70 Commits

Author SHA1 Message Date
Kilian 20aa5c2416 Update to 1.1.28 2026-04-05 17:21:46 +02:00
Kilian 01e0a155ed 1.1.26+ FS24 adjustments 2026-03-28 21:02:15 +01:00
Kilian b772119e2c 1.1.18 EFB 2026-02-21 04:25:26 +01:00
Kilian 4628c6646c 1.1.17 EFB 2026-02-16 22:57:09 +01:00
Kilian 487ed3f589 GSX synced loading of fuel 2026-02-13 21:34:56 +01:00
Kilian 69680ced03 Initial GSX Sync for fuel 2026-02-13 02:50:43 +01:00
Kilian 122a93461d Non GSX Fuel setting 2026-02-12 21:27:12 +01:00
Kilian 310b5f39dc Update to 1.1.14 2026-02-05 22:16:28 +01:00
Kilian 3b003f3363 update to 1.1.14 2026-02-05 01:04:29 +01:00
Kilian 818277edcf Build 1.1.0 2026-01-28 20:13:43 +01:00
Kilian 73ebaa311b Update configs for flap drag 2026-01-28 15:48:56 +01:00
Kilian d96ea55b31 Fix GSX deboarding 2026-01-24 21:11:40 +01:00
Kilian b379a6dccd Update to 1.1.9 2026-01-24 13:59:54 +01:00
Kilian 766d956008 2024 Build an working 2025-12-16 21:30:47 +01:00
Kilian ec9facd4d9 New Configs 2025-12-16 21:02:20 +01:00
Kilian d805d315f8 Small fixes 2025-12-13 13:57:58 +01:00
Kilian ccb96e15e2 Newest EFB 2025-12-07 02:09:41 +01:00
Kilian f708bbf72c Correct Configs 2025-12-06 18:11:39 +01:00
Kilian 695e02d143 fix configs 2025-12-06 18:05:12 +01:00
Kilian 22a41749d6 Integrated OSK 2025-12-02 21:05:59 +01:00
Kilian cd1f2048b0 Fix Auto Hide 2025-12-02 00:48:06 +01:00
Kilian dcc1161012 110 Upgrade 2025-11-30 16:16:39 +01:00
Kilian 98f72d5c83 Adj. to new structure >110 2025-11-30 03:49:39 +01:00
Kilian 5e60d0d45e 106 Upgrade 2025-11-20 16:43:32 +01:00
Kilian 872161bc8a Upgrade to 105 2025-11-17 18:17:39 +01:00
Kilian 9432dd1d84 Fully adj to 103 (no OSK yet) 2025-11-07 16:11:17 +01:00
Kilian 5ad5f16bdb Adj. to 103 2025-11-07 11:26:39 +01:00
Kilian 3d2e439674 Default Weights 2025-10-15 02:45:40 +02:00
Kilian 5a80249f0e Adj Panel CFG 2025-10-08 20:33:13 +02:00
Kilian 16de21ffec Adjust to new cabin 2025-10-02 21:04:15 +02:00
Kilian b266a82905 Clang stack usage 2025-09-29 11:41:16 +02:00
Kilian e27aee0f14 gitignore changes 2025-09-20 12:58:00 +02:00
Kilian ee43ae9363 Startup behaviour 2025-09-15 00:56:35 +02:00
Kilian acf4b9ee47 GSX Reset and Disable button 2025-09-09 23:40:24 +02:00
Kilian 04e5ec4251 Moved GSX state machine into WASM 2025-09-09 14:53:41 +02:00
Kilian dee5447bed Minimum occupancy for PAX 2025-09-08 14:15:10 +02:00
Kilian 9000d516ae Allow GSX state reset
Fix KG rounding of pax
2025-09-08 03:06:48 +02:00
Kilian d75518517a Refine GSX lockout 2025-09-08 02:00:35 +02:00
Kilian 95637c9f7f Show preview CG while GSX is loading 2025-09-05 19:21:01 +02:00
Kilian 1c7caf986a Type import 2025-09-05 19:09:01 +02:00
Kilian 95aef94c71 Include tank fix 2025-09-05 18:23:03 +02:00
Kilian 4ad0f4e3d6 Update patch 2025-08-29 19:02:42 +02:00
Kilian fcfb674522 EFB in output 2025-08-29 18:55:04 +02:00
Kilian 22b5617e39 Update to new EFB 2025-08-29 17:52:32 +02:00
Kilian d2a4846df6 SB Profile values 2025-07-08 14:19:38 +02:00
Kilian a5802f46d5 Fix Fuel lockout 2025-07-08 10:54:00 +02:00
Kilian d59ffb5e76 Update Readme 2025-07-04 22:17:45 +02:00
Kilian 57186d44b9 Loaded state save 2025-07-04 22:17:21 +02:00
Kilian c7e9bff5e2 2024 compatible 2025-07-04 17:25:50 +02:00
Kilian 9bb92371bc Remove ingame panel def. 2025-07-03 22:03:40 +02:00
Kilian 09397edef9 Integration finished 2025-07-03 21:22:06 +02:00
Kilian 8952aba12d Rem EFB 2025-07-03 15:35:02 +02:00
Kilian 6e6a5b6103 EFB Patch 2025-07-03 15:34:03 +02:00
Kilian ed48918831 initial EFB 2025-07-03 15:28:51 +02:00
Kilian a8a827b253 Try two 2025-07-03 15:24:32 +02:00
Kilian 93c7815d96 Base 2025-07-03 09:48:54 +02:00
Kilian 80cb726501 Customisable pax/bag weight
Better log
2025-06-21 21:41:17 +02:00
Kilian 2047c84d8d Fix SB persist 2025-06-19 16:05:54 +02:00
Kilian 390edd29b8 SB persist
Options page for GSX Sync
2025-06-18 23:57:46 +02:00
Kilian 4b60f8eec2 Rmv wasm build artifact 2025-06-15 02:01:03 +02:00
Kilian 9da2abdad7 Freighter 2025-06-15 01:57:28 +02:00
Kilian cbd7d4e0ae Check prog pax load/unload 2025-06-14 16:47:27 +02:00
Kilian c394cd4d7b GSX Synced boarding/deboarding 2025-06-14 03:34:22 +02:00
Kilian f7304c5c7b Setting of payload 2025-06-12 14:30:00 +02:00
Kilian 8975ea17af SB fetch and entry 2025-06-11 23:49:35 +02:00
Kilian 896a459bba Pax Station Entry 2025-06-11 17:30:36 +02:00
Kilian 890622453e Cleanup old configs 2025-06-11 00:44:15 +02:00
Kilian ee46d0bff1 ZFW Target Set 2025-06-11 00:27:27 +02:00
Kilian 9224300c85 WASM PAX data export 2025-06-10 01:12:58 +02:00
Kilian a34c532484 initial wasm commit 2025-06-09 07:04:32 +02:00
104 changed files with 15895 additions and 11470 deletions
+6
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@@ -0,0 +1,6 @@
---
BasedOnStyle: LLVM
ColumnLimit: 130
IndentCaseLabels: true
AllowShortIfStatementsOnASingleLine: Always
AllowShortLoopsOnASingleLine: true
+381 -2
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@@ -1,8 +1,387 @@
## 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
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*.rsp
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*.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
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*.psess
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# Visual Studio Trace Files
*.e2e
# TFS 2012 Local Workspace
$tf/
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*.gpState
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_ReSharper*/
*.[Rr]e[Ss]harper
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_TeamCity*
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*.dotCover
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*.coveragexml
# NCrunch
_NCrunch_*
.*crunch*.local.xml
nCrunchTemp_*
# MightyMoose
*.mm.*
AutoTest.Net/
# Web workbench (sass)
.sass-cache/
# Installshield output folder
[Ee]xpress/
# DocProject is a documentation generator add-in
DocProject/buildhelp/
DocProject/Help/*.HxT
DocProject/Help/*.HxC
DocProject/Help/*.hhc
DocProject/Help/*.hhk
DocProject/Help/*.hhp
DocProject/Help/Html2
DocProject/Help/html
# Click-Once directory
publish/
# Publish Web Output
*.[Pp]ublish.xml
*.azurePubxml
# Note: Comment the next line if you want to checkin your web deploy settings,
# but database connection strings (with potential passwords) will be unencrypted
*.pubxml
*.publishproj
# Microsoft Azure Web App publish settings. Comment the next line if you want to
# checkin your Azure Web App publish settings, but sensitive information contained
# in these scripts will be unencrypted
PublishScripts/
# NuGet Packages
*.nupkg
# NuGet Symbol Packages
*.snupkg
# The packages folder can be ignored because of Package Restore
**/[Pp]ackages/*
# except build/, which is used as an MSBuild target.
!**/[Pp]ackages/build/
# Uncomment if necessary however generally it will be regenerated when needed
#!**/[Pp]ackages/repositories.config
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*.nuget.targets
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*.build.csdef
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*.[Cc]ache
# but keep track of directories ending in .cache
!?*.[Cc]ache/
# Others
ClientBin/
~$*
*~
*.dbmdl
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# 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/
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# to a newer Visual Studio version. Backup files are not needed,
# because we have git ;-)
_UpgradeReport_Files/
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*- [Bb]ackup.rdl
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*- [Bb]ackup ([0-9][0-9]).rdl
# Microsoft Fakes
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.fake/
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# tools/**
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.mfractor/
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.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
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/MSFS
*.blend1 node_modules
*.blend1
*.tsbuildinfo
PackageSources/SimObjects/Airplanes/**/*.wasm
EFB/efb.css
EFB/efb.js
EFB/efb.html
EFB/efb.index.js
EFB/patched/
*.su
+29
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@@ -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
}
+3
View File
@@ -18,5 +18,8 @@
}, },
"[xml]": { "[xml]": {
"editor.defaultFormatter": "redhat.vscode-xml" "editor.defaultFormatter": "redhat.vscode-xml"
},
"[typescriptreact]": {
"editor.defaultFormatter": "esbenp.prettier-vscode"
} }
} }
+14
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@@ -0,0 +1,14 @@
Index: EFB.html
===================================================================
--- EFB.html
+++ EFB.html
@@ -4,7 +4,8 @@
</div>
</script>
-<script type="text/html" import-async="false" import-script="/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.index.js"></script>
+<script type="text/html" import-async="false" import-script="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/efb.index.js"></script>
<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.css" />
+<link rel="stylesheet" href="/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.css" />
+15
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@@ -0,0 +1,15 @@
Index: EFB.index.js
===================================================================
--- EFB.index.js
+++ EFB.index.js
@@ -27,9 +27,9 @@
}
connectedCallback() {
super.connectedCallback();
- Include.addScript("/Pages/VCockpit/Instruments/aircraft_efb/TFDi_MD11_efb/efb.js");
+ Include.addScript("/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/efb.js");
}
Update() {
super.Update();
+46
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@@ -0,0 +1,46 @@
Index: EFB.js
===================================================================
--- EFB.js
+++ EFB.js
@@ -50833,11 +50833,11 @@
),
/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
"button",
{
- onClick: loadPayload,
+ 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"
}
),
/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
"button",
@@ -51343,8 +51343,27 @@
] })
] }) }) });
}
+// Exports for add. script
+ window.reactExports = __toESM(require_react());
+ window.reactDomExports = __toESM(require_react_dom());
+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
+ window.useSelector = useSelector;
+ window.v4 = v4_default;
+ window.ArrowBigUp = ArrowBigUp;
+ window.Delete = Delete;
+ window.Space = Space;
+ window.X = X;
+ // Include
+ var script = document.createElement('script');
+ script.onload = function () {
+ console.log("LM App injected");
+ routes["/payload"].page = window.KH_LM
+ };
+ script.src = "/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb/App.js";
+ document.head.appendChild(script); //or something of the likes
+
// src/components/Router.tsx
init_common();
var import_jsx_runtime15 = __toESM(require_jsx_runtime());
var routes = {
+26
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@@ -0,0 +1,26 @@
const { createTwoFilesPatch } = require("diff");
const fs = require("fs");
// HTML
let file1Contents = fs.readFileSync("EFB.html").toString();
let file2Contents = fs.readFileSync("patched/EFB.html").toString();
let patch = createTwoFilesPatch(
"EFB.html",
"EFB.html",
file1Contents,
file2Contents
);
fs.writeFileSync("efb-html.patch", patch);
// JS
file1Contents = fs.readFileSync("EFB.index.js").toString();
file2Contents = fs.readFileSync("patched/EFB.index.js").toString();
patch = createTwoFilesPatch("EFB.index.js", "EFB.index.js", file1Contents, file2Contents);
fs.writeFileSync("efb-index-js.patch", patch);
file1Contents = fs.readFileSync("EFB.js").toString();
file2Contents = fs.readFileSync("patched/EFB.js").toString();
patch = createTwoFilesPatch("EFB.js", "EFB.js", file1Contents, file2Contents);
fs.writeFileSync("efb-js.patch", patch);
@@ -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>
@@ -20,21 +21,26 @@
<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>
<AssetDir>PackageSources\html_ui\</AssetDir> <AssetDir>PackageSources\html_ui\</AssetDir>
<OutputDir>html_ui\</OutputDir> <OutputDir>html_ui\</OutputDir>
<Config>
<Exclude>vendor-*</Exclude>
</Config>
</AssetGroup> </AssetGroup>
<AssetGroup Name="load-manager-panel"> <AssetGroup Name="wasm">
<Type>SPB</Type> <Type Version="0">Copy</Type>
<Flags> <Flags>
