, [simBrief, gsxActive]);
|
}, [simBrief, gsxActive]);
|
||||||
|
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -84,13 +90,6 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
const updateData = (_CGTarget?: number, SBPlan?: SimBrief) => {
|
|
||||||
CoherentCallSBEntryF(_CGTarget ?? CGTarget, SBPlan);
|
|
||||||
};
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -104,24 +103,8 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
@@ -164,14 +147,12 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
|
|||||||
increase={() =>
|
increase={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev + 0.1;
|
const _new = prev + 0.1;
|
||||||
updateData(_new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
decrease={() =>
|
decrease={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev - 0.1;
|
const _new = prev - 0.1;
|
||||||
updateData(_new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -2,7 +2,7 @@ import { FC, useEffect, useState } from 'react';
|
|||||||
import { WASMDataPax } from '../../types/WASMData';
|
import { WASMDataPax } from '../../types/WASMData';
|
||||||
import { LoadingState, SimBrief } from '../../types/general';
|
import { LoadingState, SimBrief } from '../../types/general';
|
||||||
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
|
||||||
import { CoherentCallSBEntryPax, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallSBEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import CGSelect from '../CGSelect/CGSelect';
|
import CGSelect from '../CGSelect/CGSelect';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
@@ -11,13 +11,13 @@ interface SBEntryProps {
|
|||||||
WASMData: WASMDataPax;
|
WASMData: WASMDataPax;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
const [SBInFlight, setSBInFlight] = useState(false);
|
const [SBInFlight, setSBInFlight] = useState(false);
|
||||||
|
|
||||||
// FROM EFB
|
// FROM EFB
|
||||||
@@ -52,6 +52,10 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
}
|
}
|
||||||
};
|
};
|
||||||
|
|
||||||
|
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
|
||||||
|
CoherentCallSBEntryPax(CGTarget, _fuel ?? fuel, SBPlan);
|
||||||
|
};
|
||||||
|
|
||||||
useEffect(() => {
|
useEffect(() => {
|
||||||
if (!simBrief || gsxActive) return;
|
if (!simBrief || gsxActive) return;
|
||||||
|
|
||||||
@@ -70,12 +74,17 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
return;
|
return;
|
||||||
}
|
}
|
||||||
|
|
||||||
updateData(undefined, SBResponse.message as SimBrief);
|
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);
|
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
|
||||||
setSBInFlight(false);
|
setSBInFlight(false);
|
||||||
}, [simBrief, gsxActive]);
|
}, [simBrief, gsxActive]);
|
||||||
|
|
||||||
|
useEffect(() => updateData(), [CGTarget, fuel]);
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -84,13 +93,6 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
const updateData = (_CGTarget?: number, SBPlan?: SimBrief) => {
|
|
||||||
CoherentCallSBEntryPax(_CGTarget ?? CGTarget, SBPlan);
|
|
||||||
};
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -104,24 +106,8 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
@@ -164,14 +150,12 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
increase={() =>
|
increase={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev + 0.1;
|
const _new = prev + 0.1;
|
||||||
updateData(_new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
decrease={() =>
|
decrease={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev - 0.1;
|
const _new = prev - 0.1;
|
||||||
updateData(_new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -1,6 +1,6 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { GSXLoadingState, WASMDataF } from '../../types/WASMData';
|
import { GSXFuelingState, GSXLoadingState, WASMDataF } from '../../types/WASMData';
|
||||||
import OptionsF from '../options/OptionsF';
|
import OptionsF from '../options/OptionsF';
|
||||||
import Profile from '../profile/Profile';
|
import Profile from '../profile/Profile';
|
||||||
import SBEntryF from '../SBEntry/SBEntryF';
|
import SBEntryF from '../SBEntry/SBEntryF';
|
||||||
@@ -65,6 +65,9 @@ const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
|||||||
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
|
const GSXFuelActive = () => {
|
||||||
|
return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
|
||||||
|
};
|
||||||
|
|
||||||
const CGs = (): [string, boolean, string, boolean] => {
|
const CGs = (): [string, boolean, string, boolean] => {
|
||||||
if (loadingState !== 'loaded' && !GSXActive()) {
|
if (loadingState !== 'loaded' && !GSXActive()) {
|
||||||
@@ -118,9 +121,7 @@ const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
|||||||
}
|
}
|
||||||
/>
|
/>
|
||||||
<Tabbar
|
<Tabbar
|
||||||
tabs={
|
tabs={username ? ['Simbrief', 'ZFW', 'Cargo', 'Options'] : ['ZFW', 'Cargo', 'Options']}
|
||||||
username ? ['Simbrief', 'ZFW', 'Cargo', 'Options'] : ['ZFW', 'Cargo', 'Options']
|
|
||||||
}
|
|
||||||
selectedTab={selectedTab}
|
selectedTab={selectedTab}
|
||||||
setSelectedTab={setSelectedTab}
|
setSelectedTab={setSelectedTab}
|
||||||
/>
|
/>
|
||||||
@@ -130,6 +131,7 @@ const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
||||||
@@ -138,6 +140,7 @@ const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
||||||
@@ -146,6 +149,7 @@ const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
||||||
|
|||||||
@@ -5,11 +5,11 @@ import Keyboard from '../keyboard/Keyboard';
|
|||||||
export default function Input(props: {
|
export default function Input(props: {
|
||||||
type?: string;
|
type?: string;
|
||||||
topKeyboard?: boolean;
|
topKeyboard?: boolean;
|
||||||
value: any;
|
value: number | string;
|
||||||
min?: number;
|
min?: number;
|
||||||
max?: number;
|
max?: number;
|
||||||
step?: number;
|
step?: number;
|
||||||
placeholder?: any;
|
placeholder?: string;
|
||||||
className?: string;
|
className?: string;
|
||||||
disabled?: boolean;
|
disabled?: boolean;
|
||||||
onChange?: (value: string) => void;
|
onChange?: (value: string) => void;
|
||||||
@@ -21,14 +21,28 @@ export default function Input(props: {
|
|||||||
const blurRef = useRef<boolean>(false);
|
const blurRef = useRef<boolean>(false);
|
||||||
const [isFocused, setFocused] = useState(false);
|
const [isFocused, setFocused] = useState(false);
|
||||||
const [showKeyboard, setShowKeyboard] = useState(false);
|
const [showKeyboard, setShowKeyboard] = useState(false);
|
||||||
|
const [unfocusTimer, setUnfocusTimer] = useState<NodeJS.Timeout | null>(null);
|
||||||
|
|
||||||
useEffect(() => {
|
useEffect(() => {
|
||||||
|
if (unfocusTimer) {
|
||||||
|
clearTimeout(unfocusTimer);
|
||||||
|
setUnfocusTimer(null);
|
||||||
|
}
|
||||||
|
|
||||||
if (isFocused) {
|
if (isFocused) {
|
||||||
|
setUnfocusTimer(setTimeout(() => ref.current?.blur(), 5e3));
|
||||||
Coherent.trigger('FOCUS_INPUT_FIELD', guid, '', '', '', false);
|
Coherent.trigger('FOCUS_INPUT_FIELD', guid, '', '', '', false);
|
||||||
} else {
|
} else {
|
||||||
console.log('UNFOCUS_INPUT_FIELD');
|
console.log('UNFOCUS_INPUT_FIELD');
|
||||||
Coherent.trigger('UNFOCUS_INPUT_FIELD', guid);
|
Coherent.trigger('UNFOCUS_INPUT_FIELD', guid);
|
||||||
}
|
}
|
||||||
|
|
||||||
|
return () => {
|
||||||
|
if (unfocusTimer) {
|
||||||
|
clearTimeout(unfocusTimer);
|
||||||
|
setUnfocusTimer(null);
|
||||||
|
}
|
||||||
|
};
|
||||||
}, [isFocused, guid]);
|
}, [isFocused, guid]);
|
||||||
|
|
||||||
return (
|
return (
|
||||||
@@ -60,6 +74,11 @@ export default function Input(props: {
|
|||||||
}}
|
}}
|
||||||
onChange={(e) => {
|
onChange={(e) => {
|
||||||
if (props.onChange) props.onChange(e.target.value);
|
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}
|
value={props.value}
|
||||||
className={props.className}
|
className={props.className}
|
||||||
|
|||||||
@@ -103,5 +103,6 @@ const Keyboard = forwardRef<
|
|||||||
document.body
|
document.body
|
||||||
);
|
);
|
||||||
});
|
});
|
||||||
|
Keyboard.displayName = "Keyboard"
|
||||||
|
|
||||||
export default Keyboard;
|
export default Keyboard;
|
||||||
|
|||||||
@@ -48,7 +48,7 @@ const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
|
|||||||
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Empty Weight</td>
|
<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>
|
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249537 lbs' : '113188 kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
@@ -84,7 +84,7 @@ const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
|
|||||||
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Empty Weight</td>
|
<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>
|
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249137 lbs' : '113006 kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
|
|||||||
@@ -2,8 +2,8 @@ import { FC, useEffect, useState } from 'react';
|
|||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { WASMDataPax } from '../../types/WASMData';
|
import { WASMDataPax } from '../../types/WASMData';
|
||||||
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
|
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
|
||||||
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
|
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
|
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
|
||||||
|
|
||||||
interface OptionsPaxProps {
|
interface OptionsPaxProps {
|
||||||
WASMData: WASMDataPax;
|
WASMData: WASMDataPax;
|
||||||
@@ -105,8 +105,8 @@ const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive })
|
|||||||
</td>
|
</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Empty Weight</td>
|
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '284375 lbs' : '128991 kg'}</td>
|
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286465 lbs' : '129937 kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||||
@@ -145,8 +145,8 @@ const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive })
|
|||||||
</td>
|
</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Empty Weight</td>
|
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
|
||||||
<td className="p-1 px-2">{WASMData.userData.isImperial ? '283975 lbs' : '128809 kg'}</td>
|
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286065 lbs' : '129755 kg'}</td>
|
||||||
</tr>
|
</tr>
|
||||||
<tr>
|
<tr>
|
||||||
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
<td className="p-1 px-2">Max Zero Fuel Weight</td>
|
||||||
|
|||||||
@@ -1,6 +1,6 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { GSXLoadingState, WASMDataPax } from '../../types/WASMData';
|
import { GSXFuelingState, GSXLoadingState, WASMDataPax } from '../../types/WASMData';
|
||||||
import OptionsPax from '../options/OptionsPax';
|
import OptionsPax from '../options/OptionsPax';
|
||||||
import Profile from '../profile/Profile';
|
import Profile from '../profile/Profile';
|
||||||
import SBEntryPax from '../SBEntry/SBEntryPax';
|
import SBEntryPax from '../SBEntry/SBEntryPax';
|
||||||
@@ -65,6 +65,9 @@ const Pax: FC<PaxProps> = ({ WASMData, username }) => {
|
|||||||
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
|
const GSXFuelActive = () => {
|
||||||
|
return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
|
||||||
|
};
|
||||||
|
|
||||||
const CGs = (): [string, boolean, string, boolean] => {
|
const CGs = (): [string, boolean, string, boolean] => {
|
||||||
if (loadingState !== 'loaded' && !GSXActive()) {
|
if (loadingState !== 'loaded' && !GSXActive()) {
|
||||||
@@ -134,6 +137,7 @@ const Pax: FC<PaxProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
|
||||||
@@ -142,6 +146,7 @@ const Pax: FC<PaxProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
|
||||||
@@ -150,6 +155,7 @@ const Pax: FC<PaxProps> = ({ WASMData, username }) => {
|
|||||||
loadingState={loadingState}
|
loadingState={loadingState}
|
||||||
setLoadingState={setLoadingState}
|
setLoadingState={setLoadingState}
|
||||||
gsxActive={GSXActive()}
|
gsxActive={GSXActive()}
|
||||||
|
gsxFuelActive={GSXFuelActive()}
|
||||||
/>
|
/>
|
||||||
)}
|
)}
|
||||||
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
|
||||||
|
|||||||
@@ -1,7 +1,7 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { WASMDataF } from '../../types/WASMData';
|
import { WASMDataF } from '../../types/WASMData';
|
||||||
import { CoherentCallStationEntryF, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallStationEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
|
|
||||||
@@ -9,18 +9,18 @@ interface StationEntryProps {
|
|||||||
WASMData: WASMDataF;
|
WASMData: WASMDataF;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||||
const [upper1, setUpper1] = useState(WASMData.targetPayload.upper1);
|
const [upper1, setUpper1] = useState(WASMData.targetPayload.upper1);
|
||||||
const [upper2, setUpper2] = useState(WASMData.targetPayload.upper2);
|
const [upper2, setUpper2] = useState(WASMData.targetPayload.upper2);
|
||||||
const [upper3, setUpper3] = useState(WASMData.targetPayload.upper3);
|
const [upper3, setUpper3] = useState(WASMData.targetPayload.upper3);
|
||||||
const [upper4, setUpper4] = useState(WASMData.targetPayload.upper4);
|
const [upper4, setUpper4] = useState(WASMData.targetPayload.upper4);
|
||||||
const [lowerForward, setLowerForward] = useState(WASMData.targetPayload.lowerForward);
|
const [lowerForward, setLowerForward] = useState(WASMData.targetPayload.lowerForward);
|
||||||
const [lowerRear, setLowerRear] = useState(WASMData.targetPayload.lowerRear);
|
const [lowerRear, setLowerRear] = useState(WASMData.targetPayload.lowerRear);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
|
|
||||||
const ZFW = () => {
|
const ZFW = () => {
|
||||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||||
@@ -52,10 +52,10 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
|
|||||||
};
|
};
|
||||||
|
|
||||||
const updateData = () => {
|
const updateData = () => {
|
||||||
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear);
|
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel);
|
||||||
};
|
};
|
||||||
|
|
||||||
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear]);
|
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel]);
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -64,9 +64,6 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -80,24 +77,8 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
|
|||||||
@@ -1,7 +1,7 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { WASMDataPax } from '../../types/WASMData';
|
import { WASMDataPax } from '../../types/WASMData';
|
||||||
import { CoherentCallStationEntryPax, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallStationEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
|
|
||||||
@@ -9,18 +9,24 @@ interface StationEntryProps {
|
|||||||
WASMData: WASMDataPax;
|
WASMData: WASMDataPax;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const StationEntryPax: FC<StationEntryProps> = ({
|
||||||
|
WASMData,
|
||||||
|
loadingState,
|
||||||
|
gsxActive,
|
||||||
|
gsxFuelActive,
|
||||||
|
setLoadingState,
|
||||||
|
}) => {
|
||||||
const [business1, setBusiness1] = useState(WASMData.targetPayload.business1);
|
const [business1, setBusiness1] = useState(WASMData.targetPayload.business1);
|
||||||
const [business2, setBusiness2] = useState(WASMData.targetPayload.business2);
|
const [business2, setBusiness2] = useState(WASMData.targetPayload.business2);
|
||||||
const [economy1, setEconomy1] = useState(WASMData.targetPayload.economy1);
|
const [economy1, setEconomy1] = useState(WASMData.targetPayload.economy1);
|
||||||
const [economy2, setEconomy2] = useState(WASMData.targetPayload.economy2);
|
const [economy2, setEconomy2] = useState(WASMData.targetPayload.economy2);
|
||||||
const [forwardCargo, setForwardCargo] = useState(WASMData.targetPayload.forwardCargo);
|
const [forwardCargo, setForwardCargo] = useState(WASMData.targetPayload.forwardCargo);
|
||||||
const [rearCargo, setRearCargo] = useState(WASMData.targetPayload.rearCargo);
|
const [rearCargo, setRearCargo] = useState(WASMData.targetPayload.rearCargo);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
|
|
||||||
const ZFW = () => {
|
const ZFW = () => {
|
||||||
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
|
||||||
@@ -52,10 +58,10 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
|
|||||||
};
|
};
|
||||||
|
|
||||||
const updateData = () => {
|
const updateData = () => {
|
||||||
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo);
|
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel);
|
||||||
};
|
};
|
||||||
|
|
||||||
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo]);
|
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel]);
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -64,9 +70,6 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -80,24 +83,8 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
|
|||||||
@@ -1,7 +1,7 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { WASMDataF } from '../../types/WASMData';
|
import { WASMDataF } from '../../types/WASMData';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { CoherentCallZFWEntry, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import CGSelect from '../CGSelect/CGSelect';
|
import CGSelect from '../CGSelect/CGSelect';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
@@ -10,14 +10,14 @@ interface ZFWEntryProps {
|
|||||||
WASMData: WASMDataF;
|
WASMData: WASMDataF;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
|
|
||||||
const ZFW = () => {
|
const ZFW = () => {
|
||||||
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
||||||
@@ -55,12 +55,13 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
|
|
||||||
const converted = parseInt(input);
|
const converted = parseInt(input);
|
||||||
if (converted) {
|
if (converted) {
|
||||||
if (converted < 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
|
if (converted <= 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
|
||||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||||
else setZFWTarget(converted);
|
else setZFWTarget(converted);
|
||||||
}
|
}
|
||||||
};
|
};
|
||||||
const handleBlur = (input: string) => {
|
|
||||||
|
const handleBlurZFW = (input: string) => {
|
||||||
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
||||||
|
|
||||||
if (!input) {
|
if (!input) {
|
||||||
@@ -74,10 +75,13 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||||