<FSXCompatibility>false</FSXCompatibility> <FSXCompatibility>false</FSXCompatibility>
</Flags> </Flags>
<AssetDir>PackageSources\load-manager-panel\</AssetDir> <AssetDir>PackageSources\SimObjects\Airplanes\</AssetDir>
<OutputDir>InGamePanels\</OutputDir> <OutputDir>SimObjects\Airplanes\</OutputDir>
<Config>
<Exclude>.gitkeep</Exclude>
</Config>
</AssetGroup> </AssetGroup>
</AssetGroups> </AssetGroups>
</AssetPackage> </AssetPackage>
@@ -0,0 +1,59 @@
// Panel Configuration File
// TFDi Design MD-11
[VCockpit01]
size_mm=2048,2048
visible=1
pixel_size=2048,2048
texture=vc1
background_color=0,0,0
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU1,0,0,509,510
htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU2,514,0,510,510
htmlgauge02=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU3,1027,0,510,510
htmlgauge03=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU4,1539,0,510,510
htmlgauge04=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU5,0,513,511,510
htmlgauge05=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=DU6,513,512,510,511
htmlgauge06=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=LMCDU, 0,1050,666,574
htmlgauge07=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RMCDU,678,1050,666,574
htmlgauge08=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=CMCDU,1353,1050,666,574
htmlgauge09=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=ISFD,1032,519,544,505
htmlgauge10=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=Core,0,0,1,1
//KH new gauge
htmlgauge11=WasmInstrument/WasmInstrument.html?wasm_module=load-manager.wasm&wasm_gauge=Load_Manager,0,0,509,510
[VIEWS]
VIEW_FORWARD_DIR=2.000, 0.000, 0.000
[Color]
Day=255,255,255
Night=255,255,255
Luminous=201,64,64
[Vcockpit02]
Background_color=0,0,0
size_mm=1024,1024
visible=1
pixel_size=1024,1024
texture=vc2
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=AFS,3,0,1015,185
htmlgauge01=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=FUEL,4,200,1016,196
//above should actually be 3,192,1018,199 - moved due to visual offset
[Vcockpit03]
Background_color=0,0,0
size_mm=1024,1024
visible=1
pixel_size=1024,1024
texture=RADIOS_XPNDR
htmlgauge00=WasmInstrument/WasmInstrument.html?wasm_module=md11host.wasm&wasm_gauge=RADIOS_XPNDR,0,5,1019,295
[VCockpit04]
Background_color=0,0,0
size_mm=1536,1024
visible=1
pixel_size=1536,1024
texture=EFB
htmlgauge00=aircraft_efb/KH_TFDi_MD11_efb/efb.html,0,0,1536,1024
@@ -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
@@ -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
@@ -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
@@ -0,0 +1,419 @@
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
empty_weight_roll_MOI = 6368555
empty_weight_yaw_MOI = 40761191
empty_weight_coupled_MOI = 0
activate_mach_limit_based_on_cg = 0
activate_cg_limit_based_on_mach = 0
max_number_of_stations = 21
//KH START Empty default
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
//KH END
[CONTACT_POINTS]
static_pitch = 0
static_cg_height = 16.4
gear_system_type = 1
tailwheel_lock = 0
max_number_of_points = 16
gear_locked_on_ground = 0
gear_locked_above_speed = -1
max_speed_full_steering = 25
min_available_steering_angle_pct = 0.2
max_speed_decreasing_steering = 45
max_speed_full_steering_castering = 20
max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 3.142
allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
[FUEL]
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
engine_driven_pump = 1
manual_transfer_pump = 0
manual_pump = 0
anemometer_pump = 0
fuel_dump_rate = 0.02
default_fuel_tank_selector.1 = 1
default_fuel_tank_selector.2 = 1
default_fuel_tank_selector.3 = 1
[AIRPLANE_GEOMETRY]
wing_area = 3648
wing_span = 170.5
wing_root_chord = 34.68
wing_camber = 1
wing_thickness_ratio = 0.04
wing_dihedral = 2.2
wing_incidence = 1.5
wing_twist = -0.5
oswald_efficiency_factor = 0.72
wing_winglets_flag = 1
wing_sweep = 38
wing_pos_apex_lon = 1
wing_pos_apex_vert = -2.75
htail_area = 920
htail_span = 59.5
htail_pos_lon = -88
htail_pos_vert = 5.0
htail_incidence = 0.8
htail_sweep = 36.5
htail_thickness_ratio = 0.02
vtail_area = 760
vtail_span = 28.1
vtail_sweep = 43
vtail_pos_lon = -79.5
vtail_pos_vert = 28
vtail_thickness_ratio = 0.03
fuselage_length = 200.92
fuselage_diameter = 19.75
fuselage_center_pos = 10, 0, 1.0
elevator_area = 327.0
aileron_area = 225.0
rudder_area = 190.0
elevator_up_limit = 25
elevator_down_limit = 15
aileron_up_limit = 25
aileron_down_limit = 15
rudder_limit = 23
rudder_trim_limit = 20
elevator_trim_limit = 30
spoiler_limit = 60
spoilerons_available = 1
aileron_to_spoileron_gain = 3
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoiler_extension_time = 2.0
spoiler_handle_available = 1
auto_spoiler_available = 1
auto_spoiler_auto_retracts = 0
auto_spoiler_min_speed = 72
positive_g_limit_flaps_up = 5.0
positive_g_limit_flaps_down = 4.0
negative_g_limit_flaps_up = -4.0
negative_g_limit_flaps_down = -3.0
load_safety_factor = 1.5
elevator_trim_neutral = -1
aileron_to_rudder_scale = 0
flap_to_aileron_scale = 0
fly_by_wire = 0
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
[AERODYNAMICS]
lift_coef_pitch_rate = -8.09375
lift_coef_daoa = 2.68359
lift_coef_delta_elevator = -0.28906
lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
side_force_roll_rate = 0.15478
side_force_yaw_rate = 0
side_force_delta_rudder = -0.14746
pitch_moment_horizontal_incidence = 4.24755
pitch_moment_delta_elevator = -2.37011
pitch_moment_delta_trim = 0
pitch_moment_pitch_damping = -214.1455
pitch_moment_aoa_0 = 0.11621
pitch_moment_daoa = 8.87255
pitch_moment_flaps = 0.0105
pitch_moment_gear = 0.0171
pitch_moment_spoilers = 0
pitch_moment_delta_elevator_propwash = -2.37011
pitch_moment_pitch_propwash = -214.1455
roll_moment_slip_angle = 0.26855
roll_moment_roll_damping = -3.40869
roll_moment_yaw_rate = -0.27197
roll_moment_spoilers = 0.07
roll_moment_delta_aileron = -0.34521
roll_moment_delta_rudder = 0.01660
roll_moment_delta_aileron_trim_scalar = -0.2
yaw_moment_slip_angle = 0.18066
yaw_moment_roll = 0.07470
yaw_moment_yaw_damping = -2.49023
yaw_moment_yaw_propwash = 0
yaw_moment_delta_aileron = -0.00683
yaw_moment_delta_rudder = 0.07128
yaw_moment_delta_rudder_propwash = 0.075
yaw_moment_delta_rudder_trim_scalar = -0.2
compute_aero_center = 0
aero_center_lift = -13.75
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
lift_coef_mach_table = 0:1
lift_coef_delta_elevator_mach_table = 0:0
lift_coef_daoa_mach_table = 0:0
lift_coef_pitch_rate_mach_table = 0:0
lift_coef_horizontal_incidence_mach_table = 0:0
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
side_force_slip_angle_mach_table = 0:0
side_force_delta_rudder_mach_table = 0:0
side_force_yaw_rate_mach_table = 0:0
side_force_roll_rate_mach_table = 0:0
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
pitch_moment_horizontal_incidence_aoa_table = 0:1
pitch_moment_daoa_aoa_table = 0:1
pitch_moment_pitch_alpha_table = 0:1
pitch_moment_delta_elevator_mach_table = 0:0
pitch_moment_daoa_mach_table = 0:0
pitch_moment_pitch_rate_mach_table = 0:0
pitch_moment_horizontal_incidence_mach_table = 0:0
pitch_moment_aoa_0_mach_table = 0:0
roll_moment_aoa_table = 0:0
roll_moment_slip_angle_aoa_table = 0:1
roll_moment_roll_rate_aoa_table = 0:1
roll_moment_delta_aileron_aoa_table = 0:1
roll_moment_slip_angle_mach_table = 0:0
roll_moment_delta_rudder_mach_table = 0:0
roll_moment_delta_aileron_mach_table = 0:0
roll_moment_yaw_rate_mach_table = 0:0
roll_moment_roll_rate_mach_table = 0:0
yaw_moment_aoa_table = 0:0
yaw_moment_slip_angle_aoa_table = 0:1
yaw_moment_yaw_rate_aoa_table = 0:1
yaw_moment_delta_rudder_aoa_table = 0:1
yaw_moment_slip_angle_mach_table = 0:0
yaw_moment_delta_rudder_mach_table = 0:0
yaw_moment_delta_aileron_mach_table = 0:0
yaw_moment_yaw_rate_mach_table = 0:0
yaw_moment_roll_rate_mach_table = 0:0
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
aileron_scaling_table = -0.785:1 ;0:1
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
elevator_lift_coef=3
rudder_lift_coef=2
aileron_load_factor_effectiveness_table = 0:1
lift_coef_at_drag_zero = 0.1
lift_coef_at_drag_zero_flaps = 0.1
[FLIGHT_TUNING]
modern_fm_only = 1
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
rudder_maxangle_scalar = 1
pitch_stability = 5
roll_stability = 1
yaw_stability = 1
pitch_gyro_stability = 1
roll_gyro_stability = 1
yaw_gyro_stability = 1
empty_CG_deviation_limit=0
elevator_trim_effectiveness = 1.5
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 0
hi_alpha_on_yaw = 0
p_factor_on_yaw = 0
torque_on_roll = 0
gyro_precession_on_roll = 0
gyro_precession_on_yaw = 0
engine_wash_on_roll = 0
wingflex_scalar = 2
wingflex_offset = 0
stall_coef_at_min_weight = 0.71
ground_crosswind_effect_zero_speed=10
ground_crosswind_effect_max_speed=150
ground_high_speed_steeringwheel_static_friction_scalar=1.5
ground_high_speed_otherwheel_static_friction_scalar=1.2
[REFERENCE SPEEDS]
full_flaps_stall_speed = 115
flaps_up_stall_speed = 149
cruise_speed = 345
cruise_mach = 0.85
crossover_speed = 330
max_mach = 0.9
max_indicated_speed = 395
max_flaps_extended = 170
normal_operating_speed = 325
airspeed_indicator_max = 562.5
rotation_speed_min = 145
climb_speed = 250
cruise_alt = 41000
takeoff_speed = 165
spawn_cruise_altitude = 5000
spawn_descent_altitude = 500
best_angle_climb_speed = 0
approach_speed = 0
best_glide = 0
max_gear_extended = 200
[INTERACTIVE POINTS]
number_of_interactive_points = 13
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
[STALL PROTECTION]
stall_protection = 1 ; Alpha Protection
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
;===================== FLAPS =====================
[FLAPS.0]
type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
pitch_scalar = 1
max_on_ground_position = 7
flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1]
type = 1
system_type = 1
span-outboard = 0.7
extending-time = 23
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
pitch_scalar = 1
max_on_ground_position = 7
flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2]
type = 2
system_type = 1
span-outboard = 0.2
extending-time = 8
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, 215, 0.5, 0.5
[FLAPS.3]
type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, 215, 0.5, 0.5
@@ -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
@@ -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
@@ -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
@@ -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
+7
View File
@@ -1 +1,8 @@
/// <reference types="@microsoft/msfs-types/js/common.d.ts" /> /// <reference types="@microsoft/msfs-types/js/common.d.ts" />
/// <reference types="@microsoft/msfs-types/pages/vcockpit/instruments/shared/baseinstrument.d.ts" />
/// <reference types="@microsoft/msfs-types/js/datastorage.d.ts" />
/// <reference types="@microsoft/msfs-types/js/buttons.d.ts" />
/// <reference types="@microsoft/msfs-types/js/services/toolbarpanels.d.ts" />
/// <reference types="@microsoft/msfs-types/js/simvar.d.ts" />
function useSelector(selector: (state: any) => any): any;
+11 -14
View File
@@ -1,6 +1,6 @@
{ {
"name": "tfdidesign-md11-load-manager", "name": "js-bundle",
"version": "0.1.14", "version": "0.2.34",
"description": "", "description": "",
"main": "index.js", "main": "index.js",
"type": "module", "type": "module",
@@ -10,10 +10,11 @@
"licenses": "license-report --output=markdown > ./src/assets/licenses_node.md", "licenses": "license-report --output=markdown > ./src/assets/licenses_node.md",
"debugger": "cd \"%MSFS_SDK%\\Tools\\CoherentGT Debugger\" && Debugger.exe", "debugger": "cd \"%MSFS_SDK%\\Tools\\CoherentGT Debugger\" && Debugger.exe",
"locale": "cd \"%MSFS_SDK%\\Tools\\MSFS_Localization\" && MSFSLocalizationManager.exe", "locale": "cd \"%MSFS_SDK%\\Tools\\MSFS_Localization\" && MSFSLocalizationManager.exe",
"clean": "rimraf ..\\html_ui\\Pages\\VCockpit\\Instruments\\aircraft_efb\\KH_TFDi_MD11_efb",
"dev": "npx rollup -c -w", "dev": "npx rollup -c -w",
"clean": "rimraf ../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel/ && rimraf .rollup.cache", "build": "npm version patch && npx rollup -c && pnpm efb",
"build": "npm version patch && npx rollup -c", "release": "pnpm types && pnpm lint && pnpm run licenses && pnpm clean && npm version patch && cross-env NODE_ENV=production npx rollup -c && pnpm efb ",
"release": "pnpm types && pnpm lint && pnpm run licenses && pnpm clean && npm version patch && cross-env NODE_ENV=production npx rollup -c" "efb": "cd ..\\.. && node insert-efb && rm PackageSources\\html_ui\\Pages\\VCockpit\\Instruments\\aircraft_efb\\KH_TFDi_MD11_efb/vendor*"
}, },
"engines": { "engines": {
"node": ">=22" "node": ">=22"
@@ -29,6 +30,7 @@
"@rollup/plugin-replace": "^6.0.2", "@rollup/plugin-replace": "^6.0.2",
"@rollup/plugin-terser": "^0.4.4", "@rollup/plugin-terser": "^0.4.4",
"@rollup/plugin-typescript": "^12.1.2", "@rollup/plugin-typescript": "^12.1.2",
"@types/node": "^24.3.1",
"@types/react": "^19.1.6", "@types/react": "^19.1.6",
"@types/react-dom": "^19.1.6", "@types/react-dom": "^19.1.6",
"@types/uuid": "^10.0.0", "@types/uuid": "^10.0.0",
@@ -52,20 +54,15 @@
"rollup-plugin-react-svg": "^3.0.3", "rollup-plugin-react-svg": "^3.0.3",
"rollup-plugin-version-injector": "^1.3.3", "rollup-plugin-version-injector": "^1.3.3",
"sass": "^1.89.1", "sass": "^1.89.1",
"svg-slim": "^2.0.5",
"tslib": "^2.8.1", "tslib": "^2.8.1",
"typed-scss-modules": "^8.1.1", "typed-scss-modules": "^8.1.1",
"typescript": "5.8.3" "typescript": "5.8.3"
}, },
"dependencies": { "dependencies": {
"@emotion/react": "^11.11.1", "lucide-react": "^0.555.0",
"@emotion/styled": "^11.11.0", "react": "^19.1.0",
"@mui/icons-material": "^5.14.16", "react-dom": "^19.1.0",
"@mui/material": "^5.14.17", "uuid": "^11.1.0"
"postcss-import": "^15.1.0",
"react": "^18.2.0",
"react-dom": "^18.2.0",
"uuid": "^9.0.1"
}, },
"packageManager": "pnpm@10.11.1+sha512.e519b9f7639869dc8d5c3c5dfef73b3f091094b0a006d7317353c72b124e80e1afd429732e28705ad6bfa1ee879c1fce46c128ccebd3192101f43dd67c667912" "packageManager": "pnpm@10.11.1+sha512.e519b9f7639869dc8d5c3c5dfef73b3f091094b0a006d7317353c72b124e80e1afd429732e28705ad6bfa1ee879c1fce46c128ccebd3192101f43dd67c667912"
} }
+387 -1101
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+16 -24
View File
@@ -2,7 +2,6 @@ import commonjs from '@rollup/plugin-commonjs';
import json from '@rollup/plugin-json'; import json from '@rollup/plugin-json';
import resolve from '@rollup/plugin-node-resolve'; import resolve from '@rollup/plugin-node-resolve';
import replace from '@rollup/plugin-replace'; import replace from '@rollup/plugin-replace';
import terser from '@rollup/plugin-terser';
import typescript from '@rollup/plugin-typescript'; import typescript from '@rollup/plugin-typescript';
import autoprefixer from 'autoprefixer'; import autoprefixer from 'autoprefixer';
import atImport from 'postcss-import'; import atImport from 'postcss-import';
@@ -10,29 +9,29 @@ import copy from 'rollup-plugin-copy';
import postcss from 'rollup-plugin-postcss'; import postcss from 'rollup-plugin-postcss';
import reactSvg from 'rollup-plugin-react-svg'; import reactSvg from 'rollup-plugin-react-svg';
import versionInjector from 'rollup-plugin-version-injector'; import versionInjector from 'rollup-plugin-version-injector';
import svgs from 'svg-slim';
const { NODE_ENV: targetEnv = 'development' } = process.env; const { NODE_ENV: targetEnv = 'development' } = process.env;
const outDirBase = '../html_ui'; const outDirBase = '../html_ui';
const panelDirBase = `${outDirBase}/InGamePanels/tfdidesign-md11-load-manager-panel`; const panelDirBase = `${outDirBase}/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb`;
function svgSlim(code, id) {
if (!id.endsWith('.svg')) return code;
return svgs(code.toString(), {}).then((res) => res);
}
export default { export default {
input: 'src/index.ts', input: 'src/App.tsx',
output: { output: {
dir: panelDirBase, dir: panelDirBase,
format: 'es', format: 'es',
sourcemap: targetEnv !== 'production', sourcemap: targetEnv !== 'production',
manualChunks: (id) => {
if (id.includes('node_modules')) {
return 'vendor';
}
return null;
},
}, },
plugins: [ plugins: [
replace({ replace({
'process.env.NODE_ENV': JSON.stringify(targetEnv), 'process.env.NODE_ENV': targetEnv,
'import.meta.env': true, preventAssignment: true,
'import.meta.env.MODE': JSON.stringify(targetEnv),
}), }),
versionInjector(), versionInjector(),
postcss({ postcss({
@@ -45,22 +44,15 @@ export default {
reactSvg(), reactSvg(),
resolve(), resolve(),
json(), json(),
typescript(), typescript({
outputToFilesystem: false,
}),
commonjs({ commonjs({
requireReturnsDefault: 'auto', requireReturnsDefault: 'auto',
}), }),
targetEnv === 'production' && terser(), // targetEnv === 'production' && terser(), // Disabled due to script running afterwards
copy({ copy({
targets: [ targets: [{ src: ['src/assets/*', '!**/*.svg'], dest: `${panelDirBase}/assets` }],
{ src: ['src/assets/*', '!**/*.svg'], dest: `${panelDirBase}/assets` },
{ src: 'src/assets/img/*', dest: `${panelDirBase}/assets/img`, transform: svgSlim },
{ src: ['src/index.html'], dest: `${panelDirBase}` },
{
src: ['src/assets/ICON_TFDIDESIGN_MD11_LOAD_MANAGER.svg'],
dest: [`${outDirBase}/icons/toolbar`, `${outDirBase}/Textures/Menu/toolbar`],
transform: svgSlim,
},
],
}), }),
], ],
onwarn: function (warning, warn) { onwarn: function (warning, warn) {
@@ -1,9 +0,0 @@
@import 'fonts/300.css';
@import 'fonts/400.css';
@import 'fonts/500.css';
@import 'fonts/700.css';
.app {
width: 100%;
height: 100%;
}
+39 -106
View File
@@ -1,126 +1,59 @@
import { FC, StrictMode, useCallback, useEffect, useRef, useState } from 'react'; import { FC, useCallback, useEffect, useState } from 'react';
import Freight from './components/freight/Freight'; import Freighter from './components/freighter/Freighter';
import Pax from './components/pax/Pax'; import Pax from './components/pax/Pax';
import { PayloadFreight, calculateCGsFreight, getWeightsFreight } from './configs/freighter'; import { COHERENT_COMM_BUS_WASM_CALL } from './constants';
import { PaxConfig, PayloadPax } from './configs/pax'; import { WASMDataF, WASMDataPax } from './types/WASMData';
import { Fuel, getFuel, initialFuel, initialPayload } from './configs/shared'; import { CommBusCall, CommBusEvent } from './types/general';
interface IAppProps { const App: FC = () => {
commBus: ViewListener.ViewListener;
}
const App: FC<IAppProps> = ({ commBus }) => {
// Inferred
const [unit, setUnit] = useState<'lbs' | 'kg'>('lbs');
const [isCargo, setIsCargo] = useState(false);
const [isER, setIsER] = useState(false);
const [SBUsername, setSBUsername] = useState<string>(); const [SBUsername, setSBUsername] = useState<string>();
const [WASMData, setWASMData] = useState<WASMDataPax | WASMDataF>();
// From sim
const [payloadLive, setPayloadLive] = useState<PayloadPax | PayloadFreight>(initialPayload);
const [fuel, setFuel] = useState<Fuel>(initialFuel);
const [GSXPaxNum, setGSXPaxNum] = useState(0);
const [GSXCargoPercent, setGSXCargoPercent] = useState(0);
const [GSXState, setGSXState] = useState<'boarding' | 'deboarding' | 'idle'>('idle');
// Calculated
const [CGs, setCGs] = useState<[number, number]>([0, 0]);
const [isReady, setIsReady] = useState(false);
const requestRef = useRef<number | undefined>(undefined);
// Main Loop for Live Payload
const mainLoop = () => {
try {
if (SimVar.IsReady()) {
setIsER(SimVar.GetSimVarValue('L:MD11_OPT_ER', 'bool'));
setIsCargo(SimVar.GetSimVarValue('L:MD11_EFB_IS_CARGO', 'bool'));
setUnit((SimVar.GetSimVarValue('L:MD11_EFB_OPTIONS_GENERAL', 'number') & 1) << 0 ? 'lbs' : 'kg');
// GSX
const boardingState = SimVar.GetSimVarValue('L:FSDT_GSX_BOARDING_STATE', 'number');
const deboardingState = SimVar.GetSimVarValue('L:FSDT_GSX_DEBOARDING_STATE', 'number');
setGSXState(boardingState === 5 ? 'boarding' : deboardingState === 5 ? 'deboarding' : 'idle');
setGSXPaxNum(
boardingState === 5
? SimVar.GetSimVarValue('L:FSDT_GSX_NUMPASSENGERS_BOARDING_TOTAL', 'number')
: deboardingState === 5
? SimVar.GetSimVarValue('L:FSDT_GSX_NUMPASSENGERS_DEBOARDING_TOTAL', 'number')
: 0
);
setGSXCargoPercent(
boardingState === 5
? SimVar.GetSimVarValue('L:FSDT_GSX_BOARDING_CARGO_PERCENT', 'number')
: deboardingState === 5
? 100 - SimVar.GetSimVarValue('L:FSDT_GSX_DEBOARDING_CARGO_PERCENT', 'number')
: 0
);
const payload = isCargo ? getWeightsFreight(unit) : PaxConfig.getWeights(unit);
const _fuel = getFuel(unit);
setCGs(
isCargo
? calculateCGsFreight(payload as PayloadFreight, _fuel)
: PaxConfig.calculateCGs(payload as PayloadPax, _fuel)
);
setPayloadLive(payload);
setFuel(_fuel);
}
} catch {}
requestRef.current = requestAnimationFrame(mainLoop);
};
useEffect(() => {
requestRef.current = requestAnimationFrame(mainLoop);
if (requestRef.current !== undefined) return () => cancelAnimationFrame(requestRef.current as number);
}, [unit, isCargo]);
// CommBus // CommBus
const usernameCallback = useCallback((username: string) => { const usernameCallback = useCallback((username: string) => {
setSBUsername(username); setSBUsername(username);
setIsReady(true); }, []);
const wasmCallback = useCallback((data: string) => {
setWASMData(JSON.parse(data));
}, []); }, []);
useEffect(() => { useEffect(() => {
console.log('Initializing CommBus'); console.log(
'[KHOFMANN TFDi MD-11 Load Manager] JS Version [VI]{version}[/VI]: process.env.NODE_ENV [VI]{date}[/VI]'
);
commBus.on('receiveSimBriefUsername', usernameCallback); console.log('[KHOFMANN TFDi MD-11 Load Manager] Initialising CommBus');
setTimeout(() => { const commBus = RegisterViewListener('JS_LISTENER_COMM_BUS');
Coherent.call('COMM_BUS_WASM_CALLBACK', 'requestSimBriefUsername', 'null');
}, 1000);
return () => commBus.off('receiveSimBriefUsername', usernameCallback); commBus.on(CommBusEvent.TFDI_SIMBRIEF_USERNAME, usernameCallback);
commBus.on(CommBusEvent.LIVE_DATA, wasmCallback);
Coherent.call(COHERENT_COMM_BUS_WASM_CALL, CommBusCall.TFDI_SIMBRIEF_USERNAME, 'null');
return () => {
console.log('[KHOFMANN TFDi MD-11 Load Manager] De-Initialising CommBus');
commBus.off(CommBusEvent.TFDI_SIMBRIEF_USERNAME, usernameCallback);
commBus.off(CommBusEvent.LIVE_DATA, wasmCallback);
commBus.unregister();
};
}, []); }, []);
return ( return (
<StrictMode> <div className="flex w-full justify-center py-5 bg-zinc-900">
<div className="flex w-full justify-center pt-2 bg-zinc-900"> <div className="flex w-3/4 flex-col items-center">
<div className="flex w-3/4 flex-col items-center"> {WASMData ? (
{isReady ? ( WASMData.userData.isCargo ? (
isCargo ? ( <Freighter WASMData={WASMData as WASMDataF} username={SBUsername} />
<Freight isER={isER} unit={unit} OEW={payloadLive.empty} CGs={CGs} />
) : (
<Pax
isER={isER}
unit={unit}
CGs={CGs}
fuelLive={fuel}
payloadLive={payloadLive as PayloadPax}
username={SBUsername}
GSXPaxNum={GSXPaxNum}
GSXCargoPercent={GSXCargoPercent}
GSXState={GSXState}
/>
)
) : ( ) : (
<h1 className="text-sm font-medium">LOADING</h1> <Pax WASMData={WASMData as WASMDataPax} username={SBUsername} />
)} )
</div> ) : (
<h1 className="text-sm font-medium">LOADING</h1>
)}
</div> </div>
</StrictMode> </div>
); );
}; };
@@ -1,10 +0,0 @@
<svg xmlns="http://www.w3.org/2000/svg" viewBox="0 0 54 35">
<path
d="M17.08737 32.03408c-6.24 0-11.298-5.216-11.298-11.651 0-6.434 5.058-11.651 11.298-11.651s11.298 5.217 11.298 11.651c0 .679-.059 1.343-.167 1.989l1.052.29c.13-.741.202-1.502.202-2.281 0-7.082-5.579-12.823-12.46-12.823-6.881 0-12.46 5.741-12.46 12.823 0 7.081 5.579 12.822 12.46 12.822 4.524 0 8.485-2.482 10.668-6.196h-1.301c-2.039 3.037-5.439 5.027-9.292 5.027" />
<path
d="M43.10237.39308s-1.764 2.479-3.978 5.076c-2.212 2.595-4.01 4.393-4.01 4.393l-.166-.716-.766-.116s2.147-2.33 4.343-4.56c2.197-2.23 4.577-4.077 4.577-4.077" />
<path
d="M34.63157 9.42938s-.316 1.082-.732 1.547c-.416.466-.949.649-1.431 1.065-.483.417-1.964 2.031-1.964 2.031s-5.525 5.974-9.186 9.302c-3.661 3.329-8.058 7.009-11.183 8.837-3.129 1.831-5.675 2.912-7.805 2.147-2.13-.766-2.32-2.96-1.864-4.693.416-1.581 1.598-2.646 1.598-2.646s-1.698 1.88-1.664 3.977c.014.899.299 1.664.732 2.23.251.328 1.794 1.632 4.476.766 1.598-.516 4.015-1.526 6.84-3.695 5.875-4.51 7.805-6.174 13.696-12.131 3.277-3.314 5.375-5.642 5.375-5.642s.483-.432.665-.798c.184-.367.367-1.049.883-1.448s1.564-.849 1.564-.849" />
<path
d="M17.89017 18.03288h1.023s3.096 2.696 6.915 3.994 6.989 1.997 13.28 2.296c6.29.3 10.958.375 12.431.575 1.473.199 2.197.499 2.197.499s-13.056.424-17.224.599c-4.169.174-11.857.823-11.857.823l-.625-.299 5.592-1.598-6.964-.075z" />
</svg>

Before