else setZFWTarget(converted);
|
else setZFWTarget(converted);
|
||||||
}
|
}
|
||||||
|
|
||||||
updateData(converted);
|
|
||||||
};
|
};
|
||||||
|
|
||||||
|
const updateData = () => {
|
||||||
|
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
|
||||||
|
};
|
||||||
|
|
||||||
|
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -86,13 +90,6 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
const updateData = (_ZFWTarget?: number, _CGTarget?: number) => {
|
|
||||||
CoherentCallZFWEntry(_ZFWTarget ?? ZFWTarget, _CGTarget ?? CGTarget);
|
|
||||||
};
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -106,24 +103,8 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
@@ -138,7 +119,7 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
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"
|
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}
|
value={ZFWTarget}
|
||||||
onChange={(value) => handleInputZFW(value)}
|
onChange={(value) => handleInputZFW(value)}
|
||||||
onBlur={(value) => handleBlur(value)}
|
onBlur={(value) => handleBlurZFW(value)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxActive}
|
||||||
/>
|
/>
|
||||||
</div>
|
</div>
|
||||||
@@ -156,14 +137,12 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
|
|||||||
increase={() =>
|
increase={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev + 0.1;
|
const _new = prev + 0.1;
|
||||||
updateData(undefined, _new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
decrease={() =>
|
decrease={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev - 0.1;
|
const _new = prev - 0.1;
|
||||||
updateData(undefined, _new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -1,7 +1,7 @@
|
|||||||
import { FC, useEffect, useState } from 'react';
|
import { FC, useEffect, useState } from 'react';
|
||||||
import { WASMDataPax } from '../../types/WASMData';
|
import { WASMDataPax } from '../../types/WASMData';
|
||||||
import { LoadingState } from '../../types/general';
|
import { LoadingState } from '../../types/general';
|
||||||
import { CoherentCallZFWEntry, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
|
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
|
||||||
import CGSelect from '../CGSelect/CGSelect';
|
import CGSelect from '../CGSelect/CGSelect';
|
||||||
import ActionBar from '../actionbar/ActionBar';
|
import ActionBar from '../actionbar/ActionBar';
|
||||||
import Input from '../input/Input';
|
import Input from '../input/Input';
|
||||||
@@ -10,14 +10,14 @@ interface ZFWEntryProps {
|
|||||||
WASMData: WASMDataPax;
|
WASMData: WASMDataPax;
|
||||||
loadingState: LoadingState;
|
loadingState: LoadingState;
|
||||||
gsxActive: boolean;
|
gsxActive: boolean;
|
||||||
|
gsxFuelActive: boolean;
|
||||||
setLoadingState: (newState: LoadingState) => void;
|
setLoadingState: (newState: LoadingState) => void;
|
||||||
}
|
}
|
||||||
|
|
||||||
const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
|
const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
|
||||||
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
|
||||||
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
|
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
|
||||||
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
|
||||||
const [fuelEnabled, setFuelEnabled] = useState(true);
|
|
||||||
|
|
||||||
const ZFW = () => {
|
const ZFW = () => {
|
||||||
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
|
||||||
@@ -60,7 +60,8 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
else setZFWTarget(converted);
|
else setZFWTarget(converted);
|
||||||
}
|
}
|
||||||
};
|
};
|
||||||
const handleBlur = (input: string) => {
|
|
||||||
|
const handleBlurZFW = (input: string) => {
|
||||||
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
|
||||||
|
|
||||||
if (!input) {
|
if (!input) {
|
||||||
@@ -74,10 +75,13 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
|
||||||
else setZFWTarget(converted);
|
else setZFWTarget(converted);
|
||||||
}
|
}
|
||||||
|
|
||||||
updateData(converted);
|
|
||||||
};
|
};
|
||||||
|
|
||||||
|
const updateData = () => {
|
||||||
|
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
|
||||||
|
};
|
||||||
|
|
||||||
|
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
|
||||||
useEffect(
|
useEffect(
|
||||||
() =>
|
() =>
|
||||||
setFuel((prev) => {
|
setFuel((prev) => {
|
||||||
@@ -86,13 +90,6 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
}),
|
}),
|
||||||
[WASMData.userData.isER]
|
[WASMData.userData.isER]
|
||||||
);
|
);
|
||||||
useEffect(() => {
|
|
||||||
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
|
|
||||||
}, [WASMData.livePayload.fuel]);
|
|
||||||
|
|
||||||
const updateData = (_ZFWTarget?: number, _CGTarget?: number) => {
|
|
||||||
CoherentCallZFWEntry(_ZFWTarget ?? ZFWTarget, _CGTarget ?? CGTarget);
|
|
||||||
};
|
|
||||||
|
|
||||||
return (
|
return (
|
||||||
<>
|
<>
|
||||||
@@ -106,24 +103,8 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
|
||||||
value={fuel}
|
value={fuel}
|
||||||
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxFuelActive}
|
||||||
/>
|
/>
|
||||||
<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={() => {
|
|
||||||
SimVar.SetSimVarValue(
|
|
||||||
'L:MD11_EFB_PAYLOAD_FUEL',
|
|
||||||
'lbs',
|
|
||||||
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
|
|
||||||
);
|
|
||||||
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
|
|
||||||
setFuelEnabled(WASMData.livePayload.fuel === fuel);
|
|
||||||
}}
|
|
||||||
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
|
|
||||||
>
|
|
||||||
Load Fuel
|
|
||||||
</button>
|
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
</div>
|
</div>
|
||||||
@@ -138,7 +119,7 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
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"
|
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}
|
value={ZFWTarget}
|
||||||
onChange={(value) => handleInputZFW(value)}
|
onChange={(value) => handleInputZFW(value)}
|
||||||
onBlur={(value) => handleBlur(value)}
|
onBlur={(value) => handleBlurZFW(value)}
|
||||||
disabled={loadingState !== 'preview' || gsxActive}
|
disabled={loadingState !== 'preview' || gsxActive}
|
||||||
/>
|
/>
|
||||||
</div>
|
</div>
|
||||||
@@ -156,14 +137,12 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
|
|||||||
increase={() =>
|
increase={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev + 0.1;
|
const _new = prev + 0.1;
|
||||||
updateData(undefined, _new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
decrease={() =>
|
decrease={() =>
|
||||||
setCGTarget((prev) => {
|
setCGTarget((prev) => {
|
||||||
const _new = prev - 0.1;
|
const _new = prev - 0.1;
|
||||||
updateData(undefined, _new);
|
|
||||||
return _new;
|
return _new;
|
||||||
})
|
})
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -5,6 +5,7 @@ interface WASMData {
|
|||||||
sbPlanned: {
|
sbPlanned: {
|
||||||
ZFW: number;
|
ZFW: number;
|
||||||
GW: number;
|
GW: number;
|
||||||
|
fuel: number;
|
||||||
};
|
};
|
||||||
loaded: boolean;
|
loaded: boolean;
|
||||||
}
|
}
|
||||||
@@ -26,6 +27,7 @@ interface TargetPayload {
|
|||||||
ZFWCG: number;
|
ZFWCG: number;
|
||||||
TOCG: number;
|
TOCG: number;
|
||||||
total: number;
|
total: number;
|
||||||
|
fuel: number;
|
||||||
}
|
}
|
||||||
|
|
||||||
interface TargetPayloadPax extends TargetPayload {
|
interface TargetPayloadPax extends TargetPayload {
|
||||||
@@ -39,9 +41,7 @@ interface TargetPayloadPax extends TargetPayload {
|
|||||||
rearCargo: number;
|
rearCargo: number;
|
||||||
}
|
}
|
||||||
|
|
||||||
interface LivePayloadPax extends TargetPayloadPax {
|
type LivePayloadPax = TargetPayloadPax;
|
||||||
fuel: number;
|
|
||||||
}
|
|
||||||
|
|
||||||
interface TargetPayloadF extends TargetPayload {
|
interface TargetPayloadF extends TargetPayload {
|
||||||
empty: number;
|
empty: number;
|
||||||
@@ -54,13 +54,12 @@ interface TargetPayloadF extends TargetPayload {
|
|||||||
lowerRear: number;
|
lowerRear: number;
|
||||||
}
|
}
|
||||||
|
|
||||||
interface LivePayloadF extends TargetPayloadF {
|
type LivePayloadF = TargetPayloadF;
|
||||||
fuel: number;
|
|
||||||
}
|
|
||||||
|
|
||||||
interface GSX {
|
interface GSX {
|
||||||
couatlStarted: boolean;
|
couatlStarted: boolean;
|
||||||
loadingState: GSXLoadingState;
|
loadingState: GSXLoadingState;
|
||||||
|
fuelingState: GSXFuelingState;
|
||||||
}
|
}
|
||||||
|
|
||||||
interface Limits {
|
interface Limits {
|
||||||
@@ -109,3 +108,8 @@ export enum GSXLoadingState {
|
|||||||
DEBOARDING = 3,
|
DEBOARDING = 3,
|
||||||
DEBOARDED = 4,
|
DEBOARDED = 4,
|
||||||
}
|
}
|
||||||
|
|
||||||
|
export enum GSXFuelingState {
|
||||||
|
IDLE = 0,
|
||||||
|
FUELING = 1,
|
||||||
|
}
|
||||||
|
|||||||
@@ -25,7 +25,7 @@ export const inRangeOf = (value: number, target: number, tolerance: number = 10)
|
|||||||
return Math.abs(value - target) < tolerance;
|
return Math.abs(value - target) < tolerance;
|
||||||
};
|
};
|
||||||
|
|
||||||
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number) => {
|
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number, fuelTarget: number) => {
|
||||||
Coherent.call(
|