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@@ -1,202 +0,0 @@
Apache License
Version 2.0, January 2004
http://www.apache.org/licenses/
TERMS AND CONDITIONS FOR USE, REPRODUCTION, AND DISTRIBUTION
1. Definitions.
"License" shall mean the terms and conditions for use, reproduction,
and distribution as defined by Sections 1 through 9 of this document.
"Licensor" shall mean the copyright owner or entity authorized by
the copyright owner that is granting the License.
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@@ -1,44 +1,41 @@
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author | | Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :----------- | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- | | :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :------------ | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
| kessler | stuff | @emotion/react | perpetual | material | MIT | git+https://github.com/emotion-js/emotion.git#main | 11.14.0 | 11.14.0 | ^11.11.1 | Emotion Contributors | | kessler | stuff | 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 | @emotion/styled | perpetual | material | MIT | git+https://github.com/emotion-js/emotion.git#main | 11.14.0 | 11.14.0 | ^11.11.0 | n/a | | kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.4 | 19.2.4 | ^19.1.0 | n/a |
| kessler | stuff | @mui/icons-material | perpetual | material | MIT | git+https://github.com/mui/material-ui.git | 5.17.1 | 5.17.1 | ^5.14.16 | MUI Team | | kessler | stuff | 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 | @mui/material | perpetual | material | MIT | git+https://github.com/mui/material-ui.git | 5.17.1 | 5.17.1 | ^5.14.17 | MUI Team | | kessler | stuff | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 11.1.0 | 11.1.0 | ^11.1.0 | n/a |
| kessler | stuff | postcss-import | perpetual | material | MIT | git+https://github.com/postcss/postcss-import.git | 15.1.0 | 15.1.0 | ^15.1.0 | Maxime Thirouin | | kessler | stuff | @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 | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 18.3.1 | 18.3.1 | ^18.2.0 | n/a | | 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 | react-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 18.3.1 | 18.3.1 | ^18.2.0 | n/a | | kessler | stuff | @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 | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 9.0.1 | 9.0.1 | ^9.0.1 | n/a | | 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 | @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-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-commonjs | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 25.0.8 | 25.0.8 | ^25.0.0 | Rich Harris <richard.a.harris@gmail.com> | | kessler | stuff | @rollup/plugin-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-json | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.1.0 | 6.1.0 | ^6.0.0 | rollup | | kessler | stuff | @rollup/plugin-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 12.3.0 | 12.3.0 | ^12.1.2 | Oskar Segersvärd |
| kessler | stuff | @rollup/plugin-node-resolve | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 15.3.1 | 15.3.1 | ^15.1.0 | Rich Harris <richard.a.harris@gmail.com> | | kessler | stuff | @types/node | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 24.12.2 | 24.12.0 | ^24.3.1 | n/a |
| kessler | stuff | @rollup/plugin-replace | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.0.2 | 6.0.2 | ^6.0.2 | Rich Harris <richard.a.harris@gmail.com> | | kessler | stuff | @types/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.14 | 19.2.14 | ^19.1.6 | n/a |
| kessler | stuff | @rollup/plugin-terser | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 0.4.4 | 0.4.4 | ^0.4.3 | Peter Placzek <peter.placzek1996@gmail.com> | | kessler | stuff | @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 | @rollup/plugin-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 11.1.6 | 11.1.6 | ^11.1.1 | Oskar Segersvärd | | kessler | stuff | @types/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 | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 18.3.23 | 18.3.23 | ^18.2.8 | 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/react-dom | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 18.3.7 | 18.3.7 | ^18.2.4 | 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 | @types/uuid | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 9.0.8 | 9.0.8 | ^9.0.7 | n/a | | kessler | stuff | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.27 | 10.4.27 | ^10.4.21 | Andrey Sitnik <andrey@sitnik.ru> |
| kessler | stuff | @typescript-eslint/eslint-plugin | perpetual | material | MIT | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.10.0 | n/a | | kessler | stuff | 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 | @typescript-eslint/parser | perpetual | material | BSD-2-Clause | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.10.0 | n/a | | kessler | stuff | 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 | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.21 | 10.4.21 | ^10.4.14 | Andrey Sitnik <andrey@sitnik.ru> | | kessler | stuff | 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 | 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-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 | perpetual | material | MIT | git+https://github.com/eslint/eslint.git | 8.57.1 | 8.57.1 | ^8.42.0 | Nicholas C. Zakas <nicholas+npm@nczconsulting.com> | | kessler | stuff | eslint-plugin-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-import | perpetual | material | MIT | git+https://github.com/import-js/eslint-plugin-import.git | 2.31.0 | 2.31.0 | ^2.27.5 | Ben Mosher <me@benmosher.com> | | kessler | stuff | 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 | eslint-plugin-react | perpetual | material | MIT | git+https://github.com/jsx-eslint/eslint-plugin-react.git | 7.37.5 | 7.37.5 | ^7.32.2 | Yannick Croissant <yannick.croissant+npm@gmail.com> | | kessler | stuff | 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 | eslint-plugin-react-hooks | perpetual | material | MIT | git+https://github.com/facebook/react.git | 4.6.2 | 4.6.2 | ^4.6.0 | n/a | | kessler | stuff | 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 | license-report | perpetual | material | MIT | git+https://github.com/kessler/license-report.git | 6.7.2 | 6.7.2 | ^6.5.0 | Yaniv Kessler | | kessler | stuff | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.8.1 | 3.8.1 | ^3.5.3 | James Long |
| kessler | stuff | postcss | perpetual | material | MIT | git+https://github.com/postcss/postcss.git | 8.5.4 | 8.5.4 | ^8.4.24 | Andrey Sitnik <andrey@sitnik.ru> | | kessler | stuff | prettier-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 | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.5.3 | 3.5.3 | ^3.0.3 | James Long | | 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 | prettier-plugin-organize-imports | perpetual | material | MIT | git+https://github.com/simonhaenisch/prettier-plugin-organize-imports.git | 3.2.4 | 3.2.4 | ^3.2.4 | Simon Haenisch (https://github.com/simonhaenisch) | | kessler | stuff | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.60.1 | 4.60.0 | ^4.42.0 | Rich Harris |
| kessler | stuff | rimraf | perpetual | material | ISC | git://github.com/isaacs/rimraf.git | 5.0.10 | 5.0.10 | ^5.0.1 | Isaac Z. Schlueter <i@izs.me> (http://blog.izs.me/) | | kessler | stuff | rollup-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 | 4.41.1 | 4.41.1 | ^4.3.1 | 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 | ^3.4.0 | 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 | 1.99.0 | 1.98.0 | ^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 | 1.89.1 | 1.89.1 | ^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 | svg-slim | perpetual | material | MIT | git+https://github.com/benboba/svg-slim.git | 2.0.5 | 2.0.5 | ^2.0.5 | Wang Feng <benboba@gmail.com> | | kessler | stuff | 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 | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.5.3 | Microsoft Corp. |
| kessler | stuff | typed-scss-modules | perpetual | material | MIT | git+https://github.com/skovy/typed-scss-modules.git | 7.1.4 | 7.1.4 | ^7.1.0 | Spencer Miskoviak <smiskoviak@gmail.com> |
| kessler | stuff | typescript | perpetual | material | Apache-2.0 | git+https://github.com/Microsoft/TypeScript.git | 5.2.2 | 5.2.2 | 5.2.2 | Microsoft Corp. |
@@ -1,14 +1,15 @@
import { FC } from 'react'; import { FC } from 'react';
import { SharedConfig } from '../../configs/shared';
interface CGSelectProps { interface CGSelectProps {
minCG: number;
maxCG: number;
value: number; value: number;
disabled: boolean; disabled: boolean;
increase: () => void; increase: () => void;
decrease: () => void; decrease: () => void;
} }
const CGSelect: FC<CGSelectProps> = ({ value, disabled, increase, decrease }) => { const CGSelect: FC<CGSelectProps> = ({ minCG, maxCG, value, disabled, increase, decrease }) => {
return ( return (
<div className="relative"> <div className="relative">
<input <input
@@ -17,7 +18,7 @@ const CGSelect: FC<CGSelectProps> = ({ value, disabled, increase, decrease }) =>
value={value.toFixed(1)} value={value.toFixed(1)}
/> />
<button <button
disabled={disabled || value <= SharedConfig.CGLimits.min} disabled={disabled || value <= minCG}
className="absolute right-2 top-0 -mt-[.5px] border-t bg-zinc-700 text-white disabled:text-zinc-400" className="absolute right-2 top-0 -mt-[.5px] border-t bg-zinc-700 text-white disabled:text-zinc-400"
onClick={increase} onClick={increase}
> >
@@ -45,7 +46,7 @@ const CGSelect: FC<CGSelectProps> = ({ value, disabled, increase, decrease }) =>
</svg> </svg>
</button> </button>
<button <button
disabled={disabled || value >= SharedConfig.CGLimits.max} disabled={disabled || value >= maxCG}
className="absolute bottom-0 right-2 -mt-[.5px] border-b bg-zinc-700 text-white disabled:text-zinc-400" className="absolute bottom-0 right-2 -mt-[.5px] border-b bg-zinc-700 text-white disabled:text-zinc-400"
onClick={decrease} onClick={decrease}
> >
@@ -0,0 +1,216 @@
import { FC, useEffect, useState } from 'react';
import { WASMDataF } from '../../types/WASMData';
import { LoadingState, SimBrief } from '../../types/general';
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
import { CoherentCallSBEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
interface SBEntryProps {
WASMData: WASMDataF;
loadingState: LoadingState;
gsxActive: boolean;
gsxFuelActive: boolean;
setLoadingState: (newState: LoadingState) => void;
}
const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [SBInFlight, setSBInFlight] = useState(false);
// FROM EFB
const simBrief = useSelector((state) => state.simbrief.plan);
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
return Math.round(WASMData.livePayload.total);
};
const ZFWValid = () => {
return ZFW() <= WASMData.limits.maxZFW;
};
const GW = () => {
return fuel + ZFW();
};
const GWValid = () => {
return GW() <= WASMData.limits.maxTOW;
};
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
if (!input) {
setter(0);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < 0) setter(0);
else if (converted > maxValue) setter(maxValue);
else setter(converted);
}
};
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
CoherentCallSBEntryF(CGTarget, _fuel ?? fuel, SBPlan);
};
useEffect(() => updateData(), [CGTarget, fuel]);
useEffect(() => {
if (!simBrief || gsxActive) return;
setSBInFlight(true);
const SBResponse = ImportFlightPlanKH(
simBrief,
WASMData.limits.maxZFW,
WASMData.limits.maxTOW,
WASMData.limits.maxFuel,
WASMData.userData.isImperial
);
if (SBResponse.type === 'error') {
console.error('TODO: ERROR', SBResponse.message);
setSBInFlight(false);
return;
}
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
updateData(SBResponse.message as SimBrief, _fuel);
setFuel(_fuel);
setSBInFlight(false);
}, [simBrief, gsxActive]);
useEffect(
() =>
setFuel((prev) => {
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
return prev;
}),
[WASMData.userData.isER]
);
return (
<>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
value={fuel}
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxFuelActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Planned ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={WASMData.sbPlanned.ZFW}
disabled
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Planned GW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={WASMData.sbPlanned.GW}
disabled
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
</label>
<CGSelect
minCG={WASMData.limits.minCG}
maxCG={WASMData.limits.maxCG}
value={CGTarget}
disabled={loadingState !== 'preview' || gsxActive}
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
return _new;
})
}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={ZFW()}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={GW()}
/>
</div>
</div>
</div>
<ActionBar
loadingState={loadingState}