Coherent.call(
|
||||||
COHERENT_COMM_BUS_WASM_CALL,
|
COHERENT_COMM_BUS_WASM_CALL,
|
||||||
CommBusEvent.UPDATE_TARGET,
|
CommBusEvent.UPDATE_TARGET,
|
||||||
@@ -33,6 +33,7 @@ export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number) => {
|
|||||||
mode: CallMode.ZFW_SET,
|
mode: CallMode.ZFW_SET,
|
||||||
ZFWTarget: ZFWTarget,
|
ZFWTarget: ZFWTarget,
|
||||||
CGTarget: CGTarget,
|
CGTarget: CGTarget,
|
||||||
|
fuelTarget: fuelTarget,
|
||||||
})
|
})
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
@@ -43,7 +44,8 @@ export const CoherentCallStationEntryPax = (
|
|||||||
economy1: number,
|
economy1: number,
|
||||||
economy2: number,
|
economy2: number,
|
||||||
forwardCargo: number,
|
forwardCargo: number,
|
||||||
rearCargo: number
|
rearCargo: number,
|
||||||
|
fuelTarget: number
|
||||||
) => {
|
) => {
|
||||||
Coherent.call(
|
Coherent.call(
|
||||||
COHERENT_COMM_BUS_WASM_CALL,
|
COHERENT_COMM_BUS_WASM_CALL,
|
||||||
@@ -56,6 +58,7 @@ export const CoherentCallStationEntryPax = (
|
|||||||
economy2,
|
economy2,
|
||||||
forwardCargo,
|
forwardCargo,
|
||||||
rearCargo,
|
rearCargo,
|
||||||
|
fuelTarget,
|
||||||
})
|
})
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
@@ -66,7 +69,8 @@ export const CoherentCallStationEntryF = (
|
|||||||
upper3: number,
|
upper3: number,
|
||||||
upper4: number,
|
upper4: number,
|
||||||
lowerForward: number,
|
lowerForward: number,
|
||||||
lowerRear: number
|
lowerRear: number,
|
||||||
|
fuelTarget: number
|
||||||
) => {
|
) => {
|
||||||
Coherent.call(
|
Coherent.call(
|
||||||
COHERENT_COMM_BUS_WASM_CALL,
|
COHERENT_COMM_BUS_WASM_CALL,
|
||||||
@@ -79,11 +83,12 @@ export const CoherentCallStationEntryF = (
|
|||||||
upper4,
|
upper4,
|
||||||
lowerForward,
|
lowerForward,
|
||||||
lowerRear,
|
lowerRear,
|
||||||
|
fuelTarget,
|
||||||
})
|
})
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
|
|
||||||
export const CoherentCallSBEntryPax = (CGTarget: number, SBPlan?: SimBrief) => {
|
export const CoherentCallSBEntryPax = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
|
||||||
Coherent.call(
|
Coherent.call(
|
||||||
COHERENT_COMM_BUS_WASM_CALL,
|
COHERENT_COMM_BUS_WASM_CALL,
|
||||||
CommBusEvent.UPDATE_TARGET,
|
CommBusEvent.UPDATE_TARGET,
|
||||||
@@ -94,11 +99,12 @@ export const CoherentCallSBEntryPax = (CGTarget: number, SBPlan?: SimBrief) => {
|
|||||||
CGTarget: CGTarget,
|
CGTarget: CGTarget,
|
||||||
plannedZFW: SBPlan?.plannedZFW,
|
plannedZFW: SBPlan?.plannedZFW,
|
||||||
plannedGW: SBPlan?.plannedGW,
|
plannedGW: SBPlan?.plannedGW,
|
||||||
|
fuel: fuel,
|
||||||
})
|
})
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
|
|
||||||
export const CoherentCallSBEntryF = (CGTarget: number, SBPlan?: SimBrief) => {
|
export const CoherentCallSBEntryF = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
|
||||||
Coherent.call(
|
Coherent.call(
|
||||||
COHERENT_COMM_BUS_WASM_CALL,
|
COHERENT_COMM_BUS_WASM_CALL,
|
||||||
CommBusEvent.UPDATE_TARGET,
|
CommBusEvent.UPDATE_TARGET,
|
||||||
@@ -108,6 +114,7 @@ export const CoherentCallSBEntryF = (CGTarget: number, SBPlan?: SimBrief) => {
|
|||||||
CGTarget: CGTarget,
|
CGTarget: CGTarget,
|
||||||
plannedZFW: SBPlan?.plannedZFW,
|
plannedZFW: SBPlan?.plannedZFW,
|
||||||
plannedGW: SBPlan?.plannedGW,
|
plannedGW: SBPlan?.plannedGW,
|
||||||
|
fuel: SBPlan?.fuel,
|
||||||
})
|
})
|
||||||
);
|
);
|
||||||
};
|
};
|
||||||
|
|||||||
File diff suppressed because it is too large
Load Diff
@@ -1,306 +0,0 @@
|
|||||||
#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 distributiob
|
|
||||||
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, userData->isImperial);
|
|
||||||
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, 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, userData->isImperial);
|
|
||||||
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, 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, const bool isImperial) {
|
|
||||||
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(const fPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, 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;
|
|
||||||
|
|
||||||
*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;
|
|
||||||
|
|
||||||
*TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
|
||||||
}
|
|
||||||
|
|
||||||
void load(const fPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial) {
|
|
||||||
fPayloadData_t localPayload = {};
|
|
||||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
|
||||||
normalisePayload(&localPayload, isImperial);
|
|
||||||
|
|
||||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t), &localPayload);
|
|
||||||
}
|
|
||||||
|
|
||||||
void unloadF(const HANDLE simConnect, const bool isER) {
|
|
||||||
fPayloadData_t localPayload = {};
|
|
||||||
|
|
||||||
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
|
|
||||||
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
|
|
||||||
|
|
||||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t), &localPayload);
|
|
||||||
}
|
|
||||||
@@ -1,111 +0,0 @@
|
|||||||
#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 ********************************/
|
|
||||||
//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;
|
|
||||||
|
|
||||||
// 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;
|
|
||||||
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;
|
|
||||||
} 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, const bool isImperial);
|
|
||||||
// Normalise to Pounds
|
|
||||||
// For Station Entry: CALL AFTER `generatePayload`
|
|
||||||
void normalisePayload(fPayloadData_t* const targetPayload, const bool isImperial);
|
|
||||||
void calculateCGs(const fPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial);
|
|
||||||
void load(const fPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial);
|
|
||||||
void unloadF(const HANDLE simConnect, const bool isER);
|
|
||||||
@@ -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);
|
||||||
+19
-21
@@ -1,45 +1,43 @@
|
|||||||
#pragma once
|
#pragma once
|
||||||
|
|
||||||
#ifndef __INTELLISENSE__
|
#ifndef __INTELLISENSE__
|
||||||
# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
|
#define MODULE_EXPORT __attribute__((visibility("default")))
|
||||||
# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
|
||||||
#else
|
#else
|
||||||
# define MODULE_EXPORT
|
#define MODULE_EXPORT
|
||||||
# define MODULE_WASM_MODNAME(mod)
|
#define MODULE_WASM_MODNAME(mod)
|
||||||
# define __attribute__(x)
|
#define __attribute__(x)
|
||||||
# define __restrict__
|
#define __restrict__
|
||||||
#endif
|
#endif
|
||||||
|
|
||||||
/********************************* Headers *********************************/
|
/********************************* Headers *********************************/
|
||||||
// MSFS headers
|
// MSFS headers
|
||||||
|
#include "rapidjson/filewritestream.h"
|
||||||
#include <MSFS/MSFS.h>
|
#include <MSFS/MSFS.h>
|
||||||
#include <MSFS/MSFS_CommBus.h>
|
#include <MSFS/MSFS_CommBus.h>
|
||||||
#include <MSFS/Legacy/gauges.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/document.h>
|
||||||
#include <rapidjson/filereadstream.h>
|
#include <rapidjson/filereadstream.h>
|
||||||
#include "rapidjson/filewritestream.h"
|
|
||||||
#include <rapidjson/writer.h>
|
#include <rapidjson/writer.h>
|
||||||
#include <SimConnect.h>
|
|
||||||
// C headers
|
|
||||||
#include <string.h>
|
|
||||||
// C++ headers
|
|
||||||
#include <ctime>
|
|
||||||
// Own headers
|
// Own headers
|
||||||
#include "shared.h"
|
|
||||||
#include "pax.h"
|
|
||||||
#include "freighter.h"
|
#include "freighter.h"
|
||||||
|
#include "fuel.h"
|
||||||
|
#include "log.h"
|
||||||
|
#include "pax.h"
|
||||||
|
#include "shared.h"
|
||||||
|
|
||||||
/******************************** Constants ********************************/
|
/******************************** Constants ********************************/
|
||||||
// Module identification
|
// Module identification
|
||||||
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
|
|
||||||
#define VERSION_STRING "1.6"
|
|
||||||
// COMM BUS
|
// COMM BUS
|
||||||
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
#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"
|
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
||||||
|
|
||||||
/******************************** Functions ********************************/
|
/******************************** Functions ********************************/
|
||||||
void commBusUpdateTargetCallback(const char* args, unsigned int size, void* ctx);
|
void commBusUpdateTargetCallback(const char *args, unsigned int size, void *ctx);
|
||||||
int receiveData(const char* buf);
|
int receiveData(const char *buf);
|
||||||
void sendData();
|
void sendData();
|
||||||
void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContext);
|
void CALLBACK MyDispatchProc(SIMCONNECT_RECV *pData, DWORD cbData, void *pContext);
|
||||||
void log(FILE* file, const char* format, void* optionalElement = NULL);
|
|
||||||
@@ -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;
|
||||||
@@ -1,25 +0,0 @@
|
|||||||
// load-manager-cli.cpp : This file contains the 'main' function. Program execution begins and ends there.