loadDisabled={!GWValid() || SBInFlight}
GSXSync={WASMData.options.GSXSync}
load={() => {
setLoadingState('loaded');
loadAircraft();
}}
unload={() => {
setLoadingState('preview');
unloadAircraft();
}}
/>
</>
);
};
export default SBEntryF;
@@ -1,111 +1,41 @@
import { FC, useEffect, useState } from 'react'; import { FC, useEffect, useState } from 'react';
import { PaxConfig, PayloadPax } from '../../configs/pax'; import { WASMDataPax } from '../../types/WASMData';
import { Fuel, SharedConfig } from '../../configs/shared'; import { LoadingState, SimBrief } from '../../types/general';
import { ImportFlightPlan } from '../../utils/TFDISBImport'; import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
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';
interface StationEntryProps { interface SBEntryProps {
unit: 'kg' | 'lbs'; WASMData: WASMDataPax;
isER: boolean; loadingState: LoadingState;
initialPayload: PayloadPax; gsxActive: boolean;
fuelLive: Fuel; gsxFuelActive: boolean;
payloadLive: PayloadPax; setLoadingState: (newState: LoadingState) => void;
loadingState: 'preview' | 'accepted' | 'loaded';
username: string;
setLoadingState: (newState: StationEntryProps['loadingState']) => void;
updateView: (payload: PayloadPax) => void;
loadAircraft: () => void;
} }
const SBEntryPax: FC<StationEntryProps> = ({ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
unit, const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
isER, const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
initialPayload,
fuelLive,
payloadLive,
loadingState,
username,
setLoadingState,
updateView,
loadAircraft,
}) => {
const [targetZFWCG, setTargetZFWCG] = useState(SharedConfig.CGLimits.default);
const [fuel, setFuel] = useState(
Math.round(
fuelLive.main1 +
fuelLive.main1Tip +
fuelLive.main2 +
fuelLive.main3 +
fuelLive.main3Tip +
fuelLive.upperAux +
fuelLive.lowerAux +
fuelLive.tail +
fuelLive.forwardAux1 +
fuelLive.forwardAux2
)
);
const [ZFW, setZFW] = useState(
Math.round(
PaxConfig.weights.base[unit].total +
(isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) +
payloadLive.empty +
initialPayload.business1Left +
initialPayload.business1Center +
initialPayload.business1Right +
initialPayload.business2Left +
initialPayload.business2Center +
initialPayload.business2Right +
initialPayload.economy1Left +
initialPayload.economy1Center +
initialPayload.economy1Right +
initialPayload.economy2Left +
initialPayload.economy2Center +
initialPayload.economy2Right +
initialPayload.forwardCargo +
initialPayload.rearCargo
)
);
const [SBPlan, setSBPlan] = useState<any>();
const [SBInFlight, setSBInFlight] = useState(false); const [SBInFlight, setSBInFlight] = useState(false);
const _ZFW = () => { // FROM EFB
if (loadingState !== 'loaded') return ZFW; const simBrief = useSelector((state) => state.simbrief.plan);
return Math.round( const ZFW = () => {
payloadLive.empty + if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
payloadLive.pilot +
payloadLive.firstOfficer + return Math.round(WASMData.livePayload.total);
payloadLive.engineer +
payloadLive.cabinCrewFront +
payloadLive.business1Left +
payloadLive.business1Center +
payloadLive.business1Right +
payloadLive.business2Left +
payloadLive.business2Center +
payloadLive.business2Right +
payloadLive.economy1Left +
payloadLive.economy1Center +
payloadLive.economy1Right +
payloadLive.economy2Left +
payloadLive.economy2Center +
payloadLive.economy2Right +
payloadLive.cabinCrewRear +
payloadLive.forwardCargo +
payloadLive.rearCargo +
payloadLive.leftAuxPax +
payloadLive.rightAuxPax
);
}; };
const ZFWValid = () => { const ZFWValid = () => {
return _ZFW() <= PaxConfig.maxZWF[unit]; return ZFW() <= WASMData.limits.maxZFW;
}; };
const GW = () => { const GW = () => {
return fuel + _ZFW(); return fuel + ZFW();
}; };
const GWValid = () => { const GWValid = () => {
return GW() <= (isER ? SharedConfig.maxTOW.er[unit] : SharedConfig.maxTOW.norm[unit]); return GW() <= WASMData.limits.maxTOW;
}; };
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => { const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
@@ -122,160 +52,155 @@ const SBEntryPax: FC<StationEntryProps> = ({
} }
}; };
const handleSB = async () => { const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
CoherentCallSBEntryPax(CGTarget, _fuel ?? fuel, SBPlan);
};
useEffect(() => {
if (!simBrief || gsxActive) return;
setSBInFlight(true); setSBInFlight(true);
const SBResponse = await ImportFlightPlan(username, PaxConfig, unit, isER); const SBResponse = ImportFlightPlanKH(
simBrief,
WASMData.limits.maxZFW,
WASMData.limits.maxTOW,
WASMData.limits.maxFuel,
WASMData.userData.isImperial
);
if (SBResponse.type === 'error') { if (SBResponse.type === 'error') {
console.error('TODO: ERROR', SBResponse.message); console.error('TODO: ERROR', SBResponse.message);
setSBInFlight(false); setSBInFlight(false);
return; return;
} }
const __ZFW = Math.round( const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
PaxConfig.weights.base[unit].total +
(isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) +
payloadLive.empty +
SBResponse.message.pax * (PaxConfig.weights.pax[unit] + PaxConfig.weights.baggage[unit]) +
SBResponse.message.cargo
);
const _fuel = SBResponse.message.fuel;
updateView( updateData(SBResponse.message as SimBrief, _fuel);
PaxConfig.distribute(__ZFW, targetZFWCG, payloadLive.empty, fuelLive, unit, isER, SBResponse.message.pax)
);
setSBPlan(SBResponse.message);
setZFW(__ZFW);
setFuel(_fuel); setFuel(_fuel);
setSBInFlight(false);
};
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
setSBInFlight(false);
}, [simBrief, gsxActive]);
useEffect(() => updateData(), [CGTarget, fuel]);
useEffect( useEffect(
() => () =>
setFuel((prev) => setFuel((prev) => {
prev > (isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit]) if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
? isER return prev;
? SharedConfig.maxFuel.er[unit] }),
: SharedConfig.maxFuel.norm[unit] [WASMData.userData.isER]
: prev
),
[isER]
); );
return ( return (
<> <>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4"> <div className="flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<label>Planned ZFW ({unit})</label> <div className="flex w-full items-center justify-between text-xs">
<input <label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
type="text" <Input
placeholder="" type="text"
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" placeholder=""
value={SBPlan?.plannedZFW ?? 0} className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
disabled value={fuel}
/> onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
</div> disabled={loadingState !== 'preview' || gsxFuelActive}
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4"> />
<label>Planned ZFW ({unit})</label> </div>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={SBPlan?.plannedGW ?? 0}
disabled
/>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-600 p-2 px-4">
<label>
Target ZFWCG ({SharedConfig.CGLimits.min} - {SharedConfig.CGLimits.max})
</label>
<CGSelect
value={targetZFWCG}
disabled={loadingState !== 'preview'}
increase={() =>
setTargetZFWCG((prev) => {
const _new = prev + 0.1;
updateView(PaxConfig.distribute(ZFW, _new, payloadLive.empty, fuelLive, unit, isER));
return _new;
})
}
decrease={() =>
setTargetZFWCG((prev) => {
const _new = prev - 0.1;
updateView(PaxConfig.distribute(ZFW, _new, payloadLive.empty, fuelLive, unit, isER));
return _new;
})
}
/>
</div> </div>
</div> </div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4"> <div className="flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label>Fuel ({unit})</label> <div className="flex w-full items-center justify-between text-xs">
<input <label>Planned ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
type="text" <input
placeholder="" type="text"
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`} placeholder=""
value={fuel} 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"
onChange={(e) => value={WASMData.sbPlanned.ZFW}
handleInput( disabled
e.target.value, />
isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit], </div>
setFuel </div>
) <div className="flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
} <div className="flex w-full items-center justify-between text-xs">
disabled <label>Planned GW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
/> <input
<button type="text"
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" placeholder=""
data-ripple-light="true" 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"
onClick={() => { value={WASMData.sbPlanned.GW}
SimVar.SetSimVarValue('L:MD11_EFB_PAYLOAD_FUEL', 'lbs', unit === 'kg' ? fuel * 2.20462262185 : fuel); disabled
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true); />
}} </div>
disabled={loadingState !== 'preview' || SBInFlight} </div>
> <div className="flex w-full items-center justify-between rounded-b-md bg-zinc-600 p-2 px-4">
Load Fuel <div className="flex w-full items-center justify-between text-xs">
</button> <label>
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
</label>
<CGSelect
minCG={WASMData.limits.minCG}
maxCG={WASMData.limits.maxCG}
value={CGTarget}
disabled={loadingState !== 'preview' || gsxActive}
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
return _new;
})
}
/>
</div>
</div> </div>
</div> </div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4"> <div className="flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} ZFW ({unit}) <label>
</label> {loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
<input {WASMData.userData.isImperial ? 'lbs' : 'kg'})
type="text" </label>
placeholder="" <input
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} type="text"
disabled placeholder=""
value={_ZFW()} className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
/> disabled
value={ZFW()}
/>
</div>
</div> </div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4"> <div className="flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} GW ({unit}) <label>
</label> {loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
<input {WASMData.userData.isImperial ? 'lbs' : 'kg'})
type="text" </label>
placeholder="" <input
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} type="text"
disabled placeholder=""
value={GW()} className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
/> disabled
value={GW()}
/>
</div>
</div> </div>
</div> </div>
<ActionBar <ActionBar
loadingState={loadingState} loadingState={loadingState}
acceptDisabled={!GWValid() || SBInFlight} loadDisabled={!GWValid() || SBInFlight}
//TODO: Make GSX optional (accepted state for NON GSX) GSXSync={WASMData.options.GSXSync}
accept={() => setLoadingState('loaded')}
reject={() => setLoadingState('preview')}
importSB={handleSB}
load={() => { load={() => {
setLoadingState('loaded'); setLoadingState('loaded');
@@ -284,7 +209,7 @@ const SBEntryPax: FC<StationEntryProps> = ({
unload={() => { unload={() => {
setLoadingState('preview'); setLoadingState('preview');
PaxConfig.unload(unit, isER); unloadAircraft();
}} }}
/> />
</> </>
@@ -1,62 +1,28 @@
import { FC } from 'react'; import { FC } from 'react';
import { LoadingState } from '../../types/general';
interface ActionBarProps { interface ActionBarProps {
loadingState: 'preview' | 'accepted' | 'loaded'; loadingState: LoadingState;
acceptDisabled: boolean; loadDisabled: boolean;
accept: () => void; GSXSync: boolean;
reject: () => void;
importSB?: () => void;
load: () => void; load: () => void;
unload: () => void; unload: () => void;
} }
const ActionBar: FC<ActionBarProps> = ({ loadingState, acceptDisabled, accept, reject, importSB, load, unload }) => { const ActionBar: FC<ActionBarProps> = ({ loadingState, loadDisabled, GSXSync, load, unload }) => {
return ( return (
<div className="relative flex w-full items-center justify-start gap-x-6"> <div className="relative flex w-full items-center justify-start gap-x-6">
{loadingState === 'preview' && ( {loadingState === 'preview' && !GSXSync && (
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={accept}
disabled={acceptDisabled}
>
Accept
</button>
)}
{/*TODO: Make GSX optional (accepted state for NON GSX) */}
{loadingState === 'loaded' && (
<button
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={reject}
>
Reject
</button>
)}
<div className="grow" />
{!!importSB && loadingState === 'preview' && (
<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={importSB}
>
Import from SimBrief
</button>
)}
{/*TODO: Make GSX optional */}
{/*
{loadingState === 'accepted' && (
<button <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" 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" data-ripple-light="true"
onClick={load} onClick={load}
disabled={loadDisabled}
> >
Load Load
</button> </button>
)} )}
{loadingState === 'loaded' && ( {loadingState === 'loaded' && !GSXSync && (
<button <button
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none" className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true" data-ripple-light="true"
@@ -65,7 +31,6 @@ const ActionBar: FC<ActionBarProps> = ({ loadingState, acceptDisabled, accept, r
Unload Unload
</button> </button>
)} )}
*/}
</div> </div>
); );
}; };
@@ -1,92 +0,0 @@
import { FC, useState } from 'react';
import { PayloadFreight } from '../../configs/freighter';
import { initialPayload, SharedConfig } from '../../configs/shared';
import Profile from '../profile/Profile';
import Tabbar from '../tabbar/Tabbar';
interface FreightProps {
isER: boolean;
unit: 'kg' | 'lbs';
OEW: number;
CGs: [number, number];
}
const Freight: FC<FreightProps> = ({ isER, unit, OEW, CGs }) => {
const [selectedTab, setSelectedTab] = useState(0);
const [payload, setPayload] = useState<PayloadFreight>(initialPayload);
const [inPreview, setInPreview] = useState(true);
const upper1 = () => {
return Math.round(payload.upper1Left + payload.upper1Right);
};
const upper2 = () => {
return Math.round(payload.upper2Left + payload.upper2Right);
};
const upper3 = () => {
return Math.round(payload.upper3Left + payload.upper3Right);
};
const upper4 = () => {
return Math.round(payload.upper4Left + payload.upper4Right);
};
const lower1 = () => {
return Math.round(payload.lowerForward);
};
const lower2 = () => {
return Math.round(payload.lowerRear);
};
const _OEW = () => {
return Math.round(OEW + (isER ? SharedConfig.erExtraWeight[unit] * 2 : 1));
};
const crew = () => {
return Math.round(payload.pilot + payload.firstOfficer + payload.engineer);
};
const cgs = (): [string, string] => {
return [CGs[0].toFixed(1), CGs[1].toFixed(1)];
};
return (
<>
<Profile
type="F"
isER={isER}
upper1={`${upper1()}`}
upper2={`${upper2()}`}
upper3={`${upper3()}`}
upper4={`${upper4()}`}
lower1={`${lower1()}`}
lower2={`${lower2()}`}
OEW={`${_OEW()}`}
crew={`${crew()}`}
unit={unit.toUpperCase()}
inPreview={inPreview}
CGs={cgs()}
/>
<Tabbar tabs={['Simbrief', 'ZFW', 'Cargo']} selectedTab={selectedTab} setSelectedTab={setSelectedTab} />
<div className="relative flex w-full items-center justify-start gap-x-6">
<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={() => {
console.log('TODO: SET PAYLOAD IN SIM');
setInPreview(false);
}}
>
Load
</button>
<button
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
console.log('TODO: CLEAR PAYLOAD IN SIM');
setInPreview(true);
}}
>
Unload
</button>
</div>
</>
);
};
export default Freight;
@@ -0,0 +1,162 @@
import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { GSXFuelingState, GSXLoadingState, WASMDataF } from '../../types/WASMData';
import OptionsF from '../options/OptionsF';
import Profile from '../profile/Profile';
import SBEntryF from '../SBEntry/SBEntryF';
import StationEntryF from '../stationEntry/StationEntryF';
import Tabbar from '../tabbar/Tabbar';
import ZFWEntryF from '../zfwEntry/ZFWEntryF';
interface FreighterProps {
WASMData: WASMDataF;
username?: string;
}
const Freighter: FC<FreighterProps> = ({ WASMData, username }) => {
const [selectedTab, setSelectedTab] = useState(0);
const [loadingState, setLoadingState] = useState<LoadingState>('preview');
const upper1 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper1);
return Math.round(WASMData.livePayload.upper1);
};
const upper2 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper2);
return Math.round(WASMData.livePayload.upper2);
};
const upper3 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper3);
return Math.round(WASMData.livePayload.upper3);
};
const upper4 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') return Math.round(WASMData.targetPayload.upper4);
return Math.round(WASMData.livePayload.upper4);
};
const lower1 = () => {
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.lowerForward);
return Math.round(WASMData.livePayload.lowerForward);
};
const lower2 = () => {
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.lowerRear);
return Math.round(WASMData.livePayload.lowerRear);
};
const OEW = () => {
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.empty);
return Math.round(WASMData.livePayload.empty);
};
const crew = () => {
if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.crew);
return Math.round(WASMData.livePayload.crew);
};
const GSXActive = () => {
return (
WASMData.GSX.couatlStarted &&
WASMData.GSX.loadingState !== GSXLoadingState.IDLE &&
WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
);
};
const GSXFuelActive = () => {
return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
};
const CGs = (): [string, boolean, string, boolean] => {
if (loadingState !== 'loaded' && !GSXActive()) {
return [
WASMData.targetPayload.ZFWCG.toFixed(1),
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
WASMData.targetPayload.TOCG.toFixed(1),
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
];
}
if (WASMData.options.GSXSync && GSXActive() && WASMData.GSX.loadingState === GSXLoadingState.BOARDING) {
return [
WASMData.targetPayload.ZFWCG.toFixed(1),
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
WASMData.targetPayload.TOCG.toFixed(1),
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
];
}
return [
WASMData.livePayload.ZFWCG.toFixed(1),
WASMData.livePayload.ZFWCG < WASMData.limits.minCG || WASMData.livePayload.ZFWCG > WASMData.limits.maxCG,
WASMData.livePayload.TOCG.toFixed(1),
WASMData.livePayload.TOCG < WASMData.limits.minCG || WASMData.livePayload.TOCG > WASMData.limits.maxCG,
];
};
useEffect(() => {
setLoadingState(WASMData.loaded ? 'loaded' : 'preview');
}, [WASMData.loaded]);
return (
<>
<Profile
type="F"
isER={WASMData.userData.isER}
upper1={`${upper1(GSXActive() ? 'loaded' : loadingState)}`}
upper2={`${upper2(GSXActive() ? 'loaded' : loadingState)}`}
upper3={`${upper3(GSXActive() ? 'loaded' : loadingState)}`}
upper4={`${upper4(GSXActive() ? 'loaded' : loadingState)}`}
lower1={`${lower1()}`}
lower2={`${lower2()}`}
OEW={`${OEW()}`}
crew={`${crew()}`}
unit={WASMData.userData.isImperial ? 'LBS' : 'KG'}
inPreview={loadingState !== 'loaded' && !GSXActive()}
CGs={CGs()}
done={
WASMData.options.GSXSync ? WASMData.GSX.loadingState === GSXLoadingState.BOARDED : loadingState !== 'preview'
}
/>
<Tabbar
tabs={username ? ['Simbrief', 'ZFW', 'Cargo', 'Options'] : ['ZFW', 'Cargo', 'Options']}
selectedTab={selectedTab}
setSelectedTab={setSelectedTab}
/>
{username && selectedTab === 0 && (
<SBEntryF
WASMData={WASMData}
loadingState={loadingState}
setLoadingState={setLoadingState}
gsxActive={GSXActive()}
gsxFuelActive={GSXFuelActive()}
/>
)}
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
<ZFWEntryF
WASMData={WASMData}
loadingState={loadingState}
setLoadingState={setLoadingState}
gsxActive={GSXActive()}
gsxFuelActive={GSXFuelActive()}
/>
)}
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
<StationEntryF
WASMData={WASMData}
loadingState={loadingState}
setLoadingState={setLoadingState}
gsxActive={GSXActive()}
gsxFuelActive={GSXFuelActive()}
/>
)}
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
<OptionsF WASMData={WASMData} loadingState={loadingState} gsxActive={GSXActive()} />
)}
</>
);
};
export default Freighter;
@@ -0,0 +1,102 @@
import { useEffect, useRef, useState } from 'react';
import { v4 } from 'uuid';
import Keyboard from '../keyboard/Keyboard';
export default function Input(props: {
type?: string;
topKeyboard?: boolean;
value: number | string;
min?: number;
max?: number;
step?: number;
placeholder?: string;
className?: string;
disabled?: boolean;
onChange?: (value: string) => void;
onBlur?: (value: string) => void;
}) {
const [guid] = useState(v4());
const ref = useRef<HTMLInputElement>(null);
const keyboardRef = useRef<HTMLDivElement>(null);
const blurRef = useRef<boolean>(false);
const [isFocused, setFocused] = useState(false);
const [showKeyboard, setShowKeyboard] = useState(false);
const [unfocusTimer, setUnfocusTimer] = useState<NodeJS.Timeout | null>(null);
useEffect(() => {
if (unfocusTimer) {
clearTimeout(unfocusTimer);
setUnfocusTimer(null);
}
if (isFocused) {
setUnfocusTimer(setTimeout(() => ref.current?.blur(), 5e3));
Coherent.trigger('FOCUS_INPUT_FIELD', guid, '', '', '', false);
} else {
console.log('UNFOCUS_INPUT_FIELD');
Coherent.trigger('UNFOCUS_INPUT_FIELD', guid);
}
return () => {
if (unfocusTimer) {
clearTimeout(unfocusTimer);
setUnfocusTimer(null);
}
};
}, [isFocused, guid]);
return (
<>
<input
ref={ref}
type={props.type ? props.type : 'text'}
min={props.min}
max={props.max}
step={props.step}
placeholder={props.placeholder}
disabled={props.disabled}
onFocus={() => {
if (!isFocused) {
setFocused(true);
setShowKeyboard(true);
ref.current?.select();
}
}}
onBlur={(e) => {
if (blurRef.current && isFocused) ref.current?.focus();
else {
props.onBlur?.(e.target.value);
setShowKeyboard(false);
setFocused(false);
ref.current?.blur();
}
blurRef.current = false;
}}
onChange={(e) => {
if (props.onChange) props.onChange(e.target.value);
if (unfocusTimer) {
clearTimeout(unfocusTimer);
setUnfocusTimer(null);
}
if (isFocused) setUnfocusTimer(setTimeout(() => ref.current?.blur(), 5e3));
}}
value={props.value}
className={props.className}
/>
{showKeyboard && (
<Keyboard
ref={keyboardRef}
top={props.topKeyboard}
value={String(props.value)}
blurRef={blurRef}
onInput={(value) => props.onChange && props.onChange(value)}
onClose={() => {
setShowKeyboard(false);
setFocused(false);
ref.current?.blur();
}}
/>
)}
</>
);
}
@@ -0,0 +1,108 @@
import { ArrowBigUp, Delete, Space, X } from 'lucide-react';
import { forwardRef, RefObject, useState } from 'react';
import { createPortal } from 'react-dom';
const defaultLayout = {
default: [
'1 2 3 4 5 6 7 8 9 0 {bksp}',
'q w e r t y u i o p',
'a s d f g h j k l',
'{shift} z x c v b n m /',
'{space} {close}',
],
shift: [
'1 2 3 4 5 6 7 8 9 0 {bksp}',
'Q W E R T Y U I O P',
'A S D F G H J K L',
'{shift} Z X C V B N M /',
'{space} {close}',
],
};
const Keyboard = forwardRef<
HTMLDivElement,
{
value: string;
blurRef: RefObject<boolean>;
top?: boolean;
onInput: (value: string) => void;
onClose: () => void;
}
>(({ value, top, blurRef, onInput, onClose }, ref) => {
const [shift, setShift] = useState(false);
const layout = shift ? defaultLayout.shift : defaultLayout.default;
const handleKeyPress = (key: string) => {
console.log('KEY PRESSED', key);
if (key === '{close}') {
onClose();
return;
}
blurRef.current = true;
if (key === '{shift}') {
setShift(!shift);
return;
}
let newValue = value;
if (key === '{bksp}') {
newValue = value.slice(0, -1);
} else if (key === '{space}') {
newValue = value + ' ';
} else if (key.length === 1) {
newValue = value + key;
}
onInput(newValue);
};
return createPortal(
<div
ref={ref}
className={`absolute ${top ? 'top-0' : 'bottom-0'} left-0 z-50 box-border w-full touch-manipulation select-none overflow-hidden bg-zinc-800 p-2 text-white`}
>
{layout.map((row, rowIndex) => (
<div key={`row-${rowIndex}`} className="mb-1 flex w-full justify-center gap-1">
{row.split(' ').map((key, keyIndex) => {
let keyIdent = <>{key}</>;
switch (key) {
case '{shift}':
keyIdent = <ArrowBigUp />;
break;
case '{bksp}':
keyIdent = <Delete />;
break;
case '{close}':
keyIdent = <X />;
break;
case '{space}':
keyIdent = <Space />;
break;
}
return (
<button
key={`key-${rowIndex}-${keyIndex}`}
className={`flex justify-center rounded-md p-4 ${
key === '{close}' ? 'bg-zinc-700 px-12 focus:bg-zinc-600' : 'flex-1 bg-zinc-600'
}`}
onMouseDown={() => handleKeyPress(key)}
>
{keyIdent}
</button>
);
})}
</div>
))}
</div>,
document.body
);
});
Keyboard.displayName = "Keyboard"
export default Keyboard;
@@ -0,0 +1,121 @@
import { FC } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataF } from '../../types/WASMData';
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
interface OptionsFProps {
WASMData: WASMDataF;
loadingState: LoadingState;
gsxActive: boolean;
}
const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
return (
<>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<ToggleComponentKH
optionName="GSX Sync"
value={WASMData.options.GSXSync}
leftLabel={{ value: true }}
rightLabel={{ value: false }}
backgroundColor="bg-zinc-700"
setValue={(value) => {
CoherentCallOptionsSet(value);
}}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
{WASMData.userData.isER ? (
<>
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - ER Variant</h2>
<table className="text-xs">
<tbody>
<tr>
<td className="p-1 px-2">Max Passengers</td>
<td className="p-1 px-2">0</td>
</tr>
<tr>
<td className="p-1 px-2">Passenger Weight</td>
<td className="p-1 px-2">1 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Bag Weight</td>
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249537 lbs' : '113188 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Zero Fuel Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '451300 lbs' : '204706 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Takeoff Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '630500 lbs' : '285990 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Fuel Capacity</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '282619 lbs' : '128193 kg'}</td>
</tr>
</tbody>
</table>
</>
) : (