|
|
||||||
//
|
|
||||||
|
|
||||||
#include "../wasm-module/pax.h"
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
int main()
|
|
||||||
{
|
|
||||||
bool isImperial = false;
|
|
||||||
bool isER = true;
|
|
||||||
|
|
||||||
paxPayloadData_t targetPaxPayloadData = paxPayloadData_t();
|
|
||||||
targetPaxPayloadData.empty = FROM_POUNDS(isImperial, 283975);
|
|
||||||
targetPaxPayloadData.pilot = PAX_WEIGHT(isImperial);
|
|
||||||
targetPaxPayloadData.firstOfficer = PAX_WEIGHT(isImperial);
|
|
||||||
targetPaxPayloadData.engineer = PAX_WEIGHT(isImperial);
|
|
||||||
targetPaxPayloadData.cabinCrewFront = FRONT_CREW_WEIGHT(isImperial);
|
|
||||||
targetPaxPayloadData.cabinCrewRear = REAR_CREW_WEIGHT(isImperial);
|
|
||||||
targetPaxPayloadData.leftAux = isER ? AUX_WEIGHT(isImperial) : 0;
|
|
||||||
targetPaxPayloadData.rightAux = isER ? AUX_WEIGHT(isImperial) : 0;
|
|
||||||
FuelData_t liveFuelData = FuelData_t();
|
|
||||||
|
|
||||||
distribute(&targetPaxPayloadData, &liveFuelData, 162000.0, 20.5, isImperial);
|
|
||||||
}
|
|
||||||
@@ -1,109 +0,0 @@
|
|||||||
<?xml version="1.0" encoding="utf-8"?>
|
|
||||||
<Project DefaultTargets="Build" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
|
||||||
<ItemGroup Label="ProjectConfigurations">
|
|
||||||
<ProjectConfiguration Include="Debug|x64">
|
|
||||||
<Configuration>Debug</Configuration>
|
|
||||||
<Platform>x64</Platform>
|
|
||||||
</ProjectConfiguration>
|
|
||||||
<ProjectConfiguration Include="Release|x64">
|
|
||||||
<Configuration>Release</Configuration>
|
|
||||||
<Platform>x64</Platform>
|
|
||||||
</ProjectConfiguration>
|
|
||||||
</ItemGroup>
|
|
||||||
<PropertyGroup Label="Globals">
|
|
||||||
<VCProjectVersion>17.0</VCProjectVersion>
|
|
||||||
<Keyword>Win32Proj</Keyword>
|
|
||||||
<ProjectGuid>{992caf4b-b3f6-4a86-a1c1-663686082c5e}</ProjectGuid>
|
|
||||||
<RootNamespace>loadmanagercli</RootNamespace>
|
|
||||||
<WindowsTargetPlatformVersion>10.0</WindowsTargetPlatformVersion>
|
|
||||||
</PropertyGroup>
|
|
||||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.Default.props" />
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'" Label="Configuration">
|
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
|
||||||
<UseDebugLibraries>true</UseDebugLibraries>
|
|
||||||
<PlatformToolset>v143</PlatformToolset>
|
|
||||||
<CharacterSet>Unicode</CharacterSet>
|
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'" Label="Configuration">
|
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
|
||||||
<UseDebugLibraries>false</UseDebugLibraries>
|
|
||||||
<PlatformToolset>v143</PlatformToolset>
|
|
||||||
<WholeProgramOptimization>true</WholeProgramOptimization>
|
|
||||||
<CharacterSet>Unicode</CharacterSet>
|
|
||||||
</PropertyGroup>
|
|
||||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.props" />
|
|
||||||
<ImportGroup Label="ExtensionSettings">
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Label="Shared">
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Label="PropertySheets" Condition="'$(Configuration)|$(Platform)'=='Debug|Win32'">
|
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Label="PropertySheets" Condition="'$(Configuration)|$(Platform)'=='Release|Win32'">
|
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Label="PropertySheets" Condition="'$(Configuration)|$(Platform)'=='Debug|x64'">
|
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Label="PropertySheets" Condition="'$(Configuration)|$(Platform)'=='Release|x64'">
|
|
||||||
<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|x64'">
|
|
||||||
<IntDir>$(Platform)\$(Configuration)\</IntDir>
|
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'">
|
|
||||||
<IntDir>$(Platform)\$(Configuration)\</IntDir>
|
|
||||||
</PropertyGroup>
|
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|Win32'">
|
|
||||||
<ClCompile>
|
|
||||||
<WarningLevel>Level3</WarningLevel>
|
|
||||||
<SDLCheck>true</SDLCheck>
|
|
||||||
<PreprocessorDefinitions>WIN32;_DEBUG;_CONSOLE;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
|
||||||
<ConformanceMode>true</ConformanceMode>
|
|
||||||
</ClCompile>
|
|
||||||
<Link>
|
|
||||||
<SubSystem>Console</SubSystem>
|
|
||||||
<GenerateDebugInformation>true</GenerateDebugInformation>
|
|
||||||
</Link>
|
|
||||||
</ItemDefinitionGroup>
|
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'">
|
|
||||||
<ClCompile>
|
|
||||||
<WarningLevel>Level3</WarningLevel>
|
|
||||||
<SDLCheck>true</SDLCheck>
|
|
||||||
<PreprocessorDefinitions>_DEBUG;_CONSOLE;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
|
||||||
<ConformanceMode>true</ConformanceMode>
|
|
||||||
</ClCompile>
|
|
||||||
<Link>
|
|
||||||
<SubSystem>Console</SubSystem>
|
|
||||||
<GenerateDebugInformation>true</GenerateDebugInformation>
|
|
||||||
</Link>
|
|
||||||
</ItemDefinitionGroup>
|
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'">
|
|
||||||
<ClCompile>
|
|
||||||
<WarningLevel>Level3</WarningLevel>
|
|
||||||
<FunctionLevelLinking>true</FunctionLevelLinking>
|
|
||||||
<IntrinsicFunctions>true</IntrinsicFunctions>
|
|
||||||
<SDLCheck>true</SDLCheck>
|
|
||||||
<PreprocessorDefinitions>NDEBUG;_CONSOLE;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
|
||||||
<ConformanceMode>true</ConformanceMode>
|
|
||||||
</ClCompile>
|
|
||||||
<Link>
|
|
||||||
<SubSystem>Console</SubSystem>
|
|
||||||
<EnableCOMDATFolding>true</EnableCOMDATFolding>
|
|
||||||
<OptimizeReferences>true</OptimizeReferences>
|
|
||||||
<GenerateDebugInformation>true</GenerateDebugInformation>
|
|
||||||
</Link>
|
|
||||||
</ItemDefinitionGroup>
|
|
||||||
<ItemGroup>
|
|
||||||
<ClCompile Include="pax.cpp" />
|
|
||||||
<ClCompile Include="load-manager-cli.cpp" />
|
|
||||||
</ItemGroup>
|
|
||||||
<ItemGroup>
|
|
||||||
<ClInclude Include="pax.h" />
|
|
||||||
<ClInclude Include="types.h" />
|
|
||||||
</ItemGroup>
|
|
||||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
|
|
||||||
<ImportGroup Label="ExtensionTargets">
|
|
||||||
</ImportGroup>
|
|
||||||
</Project>
|
|
||||||
@@ -1,34 +0,0 @@
|
|||||||
<?xml version="1.0" encoding="utf-8"?>
|
|
||||||
<Project ToolsVersion="4.0" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
|
||||||
<ItemGroup>
|
|
||||||
<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>
|
|
||||||
<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="Resource Files">
|
|
||||||
<UniqueIdentifier>{67DA6AB6-F800-4c08-8B7A-83BB121AAD01}</UniqueIdentifier>
|
|
||||||
<Extensions>
|
|
||||||
rc;ico;cur;bmp;dlg;rc2;rct;bin;rgs;gif;jpg;jpeg;jpe;resx;tiff;tif;png;wav;mfcribbon-ms</Extensions>
|
|
||||||
</Filter>
|
|
||||||
</ItemGroup>
|
|
||||||
<ItemGroup>
|
|
||||||
<ClCompile Include="load-manager-cli.cpp">
|
|
||||||
<Filter>Source Files</Filter>
|
|
||||||
</ClCompile>
|
|
||||||
<ClCompile Include="pax.cpp">
|
|
||||||
<Filter>Source Files</Filter>
|
|
||||||
</ClCompile>
|
|
||||||
</ItemGroup>
|
|
||||||
<ItemGroup>
|
|
||||||
<ClInclude Include="pax.h">
|
|
||||||
<Filter>Header Files</Filter>
|
|
||||||
</ClInclude>
|
|
||||||
<ClInclude Include="types.h">
|
|
||||||
<Filter>Header Files</Filter>
|
|
||||||
</ClInclude>
|
|
||||||
</ItemGroup>
|
|
||||||
</Project>
|
|
||||||
@@ -1,4 +0,0 @@
|
|||||||
<?xml version="1.0" encoding="utf-8"?>
|
|
||||||
<Project ToolsVersion="Current" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
|
||||||
<PropertyGroup />
|
|
||||||
</Project>
|
|
||||||
File diff suppressed because it is too large
Load Diff
@@ -5,28 +5,16 @@ VisualStudioVersion = 17.13.36105.23
|
|||||||
MinimumVisualStudioVersion = 10.0.40219.1
|
MinimumVisualStudioVersion = 10.0.40219.1
|
||||||
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager", "load-manager.vcxproj", "{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}"
|
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager", "load-manager.vcxproj", "{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}"
|
||||||
EndProject
|
EndProject
|
||||||
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager-cli", "load-manager-cli.vcxproj", "{992CAF4B-B3F6-4A86-A1C1-663686082C5E}"
|
|
||||||
EndProject
|
|
||||||
Global
|
Global
|
||||||
GlobalSection(SolutionConfigurationPlatforms) = preSolution
|
GlobalSection(SolutionConfigurationPlatforms) = preSolution
|
||||||
Debug|MSFS = Debug|MSFS
|
Debug|MSFS = Debug|MSFS
|
||||||
Debug|x64 = Debug|x64
|
|
||||||
Release|MSFS = Release|MSFS
|
Release|MSFS = Release|MSFS
|
||||||
Release|x64 = Release|x64
|
|
||||||
EndGlobalSection
|
EndGlobalSection
|
||||||
GlobalSection(ProjectConfigurationPlatforms) = postSolution
|
GlobalSection(ProjectConfigurationPlatforms) = postSolution
|
||||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|MSFS.ActiveCfg = Debug|MSFS
|
{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}.Debug|MSFS.Build.0 = Debug|MSFS
|
||||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|x64.ActiveCfg = Debug|x64
|
|
||||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.ActiveCfg = Release|MSFS
|
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.ActiveCfg = Release|MSFS
|
||||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.Build.0 = Release|MSFS
|
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.Build.0 = Release|MSFS
|
||||||
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|x64.ActiveCfg = Release|MSFS
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|MSFS.ActiveCfg = Debug|x64
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|x64.ActiveCfg = Debug|x64
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|x64.Build.0 = Debug|x64
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|MSFS.ActiveCfg = Release|x64
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|x64.ActiveCfg = Release|x64
|
|
||||||
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|x64.Build.0 = Release|x64
|
|
||||||
EndGlobalSection
|
EndGlobalSection
|
||||||
GlobalSection(SolutionProperties) = preSolution
|
GlobalSection(SolutionProperties) = preSolution
|
||||||
HideSolutionNode = FALSE
|
HideSolutionNode = FALSE
|
||||||
|
|||||||
@@ -5,18 +5,10 @@
|
|||||||
<Configuration>Debug</Configuration>
|
<Configuration>Debug</Configuration>
|
||||||
<Platform>MSFS</Platform>
|
<Platform>MSFS</Platform>
|
||||||
</ProjectConfiguration>
|
</ProjectConfiguration>
|
||||||
<ProjectConfiguration Include="Debug|x64">
|
|
||||||
<Configuration>Debug</Configuration>
|
|
||||||
<Platform>x64</Platform>
|
|
||||||
</ProjectConfiguration>
|
|
||||||
<ProjectConfiguration Include="Release|MSFS">
|
<ProjectConfiguration Include="Release|MSFS">
|
||||||
<Configuration>Release</Configuration>
|
<Configuration>Release</Configuration>
|
||||||
<Platform>MSFS</Platform>
|
<Platform>MSFS</Platform>
|
||||||
</ProjectConfiguration>
|
</ProjectConfiguration>
|
||||||
<ProjectConfiguration Include="Release|x64">
|
|
||||||
<Configuration>Release</Configuration>
|
|
||||||
<Platform>x64</Platform>
|
|
||||||
</ProjectConfiguration>
|
|
||||||
</ItemGroup>
|
</ItemGroup>
|
||||||
<PropertyGroup Label="Globals">
|
<PropertyGroup Label="Globals">
|
||||||
<VCProjectVersion>16.0</VCProjectVersion>
|
<VCProjectVersion>16.0</VCProjectVersion>
|
||||||
@@ -29,26 +21,13 @@
|
|||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="Configuration">
|
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="Configuration">
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
<ConfigurationType>Application</ConfigurationType>
|
||||||
<UseDebugLibraries>true</UseDebugLibraries>
|
<UseDebugLibraries>true</UseDebugLibraries>
|
||||||
<PlatformToolset>MSFS</PlatformToolset>
|
<PlatformToolset>MSFS2024</PlatformToolset>
|
||||||
<CharacterSet>MultiByte</CharacterSet>
|
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'" Label="Configuration">
|
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
|
||||||
<UseDebugLibraries>true</UseDebugLibraries>
|
|
||||||
<PlatformToolset>MSFS</PlatformToolset>
|
|
||||||
<CharacterSet>MultiByte</CharacterSet>
|
<CharacterSet>MultiByte</CharacterSet>
|
||||||
</PropertyGroup>
|
</PropertyGroup>
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="Configuration">
|
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="Configuration">
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
<ConfigurationType>Application</ConfigurationType>
|
||||||
<UseDebugLibraries>false</UseDebugLibraries>
|
<UseDebugLibraries>false</UseDebugLibraries>
|
||||||
<PlatformToolset>MSFS</PlatformToolset>
|
<PlatformToolset>MSFS2024</PlatformToolset>
|
||||||
<WholeProgramOptimization>true</WholeProgramOptimization>
|
|
||||||
<CharacterSet>MultiByte</CharacterSet>
|
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'" Label="Configuration">
|
|
||||||
<ConfigurationType>Application</ConfigurationType>
|
|
||||||
<UseDebugLibraries>false</UseDebugLibraries>
|
|
||||||
<PlatformToolset>MSFS</PlatformToolset>
|
|
||||||
<WholeProgramOptimization>true</WholeProgramOptimization>
|
<WholeProgramOptimization>true</WholeProgramOptimization>
|
||||||
<CharacterSet>MultiByte</CharacterSet>
|
<CharacterSet>MultiByte</CharacterSet>
|
||||||
</PropertyGroup>
|
</PropertyGroup>
|
||||||
@@ -60,37 +39,20 @@
|
|||||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="PropertySheets">
|
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="PropertySheets">
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
||||||
</ImportGroup>
|
</ImportGroup>
|
||||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'" Label="PropertySheets">
|
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
|
||||||
</ImportGroup>
|
|
||||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="PropertySheets">
|
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="PropertySheets">
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
||||||
</ImportGroup>
|
</ImportGroup>
|
||||||
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'" Label="PropertySheets">
|
|
||||||
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
|
|
||||||
</ImportGroup>
|
|
||||||
<PropertyGroup Label="UserMacros" />
|
<PropertyGroup Label="UserMacros" />
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
|
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
|
||||||
<TargetExt>.wasm</TargetExt>
|
<TargetExt>.wasm</TargetExt>
|
||||||
<GenerateManifest />
|
<GenerateManifest />
|
||||||
<LinkIncremental />
|
<LinkIncremental />
|
||||||
<IncludePath>$(MSFS_IncludePath)</IncludePath>
|
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
|
||||||
<TargetName>$(ProjectName)</TargetName>
|
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'">
|
|
||||||
<TargetExt>.wasm</TargetExt>
|
|
||||||
<GenerateManifest />
|
|
||||||
<LinkIncremental />
|
|
||||||
<IncludePath>$(MSFS_IncludePath)</IncludePath>
|
|
||||||
<TargetName>$(ProjectName)</TargetName>
|
<TargetName>$(ProjectName)</TargetName>
|
||||||
</PropertyGroup>
|
</PropertyGroup>
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
||||||
<TargetExt>.wasm</TargetExt>
|
<TargetExt>.wasm</TargetExt>
|
||||||
<IncludePath>$(MSFS_IncludePath)</IncludePath>
|
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
|
||||||
</PropertyGroup>
|
|
||||||
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'">
|
|
||||||
<TargetExt>.wasm</TargetExt>
|
|
||||||
<IncludePath>$(MSFS_IncludePath)</IncludePath>
|
|
||||||
</PropertyGroup>
|
</PropertyGroup>
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
|
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
|
||||||
<ClCompile>
|
<ClCompile>
|
||||||
@@ -114,7 +76,8 @@
|
|||||||
</BasicRuntimeChecks>
|
</BasicRuntimeChecks>
|
||||||
<LanguageStandard>stdcpp14</LanguageStandard>
|
<LanguageStandard>stdcpp14</LanguageStandard>
|
||||||
<MultiProcessorCompilation>true</MultiProcessorCompilation>
|
<MultiProcessorCompilation>true</MultiProcessorCompilation>
|
||||||
<AdditionalOptions>/clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
|
||||||
|
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
||||||
</ClCompile>
|
</ClCompile>
|
||||||
<Link>
|
<Link>
|
||||||
<SubSystem>
|
<SubSystem>
|
||||||
@@ -144,57 +107,6 @@
|
|||||||
Powershell.exe -File .\copy-debug.ps1</Command>
|
Powershell.exe -File .\copy-debug.ps1</Command>
|
||||||
</PostBuildEvent>
|
</PostBuildEvent>
|
||||||
</ItemDefinitionGroup>
|
</ItemDefinitionGroup>
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'">
|
|
||||||
<ClCompile>
|
|
||||||
<WarningLevel>Level3</WarningLevel>
|
|
||||||
<Optimization>Disabled</Optimization>
|
|
||||||
<SDLCheck>
|
|
||||||
</SDLCheck>
|
|
||||||
<ConformanceMode>true</ConformanceMode>
|
|
||||||
<BufferSecurityCheck>false</BufferSecurityCheck>
|
|
||||||
<AdditionalIncludeDirectories>
|
|
||||||
</AdditionalIncludeDirectories>
|
|
||||||
<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>
|
|
||||||
</ClCompile>
|
|
||||||
<Link>
|
|
||||||
<SubSystem>
|
|
||||||
</SubSystem>
|
|
||||||
<AdditionalDependencies>
|
|
||||||
</AdditionalDependencies>
|
|
||||||
<IgnoreAllDefaultLibraries>
|
|
||||||
</IgnoreAllDefaultLibraries>
|
|
||||||
<NoEntryPoint>true</NoEntryPoint>
|
|
||||||
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
|
|
||||||
<RandomizedBaseAddress>
|
|
||||||
</RandomizedBaseAddress>
|
|
||||||
<DataExecutionPrevention>
|
|
||||||
</DataExecutionPrevention>
|
|
||||||
<GenerateDebugInformation>true</GenerateDebugInformation>
|
|
||||||
<ProgramDatabaseFile>
|
|
||||||
</ProgramDatabaseFile>
|
|
||||||
<ImportLibrary>
|
|
||||||
</ImportLibrary>
|
|
||||||
<ProfileGuidedDatabase>