<>
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - Normal variant</h2>
<table className="text-xs">
<tbody>
<tr>
<td className="p-1 px-2">Max Passengers</td>
<td className="p-1 px-2">0</td>
</tr>
<tr>
<td className="p-1 px-2">Passenger Weight</td>
<td className="p-1 px-2">1 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Bag Weight</td>
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249137 lbs' : '113006 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Zero Fuel Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '451300 lbs' : '204706 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Takeoff Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '625500 lbs' : '283722 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Fuel Capacity</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '256207 lbs' : '116213 kg'}</td>
</tr>
</tbody>
</table>
</>
)}
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<button
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={CoherentCallGSXReset}
>
Reset internal GSX state
</button>
</div>
</>
);
};
export default OptionsF;
@@ -0,0 +1,182 @@
import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataPax } from '../../types/WASMData';
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
import Input from '../input/Input';
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
interface OptionsPaxProps {
WASMData: WASMDataPax;
loadingState: LoadingState;
gsxActive: boolean;
}
const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive }) => {
const [paxWeight, setPaxWeight] = useState(WASMData.options.paxWeight);
const [bagWeight, setBagWeight] = useState(WASMData.options.bagWeight);
const updateData = () => {
CoherentCallOptionsSet(undefined, paxWeight, bagWeight);
};
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
if (!input) {
setter(0);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < 0) setter(0);
else if (converted > maxValue) setter(maxValue);
else setter(converted);
}
};
useEffect(() => updateData(), [paxWeight, bagWeight]);
return (
<>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<ToggleComponentKH
optionName="GSX Sync"
value={WASMData.options.GSXSync}
leftLabel={{ value: true }}
rightLabel={{ value: false }}
backgroundColor="bg-zinc-700"
setValue={(value) => {
CoherentCallOptionsSet(value);
}}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Pax Weight ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={paxWeight}
onChange={(value) => handleInput(value, Number.MAX_VALUE, setPaxWeight)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Bag Weight ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={bagWeight}
onChange={(value) => handleInput(value, Number.MAX_VALUE, setBagWeight)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
{WASMData.userData.isER ? (
<>
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - ER Variant</h2>
<table className="text-xs">
<tbody>
<tr>
<td className="p-1 px-2">Max Passengers</td>
<td className="p-1 px-2">313</td>
</tr>
<tr>
<td className="p-1 px-2">Passenger Weight</td>
<td className="p-1 px-2">
{WASMData.options.paxWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
</td>
</tr>
<tr>
<td className="p-1 px-2">Bag Weight</td>
<td className="p-1 px-2">
{WASMData.options.bagWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286465 lbs' : '129937 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Zero Fuel Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '400000 lbs' : '181437 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Takeoff Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '630500 lbs' : '285990 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Fuel Capacity</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '282619 lbs' : '128193 kg'}</td>
</tr>
</tbody>
</table>
</>
) : (
<>
<h2 className="text-sm font-medium uppercase">SimBrief Profile Settings - Normal variant</h2>
<table className="text-xs">
<tbody>
<tr>
<td className="p-1 px-2">Max Passengers</td>
<td className="p-1 px-2">313</td>
</tr>
<tr>
<td className="p-1 px-2">Passenger Weight</td>
<td className="p-1 px-2">
{WASMData.options.paxWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
</td>
</tr>
<tr>
<td className="p-1 px-2">Bag Weight</td>
<td className="p-1 px-2">
{WASMData.options.bagWeight} {WASMData.userData.isImperial ? 'lbs' : 'kg'}
</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '286065 lbs' : '129755 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Zero Fuel Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '400000 lbs' : '181437 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Takeoff Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '625500 lbs' : '283722 kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Max Fuel Capacity</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '256207 lbs' : '116213 kg'}</td>
</tr>
</tbody>
</table>
</>
)}
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<button
className="middle none center rounded-lg bg-red-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-red-500/20 transition-all hover:shadow-lg hover:shadow-red-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={CoherentCallGSXReset}
>
Reset internal GSX state & disable SYNC
</button>
</div>
</>
);
};
export default OptionsPax;
@@ -1,167 +1,128 @@
import { FC, useEffect, useState } from 'react'; import { FC, useEffect, useState } from 'react';
import { PaxConfig, PayloadPax } from '../../configs/pax'; import { LoadingState } from '../../types/general';
import { Fuel, initialPayload, SharedConfig } from '../../configs/shared'; import { GSXFuelingState, GSXLoadingState, WASMDataPax } from '../../types/WASMData';
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';
import StationEntryPax from '../stationEntry/StationEntryPax'; import StationEntryPax from '../stationEntry/StationEntryPax';
import Tabbar from '../tabbar/Tabbar'; import Tabbar from '../tabbar/Tabbar';
import ZFWEntryPax from '../ZFWEntry/ZFWEntryPax'; import ZFWEntryPax from '../zfwEntry/ZFWEntryPax';
interface PaxProps { interface PaxProps {
isER: boolean; WASMData: WASMDataPax;
unit: 'kg' | 'lbs';
CGs: [number, number];
payloadLive: PayloadPax;
fuelLive: Fuel;
username?: string; username?: string;
GSXPaxNum: number;
GSXCargoPercent: number;
GSXState: 'boarding' | 'deboarding' | 'idle';
} }
const Pax: FC<PaxProps> = ({ const Pax: FC<PaxProps> = ({ WASMData, username }) => {
isER,
unit,
CGs,
fuelLive,
payloadLive,
username,
GSXPaxNum,
GSXCargoPercent,
GSXState,
}) => {
const [selectedTab, setSelectedTab] = useState(0); const [selectedTab, setSelectedTab] = useState(0);
const [payload, setPayload] = useState<PayloadPax>(initialPayload); const [loadingState, setLoadingState] = useState<LoadingState>('preview');
const [loadingState, setLoadingState] = useState<'preview' | 'accepted' | 'loaded'>('preview');
const upper1 = (overrideState: 'preview' | 'accepted' | 'loaded' = loadingState) => { const upper1 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') if (overrideState !== 'loaded') return WASMData.targetPayload.business1;
return PaxConfig.weightToPax(payload.business1Left + payload.business1Center + payload.business1Right, unit);
return PaxConfig.weightToPax( return WASMData.livePayload.business1;
payloadLive.business1Left + payloadLive.business1Center + payloadLive.business1Right,
unit
);
}; };
const upper2 = (overrideState: 'preview' | 'accepted' | 'loaded' = loadingState) => { const upper2 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') if (overrideState !== 'loaded') return WASMData.targetPayload.business2;
return PaxConfig.weightToPax(payload.business2Left + payload.business2Center + payload.business2Right, unit);
return PaxConfig.weightToPax( return WASMData.livePayload.business2;
payloadLive.business2Left + payloadLive.business2Center + payloadLive.business2Right,
unit
);
}; };
const upper3 = (overrideState: 'preview' | 'accepted' | 'loaded' = loadingState) => { const upper3 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') if (overrideState !== 'loaded') return WASMData.targetPayload.economy1;
return PaxConfig.weightToPax(payload.economy1Left + payload.economy1Center + payload.economy1Right, unit);
return PaxConfig.weightToPax( return WASMData.livePayload.economy1;
payloadLive.economy1Left + payloadLive.economy1Center + payloadLive.economy1Right,
unit
);
}; };
const upper4 = (overrideState: 'preview' | 'accepted' | 'loaded' = loadingState) => { const upper4 = (overrideState: LoadingState = loadingState) => {
if (overrideState !== 'loaded') if (overrideState !== 'loaded') return WASMData.targetPayload.economy2;
return PaxConfig.weightToPax(payload.economy2Left + payload.economy2Center + payload.economy2Right, unit);
return PaxConfig.weightToPax( return WASMData.livePayload.economy2;
payloadLive.economy2Left + payloadLive.economy2Center + payloadLive.economy2Right,
unit
);
}; };
const lower1 = () => { const lower1 = () => {
if (loadingState !== 'loaded') return Math.round(payload.forwardCargo); if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.forwardCargo);
return Math.round(payloadLive.forwardCargo); return Math.round(WASMData.livePayload.forwardCargo);
}; };
const lower2 = () => { const lower2 = () => {
if (loadingState !== 'loaded') return Math.round(payload.rearCargo); if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.rearCargo);
return Math.round(payloadLive.rearCargo); return Math.round(WASMData.livePayload.rearCargo);
}; };
const _OEW = () => { const OEW = () => {
if (loadingState !== 'loaded') if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.empty);
return Math.round(payloadLive.empty + (isER ? SharedConfig.erExtraWeight[unit] * 2 : 1));
return Math.round(payloadLive.empty + payloadLive.leftAuxPax + payloadLive.rightAuxPax); return Math.round(WASMData.livePayload.empty);
}; };
const crew = () => { const crew = () => {
if (loadingState !== 'loaded') return PaxConfig.weights.base[unit].total; if (loadingState !== 'loaded' && !GSXActive()) return Math.round(WASMData.targetPayload.crew);
return Math.round( return Math.round(WASMData.livePayload.crew);
payloadLive.cabinCrewFront +
payloadLive.cabinCrewRear +
payloadLive.pilot +
payloadLive.firstOfficer +
payloadLive.engineer
);
}; };
const _CGs = (): [string, boolean, string, boolean] => { const GSXActive = () => {
if (loadingState !== 'loaded') { return (
const __CGs = PaxConfig.calculateCGs( WASMData.GSX.couatlStarted &&
{ WASMData.GSX.loadingState !== GSXLoadingState.IDLE &&
...payload, WASMData.GSX.loadingState !== GSXLoadingState.DEBOARDED
empty: payloadLive.empty, );
cabinCrewFront: PaxConfig.weights.base[unit].cabinCrewFront, };
cabinCrewRear: PaxConfig.weights.base[unit].cabinCrewRear, const GSXFuelActive = () => {
pilot: PaxConfig.weights.base[unit].pilot, return WASMData.GSX.couatlStarted && WASMData.GSX.fuelingState !== GSXFuelingState.IDLE;
firstOfficer: PaxConfig.weights.base[unit].firstOfficer, };
engineer: PaxConfig.weights.base[unit].engineer,
leftAuxPax: isER ? SharedConfig.erExtraWeight[unit] : 0, const CGs = (): [string, boolean, string, boolean] => {
rightAuxPax: isER ? SharedConfig.erExtraWeight[unit] : 0, if (loadingState !== 'loaded' && !GSXActive()) {
},
fuelLive
);
return [ return [
__CGs[0].toFixed(1), WASMData.targetPayload.ZFWCG.toFixed(1),
__CGs[0] < SharedConfig.CGLimits.min || __CGs[0] > SharedConfig.CGLimits.max, WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
__CGs[1].toFixed(1), WASMData.targetPayload.TOCG.toFixed(1),
__CGs[1] < SharedConfig.CGLimits.min || __CGs[1] > SharedConfig.CGLimits.max, WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
];
}
if (WASMData.options.GSXSync && GSXActive() && WASMData.GSX.loadingState === GSXLoadingState.BOARDING) {
return [
WASMData.targetPayload.ZFWCG.toFixed(1),
WASMData.targetPayload.ZFWCG < WASMData.limits.minCG || WASMData.targetPayload.ZFWCG > WASMData.limits.maxCG,
WASMData.targetPayload.TOCG.toFixed(1),
WASMData.targetPayload.TOCG < WASMData.limits.minCG || WASMData.targetPayload.TOCG > WASMData.limits.maxCG,
]; ];
} }
return [ return [
CGs[0].toFixed(1), WASMData.livePayload.ZFWCG.toFixed(1),
CGs[0] < SharedConfig.CGLimits.min || CGs[0] > SharedConfig.CGLimits.max, WASMData.livePayload.ZFWCG < WASMData.limits.minCG || WASMData.livePayload.ZFWCG > WASMData.limits.maxCG,
CGs[1].toFixed(1), WASMData.livePayload.TOCG.toFixed(1),
CGs[1] < SharedConfig.CGLimits.min || CGs[1] > SharedConfig.CGLimits.max, WASMData.livePayload.TOCG < WASMData.limits.minCG || WASMData.livePayload.TOCG > WASMData.limits.maxCG,
]; ];
}; };
//TODO: Make GSX optional
useEffect(() => { useEffect(() => {
if (GSXState === 'idle') return; setLoadingState(WASMData.loaded ? 'loaded' : 'preview');
}, [WASMData.loaded]);
PaxConfig.setWeightsProgressive(
payload,
GSXState === 'boarding' ? GSXPaxNum : payload.paxCount.total - GSXPaxNum,
GSXCargoPercent,
unit
);
}, [GSXPaxNum, GSXCargoPercent, GSXState]);
return ( return (
<> <>
<Profile <Profile
type="PAX" type="PAX"