|
|
||||||
</ProfileGuidedDatabase>
|
|
||||||
<AdditionalLibraryDirectories>
|
|
||||||
</AdditionalLibraryDirectories>
|
|
||||||
</Link>
|
|
||||||
<PostBuildEvent>
|
|
||||||
<Command>
|
|
||||||
</Command>
|
|
||||||
</PostBuildEvent>
|
|
||||||
</ItemDefinitionGroup>
|
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
|
||||||
<ClCompile>
|
<ClCompile>
|
||||||
<WarningLevel>Level3</WarningLevel>
|
<WarningLevel>Level3</WarningLevel>
|
||||||
@@ -212,7 +124,8 @@ Powershell.exe -File .\copy-debug.ps1</Command>
|
|||||||
<SupportJustMyCode>
|
<SupportJustMyCode>
|
||||||
</SupportJustMyCode>
|
</SupportJustMyCode>
|
||||||
<LanguageStandard>stdcpp14</LanguageStandard>
|
<LanguageStandard>stdcpp14</LanguageStandard>
|
||||||
<AdditionalOptions>/clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
|
||||||
|
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
|
||||||
</ClCompile>
|
</ClCompile>
|
||||||
<Link>
|
<Link>
|
||||||
<SubSystem>
|
<SubSystem>
|
||||||
@@ -240,60 +153,20 @@ Powershell.exe -File .\copy-debug.ps1</Command>
|
|||||||
Powershell.exe -File .\copy-release.ps1</Command>
|
Powershell.exe -File .\copy-release.ps1</Command>
|
||||||
</PostBuildEvent>
|
</PostBuildEvent>
|
||||||
</ItemDefinitionGroup>
|
</ItemDefinitionGroup>
|
||||||
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|x64'">
|
|
||||||
<ClCompile>
|
|
||||||
<WarningLevel>Level3</WarningLevel>
|
|
||||||
<Optimization>MaxSpeed</Optimization>
|
|
||||||
<FunctionLevelLinking>true</FunctionLevelLinking>
|
|
||||||
<IntrinsicFunctions>true</IntrinsicFunctions>
|
|
||||||
<SDLCheck>true</SDLCheck>
|
|
||||||
<ConformanceMode>true</ConformanceMode>
|
|
||||||
<AdditionalIncludeDirectories>
|
|
||||||
</AdditionalIncludeDirectories>
|
|
||||||
<PreprocessorDefinitions>__wasi__;__wasm32__;_STRING_H_CPLUSPLUS_98_CONFORMANCE_;_WCHAR_H_CPLUSPLUS_98_CONFORMANCE_;_LIBCPP_NO_EXCEPTIONS;_LIBCPP_HAS_NO_THREADS;_LIBCPP_STD_VER=14;_WINDLL;%(PreprocessorDefinitions)</PreprocessorDefinitions>
|
|
||||||
<BufferSecurityCheck>false</BufferSecurityCheck>
|
|
||||||
<ExceptionHandling>false</ExceptionHandling>
|
|
||||||
<DebugInformationFormat>false</DebugInformationFormat>
|
|
||||||
<SupportJustMyCode>
|
|
||||||
</SupportJustMyCode>
|
|
||||||
<LanguageStandard>stdcpp14</LanguageStandard>
|
|
||||||
</ClCompile>
|
|
||||||
<Link>
|
|
||||||
<SubSystem>
|
|
||||||
</SubSystem>
|
|
||||||
<AdditionalDependencies>%(AdditionalDependencies)</AdditionalDependencies>
|
|
||||||
<IgnoreAllDefaultLibraries>
|
|
||||||
</IgnoreAllDefaultLibraries>
|
|
||||||
<NoEntryPoint>true</NoEntryPoint>
|
|
||||||
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
|
|
||||||
<RandomizedBaseAddress>
|
|
||||||
</RandomizedBaseAddress>
|
|
||||||
<DataExecutionPrevention>
|
|
||||||
</DataExecutionPrevention>
|
|
||||||
<GenerateDebugInformation>false</GenerateDebugInformation>
|
|
||||||
<ProgramDatabaseFile>
|
|
||||||
</ProgramDatabaseFile>
|
|
||||||
<ImportLibrary>
|
|
||||||
</ImportLibrary>
|
|
||||||
<ProfileGuidedDatabase>
|
|
||||||
</ProfileGuidedDatabase>
|
|
||||||
<AdditionalLibraryDirectories>$(OutDir)</AdditionalLibraryDirectories>
|
|
||||||
</Link>
|
|
||||||
<PostBuildEvent>
|
|
||||||
<Command>
|
|
||||||
</Command>
|
|
||||||
</PostBuildEvent>
|
|
||||||
</ItemDefinitionGroup>
|
|
||||||
<ItemGroup>
|
<ItemGroup>
|
||||||
<ClCompile Include="freighter.cpp" />
|
<ClCompile Include="src/freighter.cpp" />
|
||||||
<ClCompile Include="load-manager.cpp" />
|
<ClCompile Include="src/load-manager.cpp" />
|
||||||
<ClCompile Include="pax.cpp" />
|
<ClCompile Include="src/log.cpp" />
|
||||||
|
<ClCompile Include="src/pax.cpp" />
|
||||||
|
<ClCompile Include="src/fuel.cpp" />
|
||||||
</ItemGroup>
|
</ItemGroup>
|
||||||
<ItemGroup>
|
<ItemGroup>
|
||||||
<ClInclude Include="freighter.h" />
|
<ClInclude Include="include/freighter.h" />
|
||||||
<ClInclude Include="load-manager.h" />
|
<ClInclude Include="include/load-manager.h" />
|
||||||
<ClInclude Include="pax.h" />
|
<ClInclude Include="include/log.h" />
|
||||||
<ClInclude Include="shared.h" />
|
<ClInclude Include="include/pax.h" />
|
||||||
|
<ClInclude Include="include/shared.h" />
|
||||||
|
<ClInclude Include="include/fuel.h" />
|
||||||
</ItemGroup>
|
</ItemGroup>
|
||||||
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
|
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
|
||||||
<ImportGroup Label="ExtensionTargets">
|
<ImportGroup Label="ExtensionTargets">
|
||||||
|
|||||||
@@ -1,27 +1,39 @@
|
|||||||
<?xml version="1.0" encoding="utf-8"?>
|
<?xml version="1.0" encoding="utf-8"?>
|
||||||
<Project ToolsVersion="4.0" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
<Project ToolsVersion="4.0" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
|
||||||
<ItemGroup>
|
<ItemGroup>
|
||||||
<ClCompile Include="load-manager.cpp">
|
<ClCompile Include="src/freighter.cpp">
|
||||||
<Filter>Source Files</Filter>
|
<Filter>Source Files</Filter>
|
||||||
</ClCompile>
|
</ClCompile>
|
||||||
<ClCompile Include="pax.cpp">
|
<ClCompile Include="src/load-manager.cpp">
|
||||||
<Filter>Source Files</Filter>
|
<Filter>Source Files</Filter>
|
||||||
</ClCompile>
|
</ClCompile>
|
||||||
<ClCompile Include="freighter.cpp">
|
<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>
|
<Filter>Source Files</Filter>
|
||||||
</ClCompile>
|
</ClCompile>
|
||||||
</ItemGroup>
|
</ItemGroup>
|
||||||
<ItemGroup>
|
<ItemGroup>
|
||||||
<ClInclude Include="pax.h">
|
<ClInclude Include="include/freighter.h">
|
||||||
<Filter>Header Files</Filter>
|
<Filter>Header Files</Filter>
|
||||||
</ClInclude>
|
</ClInclude>
|
||||||
<ClInclude Include="load-manager.h">
|
<ClInclude Include="include/load-manager.h">
|
||||||
<Filter>Header Files</Filter>
|
<Filter>Header Files</Filter>
|
||||||
</ClInclude>
|
</ClInclude>
|
||||||
<ClInclude Include="shared.h">
|
<ClInclude Include="include/log.h">
|
||||||
<Filter>Header Files</Filter>
|
<Filter>Header Files</Filter>
|
||||||
</ClInclude>
|
</ClInclude>
|
||||||
<ClInclude Include="freighter.h">
|
<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>
|
<Filter>Header Files</Filter>
|
||||||
</ClInclude>
|
</ClInclude>
|
||||||
</ItemGroup>
|
</ItemGroup>
|
||||||
|
|||||||
@@ -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"
|
||||||
|
}
|
||||||
@@ -1,329 +0,0 @@
|
|||||||
#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 distibution 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, &targetPayload->ZFWCG, &targetPayload->TOCG, 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, &targetPayload->ZFWCG, &targetPayload->TOCG, 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(const paxPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, 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;
|
|
||||||
|
|
||||||
*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;
|
|
||||||
|
|
||||||
*TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
|
|
||||||
}
|
|
||||||
|
|
||||||
void load(const paxPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial) {
|
|
||||||
paxPayloadData_t localPayload = {};
|
|
||||||
memcpy(&localPayload, targetPayload, sizeof(localPayload));
|
|
||||||
normalisePayload(&localPayload, isImperial);
|
|
||||||
|
|
||||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(paxPayloadDataSet_t), &localPayload);
|
|
||||||
}
|
|
||||||
|
|
||||||
void unload(const HANDLE simConnect, const bool isER) {
|
|
||||||
paxPayloadDataSet_t localPayload = {};
|
|
||||||
|
|
||||||
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);
|
|
||||||
|
|
||||||
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(paxPayloadDataSet_t), &localPayload);
|
|
||||||
}
|
|
||||||
|
|
||||||
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t* const options) {
|
|
||||||
return (isImperial) ? (options->paxWeightLBS) : (options->paxWeightKG);
|
|
||||||
}
|
|
||||||
|
|
||||||
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t* const options) {
|
|
||||||
return (isImperial) ? (options->bagWeightLBS) : (options->bagWeightKG);
|
|
||||||
}
|
|
||||||
@@ -1,150 +0,0 @@
|
|||||||
#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 ********************************/
|
|
||||||
// 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;
|
|
||||||
|
|
||||||
// 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;
|
|
||||||
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;
|
|
||||||
} 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(const paxPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial);
|
|
||||||
void load(const paxPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial);
|
|
||||||
void unload(const HANDLE simConnect, const bool isER);
|
|
||||||
// Based on ICAO/LH findings
|
|
||||||
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t* const options);
|
|
||||||
// Based on ICAO/LH findings
|
|
||||||
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t* const options);
|
|
||||||
@@ -1,154 +0,0 @@
|
|||||||
#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))
|
|
||||||
// Max Fuel
|
|
||||||
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
|
|
||||||
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
|
|
||||||
// Arms Shared
|
|
||||||
#define ARM_EMPTY -159.6
|
|
||||||
#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
|
|
||||||
// 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
|
|
||||||
// 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_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_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_GSX,
|
|
||||||
DATA_REQUEST_USER_DATA,
|
|
||||||
};
|
|
||||||
|
|
||||||
enum LOADING_STATES {
|
|
||||||
LOADING_STATE_IDLE,
|
|
||||||
LOADING_STATE_BOARDING,
|
|
||||||
LOADING_STATE_BOARDED,
|
|
||||||
LOADING_STATE_DEBOARDING,
|
|
||||||
LOADING_STATE_DEBOARDED,
|
|
||||||
};
|
|
||||||
|
|
||||||
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 passengersBoarded; // Num pax
|
|
||||||
double passengersDeboarded; // Num pax
|
|
||||||
double cargoBoarded; // In percent
|
|
||||||
double cargoDeboarded; // In percent
|
|
||||||
|
|
||||||
// Additional properties
|
|
||||||
enum LOADING_STATES loadingState;
|
|
||||||
} GSXData_t;
|
|
||||||
|
|
||||||
typedef struct {
|
|
||||||
// SimConnect mapped
|
|
||||||
double poundsPerGallon; // DO NOT USE
|
|
||||||
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 {
|
|
||||||
bool GSXSync;
|
|
||||||
double paxWeightKG;
|
|
||||||
double bagWeightKG;
|
|
||||||
double paxWeightLBS;
|
|
||||||
double bagWeightLBS;
|
|
||||||
} UserOptions_t;
|
|
||||||
@@ -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
-1
@@ -1 +1 @@
|
|||||||
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
|
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
|
||||||
+1
-1
@@ -1 +1 @@
|
|||||||
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
|
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
|
||||||
|
|||||||
+19
-24
@@ -1,45 +1,40 @@
|
|||||||
const { applyPatch } = require("diff");
|
const { applyPatch } = require('diff');
|
||||||
const fs = require("fs");
|
const fs = require('fs');
|
||||||
const util = require("node:util");
|
const readline = require('readline');
|
||||||
const exec = util.promisify(require("node:child_process").exec);
|
|
||||||
const readline = require("readline");
|
|
||||||
|
|
||||||
const outPath =
|
const outPath = './PackageSources/html_ui/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb';
|
||||||
"./PackageSources/html_ui/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb";
|
|
||||||
|
|
||||||
fs.copyFileSync("./EFB/efb.css", `${outPath}/efb.css`);
|
let file1Contents = fs.readFileSync('./EFB/efb.js').toString();
|
||||||
|
let patch = fs.readFileSync('./EFB/efb-js.patch').toString();
|
||||||
let file1Contents = fs.readFileSync("./EFB/efb.js").toString();
|
|
||||||
let patch = fs.readFileSync("./EFB/efb-js.patch").toString();
|
|
||||||
let patchedFile = applyPatch(file1Contents, patch);
|
let patchedFile = applyPatch(file1Contents, patch);
|
||||||
fs.writeFileSync(`${outPath}/efb.js`, patchedFile);
|
fs.writeFileSync(`${outPath}/efb.js`, patchedFile);
|
||||||
|
|
||||||
file1Contents = fs.readFileSync("./EFB/efb.index.js").toString();
|
file1Contents = fs.readFileSync('./EFB/efb.index.js').toString();
|
||||||
patch = fs.readFileSync("./EFB/efb-index-js.patch").toString();
|
patch = fs.readFileSync('./EFB/efb-index-js.patch').toString();
|
||||||
patchedFile = applyPatch(file1Contents, patch);
|
patchedFile = applyPatch(file1Contents, patch);
|
||||||
fs.writeFileSync(`${outPath}/efb.index.js`, patchedFile);
|
fs.writeFileSync(`${outPath}/efb.index.js`, patchedFile);
|
||||||
|
|
||||||
file1Contents = fs.readFileSync("./EFB/efb.html").toString();
|
file1Contents = fs.readFileSync('./EFB/efb.html').toString();
|
||||||
patch = fs.readFileSync("./EFB/efb-html.patch").toString();
|
patch = fs.readFileSync('./EFB/efb-html.patch').toString();
|
||||||
patchedFile = applyPatch(file1Contents, patch);
|
patchedFile = applyPatch(file1Contents, patch);
|
||||||
fs.writeFileSync(`${outPath}/efb.html`, patchedFile);
|
fs.writeFileSync(`${outPath}/efb.html`, patchedFile);
|
||||||
|
|
||||||
var output = "";
|
var output = '';
|
||||||
var lineReader = readline.createInterface({
|
var lineReader = readline.createInterface({
|
||||||
input: fs.createReadStream(`${outPath}/App.js`),
|
input: fs.createReadStream(`${outPath}/App.js`),
|
||||||
});
|
});
|
||||||
lineReader.on("line", (line) => {
|
lineReader.on('line', (line) => {
|
||||||
if (line.startsWith("import")) {
|
if (line.startsWith('import')) {
|
||||||
output += "// " + line + "\n";
|
output += '// ' + line + '\n';
|
||||||
} else if (line.startsWith("export")) {
|
} else if (line.startsWith('export')) {
|
||||||
output += "window.KH_LM = App;\n";
|
output += 'window.KH_LM = App;\n';
|
||||||
} else {
|
} else {
|
||||||
output += line + "\n";
|
output += line + '\n';
|
||||||
}
|
}
|
||||||
});
|
});
|
||||||
lineReader.on("close", () => {
|
lineReader.on('close', () => {
|
||||||
fs.writeFile(`${outPath}/App.js`, output, (err) => {
|
fs.writeFile(`${outPath}/App.js`, output, (err) => {
|
||||||
if (err) console.log(err);
|
if (err) console.log(err);
|
||||||
console.log("Import/Export removed.");
|
console.log('Import/Export removed.');
|
||||||
});
|
});
|
||||||
});
|
});
|
||||||
|
|||||||
+24
-3
@@ -1,5 +1,26 @@
|
|||||||
{
|
{
|
||||||
"devDependencies": {
|
"name": "xkhofmann-tfdidesign-md11-load-manager",
|
||||||
"diff": "^8.0.2"
|
"version": "0.0.1",
|
||||||
}
|
"description": "TFDi MD11 Load Manager project",
|
||||||
|
"scripts": {
|
||||||
|
"debugger": "cd \"$env:MSFS_SDK/Tools/CoherentGT Debugger\" && ./Debugger.exe",
|
||||||
|
"locale": "cd \"$env:MSFS_SDK/Tools/MSFS_Localization\" && ./MSFSLocalizationManager.exe",
|
||||||
|
"build": "pnpm -r build",
|
||||||
|
"release": "pnpm -r release",
|
||||||
|
"archive:2024": "Compress-Archive -Path Packages/xkhofmann-tfdidesign-md11-load-manager -DestinationPath Packages/xkhofmann-tfdidesign-md11-load-manager",
|
||||||
|
"package": "rimraf Packages && pnpm release && & \"$env:MSFS2024_SDK/Tools/bin/fspackagetool.exe\" -nopause xkhofmann-tfdidesign-md11-load-manager.xml && pnpm archive:2024"
|
||||||
|
},
|
||||||
|
"keywords": [],
|
||||||
|
"author": "Kilian Kurt Hofmann",
|
||||||
|
"license": "MIT",
|
||||||
|
"packageManager": "pnpm@10.25.0",
|
||||||
|
"engines": {
|
||||||
|
"node": ">=22"
|
||||||
|
},
|
||||||
|
"devDependencies": {
|
||||||
|
"diff": "^8.0.2"
|
||||||
|
},
|
||||||
|
"dependencies": {
|
||||||
|
"rimraf": "^6.1.3"
|
||||||
|
}
|
||||||
}
|
}
|
||||||
Generated
+6012
File diff suppressed because it is too large
Load Diff
@@ -0,0 +1,3 @@
|
|||||||
|
packages:
|
||||||
|
- PackageSources/js-bundle
|
||||||
|
- PackageSources/wasm-module
|
||||||
@@ -1,19 +1,51 @@
|
|||||||
{
|
{
|
||||||
"folders": [
|
"folders": [
|
||||||
{
|
{
|
||||||
"path": "."
|
"path": ".",
|
||||||
}
|
},
|
||||||
],
|
],
|
||||||
"settings": {
|
"settings": {
|
||||||
"cSpell.words": [
|
"cSpell.words": [
|
||||||
|
"AUXLWR",
|
||||||
|
"AUXUPR",
|
||||||
|
"bksp",
|
||||||
|
"CMCDU",
|
||||||
"couatl",
|
"couatl",
|
||||||
|
"Deboarded",
|
||||||
"DEBOARDED",
|
"DEBOARDED",
|
||||||
"deboarding",
|
"deboarding",
|
||||||
|
"Deinitialized",
|
||||||
|
"EXTCTL",
|
||||||
|
"FCOMs",
|
||||||
|
"FSDT",
|
||||||
|
"fspackagetool",
|
||||||
|
"FUELHOSE",
|
||||||
|
"FWDAUXL",
|
||||||
|
"FWDAUXR",
|
||||||
|
"HRESULT",
|
||||||
|
"htmlgauge",
|
||||||
|
"ISFD",
|
||||||
"khofmann",
|
"khofmann",
|
||||||
|
"LEMAC",
|
||||||
|
"LMCDU",
|
||||||
|
"mbelow",
|
||||||
|
"mexceeds",
|
||||||
|
"msfs",
|
||||||
|
"MSFS",
|
||||||
|
"nopause",
|
||||||
|
"NUMPASSENGERS",
|
||||||
|
"RMCDU",
|
||||||
|
"SIMCONNECT",
|
||||||
|
"SIMOBJECT",
|
||||||
|
"SIMOBJECTS",
|
||||||
"tfdi",
|
"tfdi",
|
||||||
"TFDI",
|
"TFDI",
|
||||||
|
"tfdidesign",
|
||||||
"TOCG",
|
"TOCG",
|
||||||
"ZFWCG"
|
"Vcockpit",
|
||||||
]
|
"xkhofmann",
|
||||||
}
|
"XPNDR",
|
||||||
|
"ZFWCG",
|
||||||
|
],
|
||||||
|
},
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -0,0 +1,9 @@
|
|||||||
|
<UserSettings>
|
||||||
|
<CheckedOutPackages>
|
||||||
|
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
|
||||||
|
</CheckedOutPackages>
|
||||||
|
<SelectedPackages/>
|
||||||
|
<Filter/>
|
||||||
|
<ShowOnlyEdited>false</ShowOnlyEdited>
|
||||||
|
</UserSettings>
|
||||||
|
|
||||||
Reference in New Issue
Block a user