isER={isER} isER={WASMData.userData.isER}
upper1={`${upper1()}`} upper1={`${upper1(GSXActive() ? 'loaded' : loadingState)}`}
upper1max={loadingState === 'loaded' ? `${upper1('preview')}` : `${PaxConfig.stationMax.business1}`} upper1max={loadingState === 'loaded' || GSXActive() ? `${upper1('preview')}` : `${WASMData.limits.business1}`}
upper2={`${upper2()}`} upper2={`${upper2(GSXActive() ? 'loaded' : loadingState)}`}
upper2max={loadingState === 'loaded' ? `${upper2('preview')}` : `${PaxConfig.stationMax.business2}`} upper2max={loadingState === 'loaded' || GSXActive() ? `${upper2('preview')}` : `${WASMData.limits.business2}`}
upper3={`${upper3()}`} upper3={`${upper3(GSXActive() ? 'loaded' : loadingState)}`}
upper3max={loadingState === 'loaded' ? `${upper3('preview')}` : `${PaxConfig.stationMax.economy1}`} upper3max={loadingState === 'loaded' || GSXActive() ? `${upper3('preview')}` : `${WASMData.limits.economy1}`}
upper4={`${upper4()}`} upper4={`${upper4(GSXActive() ? 'loaded' : loadingState)}`}
upper4max={loadingState === 'loaded' ? `${upper4('preview')}` : `${PaxConfig.stationMax.economy2}`} upper4max={loadingState === 'loaded' || GSXActive() ? `${upper4('preview')}` : `${WASMData.limits.economy2}`}
lower1={`${lower1()}`} lower1={`${lower1()}`}
lower2={`${lower2()}`} lower2={`${lower2()}`}
OEW={`${_OEW()}`} OEW={`${OEW()}`}
crew={`${crew()}`} crew={`${crew()}`}
unit={unit.toUpperCase()} unit={WASMData.userData.isImperial ? 'LBS' : 'KG'}
inPreview={loadingState !== 'loaded'} inPreview={loadingState !== 'loaded' && !GSXActive()}
CGs={_CGs()} CGs={CGs()}
done={
WASMData.options.GSXSync ? WASMData.GSX.loadingState === GSXLoadingState.BOARDED : loadingState !== 'preview'
}
/> />
<Tabbar <Tabbar
tabs={ tabs={
@@ -170,64 +131,36 @@ const Pax: FC<PaxProps> = ({
selectedTab={selectedTab} selectedTab={selectedTab}
setSelectedTab={setSelectedTab} setSelectedTab={setSelectedTab}
/> />
{username && selectedTab === 0 && ( {username && selectedTab === 0 && (
<SBEntryPax <SBEntryPax
unit={unit} WASMData={WASMData}
isER={isER}
initialPayload={payload}
fuelLive={fuelLive}
payloadLive={payloadLive}
loadingState={loadingState} loadingState={loadingState}
username={username}
setLoadingState={setLoadingState} setLoadingState={setLoadingState}
updateView={(_payload) => { gsxActive={GSXActive()}
setPayload(_payload); gsxFuelActive={GSXFuelActive()}
}}
loadAircraft={() => {
PaxConfig.setBaseWeight(unit, isER);
PaxConfig.setWeights(payload, unit);
}}
/> />
)} )}
{((username && selectedTab === 1) || (!username && selectedTab === 0)) && ( {((username && selectedTab === 1) || (!username && selectedTab === 0)) && (
<ZFWEntryPax <ZFWEntryPax
unit={unit} WASMData={WASMData}
isER={isER}
initialPayload={payload}
fuelLive={fuelLive}
payloadLive={payloadLive}
loadingState={loadingState} loadingState={loadingState}
setLoadingState={setLoadingState} setLoadingState={setLoadingState}
updateView={(_payload) => { gsxActive={GSXActive()}
setPayload(_payload); gsxFuelActive={GSXFuelActive()}
}}
loadAircraft={() => {
PaxConfig.setBaseWeight(unit, isER);
PaxConfig.setWeights(payload, unit);
}}
/> />
)} )}
{((username && selectedTab === 2) || (!username && selectedTab === 1)) && ( {((username && selectedTab === 2) || (!username && selectedTab === 1)) && (
<StationEntryPax <StationEntryPax
unit={unit} WASMData={WASMData}
isER={isER}
initialPayload={payload}
fuelLive={fuelLive}
payloadLive={payloadLive}
loadingState={loadingState} loadingState={loadingState}
setLoadingState={setLoadingState} setLoadingState={setLoadingState}
updateView={(_payload) => { gsxActive={GSXActive()}
setPayload(_payload); gsxFuelActive={GSXFuelActive()}
}}
loadAircraft={() => {
PaxConfig.setBaseWeight(unit, isER);
PaxConfig.setWeights(payload, unit);
}}
/> />
)} )}
{((username && selectedTab === 3) || (!username && selectedTab === 2)) && (
<OptionsPax WASMData={WASMData} loadingState={loadingState} gsxActive={GSXActive()} />
)}
</> </>
); );
}; };
@@ -20,6 +20,7 @@ interface ProfileProps {
CGs: [string, boolean, string, boolean]; CGs: [string, boolean, string, boolean];
unit: string; unit: string;
inPreview: boolean; inPreview: boolean;
done: boolean;
} }
const Profile: FC<ProfileProps> = ({ const Profile: FC<ProfileProps> = ({
@@ -40,10 +41,12 @@ const Profile: FC<ProfileProps> = ({
CGs, CGs,
unit, unit,
inPreview, inPreview,
done,
}) => { }) => {
const previewClass = inPreview ? styles['fill-neutral-500'] : undefined; const previewClass = inPreview ? styles['fill-neutral-500'] : undefined;
const ZFWCGClass = CGs[1] ? styles['fill-red-500'] : previewClass; const doneClass = done ? undefined : styles['fill-neutral-500'];
const TOCGClass = CGs[3] ? styles['fill-red-500'] : previewClass; const ZFWCGClass = CGs[1] ? styles['fill-red-500'] : doneClass;
const TOCGClass = CGs[3] ? styles['fill-red-500'] : doneClass;
return ( return (
<svg viewBox="0 0 4002 780" version="1.1" xmlns="http://www.w3.org/2000/svg" className="mb-4"> <svg viewBox="0 0 4002 780" version="1.1" xmlns="http://www.w3.org/2000/svg" className="mb-4">
@@ -113,17 +116,17 @@ const Profile: FC<ProfileProps> = ({
</text> </text>
<text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="142.15625"> <text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="142.15625">
ZFWCG:
</text>
<text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="142.15625">
<tspan className={ZFWCGClass}>{CGs[0]}</tspan>
</text>
<text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="288.875">
TOCG: TOCG:
</text> </text>
<text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="288.875"> <text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="142.15625">
<tspan className={TOCGClass}>{CGs[2]}</tspan> <tspan className={TOCGClass}>{CGs[2]}</tspan>
</text> </text>
<text style={{ fill: 'white', fontSize: '160px' }} x="1730.4194" y="288.875">
ZFWCG:
</text>
<text style={{ fill: 'white', fontSize: '160px' }} x="2540.771" y="288.875">
<tspan className={ZFWCGClass}>{CGs[0]}</tspan>
</text>
<path <path
style={{ style={{
@@ -0,0 +1,221 @@
import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataF } from '../../types/WASMData';
import { CoherentCallStationEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
interface StationEntryProps {
WASMData: WASMDataF;
loadingState: LoadingState;
gsxActive: boolean;
gsxFuelActive: boolean;
setLoadingState: (newState: LoadingState) => void;
}
const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
const [upper1, setUpper1] = useState(WASMData.targetPayload.upper1);
const [upper2, setUpper2] = useState(WASMData.targetPayload.upper2);
const [upper3, setUpper3] = useState(WASMData.targetPayload.upper3);
const [upper4, setUpper4] = useState(WASMData.targetPayload.upper4);
const [lowerForward, setLowerForward] = useState(WASMData.targetPayload.lowerForward);
const [lowerRear, setLowerRear] = useState(WASMData.targetPayload.lowerRear);
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
return Math.round(WASMData.livePayload.total);
};
const ZFWValid = () => {
return ZFW() <= WASMData.limits.maxZFW;
};
const GW = () => {
return fuel + ZFW();
};
const GWValid = () => {
return GW() <= WASMData.limits.maxTOW;
};
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
if (!input) {
setter(0);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < 0) setter(0);
else if (converted > maxValue) setter(maxValue);
else setter(converted);
}
};
const updateData = () => {
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel);
};
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel]);
useEffect(
() =>
setFuel((prev) => {
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
return prev;
}),
[WASMData.userData.isER]
);
return (
<>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
value={fuel}
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxFuelActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Upper 1</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={upper1}
onChange={(value) => handleInput(value, WASMData.limits.upper1, setUpper1)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Upper 2</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={upper2}
onChange={(value) => handleInput(value, WASMData.limits.upper2, setUpper2)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Upper 3</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={upper3}
onChange={(value) => handleInput(value, WASMData.limits.upper3, setUpper3)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Upper 4</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={upper4}
onChange={(value) => handleInput(value, WASMData.limits.upper4, setUpper4)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Forward Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
topKeyboard
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={lowerForward}
onChange={(value) => handleInput(value, WASMData.limits.lowerForward, setLowerForward)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Aft Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
topKeyboard
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={lowerRear}
onChange={(value) => handleInput(value, WASMData.limits.lowerRear, setLowerRear)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={ZFW()}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={GW()}
/>
</div>
</div>
</div>
<ActionBar
loadingState={loadingState}
loadDisabled={!ZFWValid() || !GWValid()}
GSXSync={WASMData.options.GSXSync}
load={() => {
setLoadingState('loaded');
loadAircraft();
}}
unload={() => {
setLoadingState('preview');
unloadAircraft();
}}
/>
</>
);
};
export default StationEntryF;
@@ -1,117 +1,46 @@
import { FC, useEffect, useState } from 'react'; import { FC, useEffect, useState } from 'react';
import { PaxConfig, PayloadPax } from '../../configs/pax'; import { LoadingState } from '../../types/general';
import { Fuel, SharedConfig } from '../../configs/shared'; import { WASMDataPax } from '../../types/WASMData';
import { CoherentCallStationEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
import ActionBar from '../actionbar/ActionBar'; import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
interface StationEntryProps { interface StationEntryProps {
unit: 'kg' | 'lbs'; WASMData: WASMDataPax;
isER: boolean; loadingState: LoadingState;
initialPayload: PayloadPax; gsxActive: boolean;
fuelLive: Fuel; gsxFuelActive: boolean;
payloadLive: PayloadPax; setLoadingState: (newState: LoadingState) => void;
loadingState: 'preview' | 'accepted' | 'loaded';
setLoadingState: (newState: StationEntryProps['loadingState']) => void;
updateView: (payload: PayloadPax) => void;
loadAircraft: () => void;
} }
const StationEntryPax: FC<StationEntryProps> = ({ const StationEntryPax: FC<StationEntryProps> = ({
unit, WASMData,
isER,
initialPayload,
fuelLive,
payloadLive,
loadingState, loadingState,
gsxActive,
gsxFuelActive,
setLoadingState, setLoadingState,
updateView,
loadAircraft,
}) => { }) => {
const [business1, setBusiness1] = useState( const [business1, setBusiness1] = useState(WASMData.targetPayload.business1);
PaxConfig.weightToPax( const [business2, setBusiness2] = useState(WASMData.targetPayload.business2);
initialPayload.business1Left + initialPayload.business1Center + initialPayload.business1Right, const [economy1, setEconomy1] = useState(WASMData.targetPayload.economy1);
unit const [economy2, setEconomy2] = useState(WASMData.targetPayload.economy2);
) const [forwardCargo, setForwardCargo] = useState(WASMData.targetPayload.forwardCargo);
); const [rearCargo, setRearCargo] = useState(WASMData.targetPayload.rearCargo);
const [business2, setBusiness2] = useState( const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
PaxConfig.weightToPax(
initialPayload.business2Left + initialPayload.business2Center + initialPayload.business2Right,
unit
)
);
const [economy1, setEconomy1] = useState(
PaxConfig.weightToPax(
initialPayload.economy1Left + initialPayload.economy1Center + initialPayload.economy1Right,
unit
)
);
const [economy2, setEconomy2] = useState(
PaxConfig.weightToPax(
initialPayload.economy2Left + initialPayload.economy2Center + initialPayload.economy2Right,
unit
)
);
const [forwardCargo, setForwardCargo] = useState(initialPayload.forwardCargo);
const [rearCargo, setRearCargo] = useState(initialPayload.rearCargo);
const [fuel, setFuel] = useState(
Math.round(
fuelLive.main1 +
fuelLive.main1Tip +
fuelLive.main2 +
fuelLive.main3 +
fuelLive.main3Tip +
fuelLive.upperAux +
fuelLive.lowerAux +
fuelLive.tail +
fuelLive.forwardAux1 +
fuelLive.forwardAux2
)
);
const ZFW = () => { const ZFW = () => {
if (loadingState !== 'loaded') if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
return Math.round(
(business1 + business2 + economy1 + economy2) * PaxConfig.weights.pax[unit] +
forwardCargo +
rearCargo +
PaxConfig.weights.base[unit].total +
(isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) +
payloadLive.empty
);
return Math.round( return Math.round(WASMData.livePayload.total);
payloadLive.empty +
payloadLive.pilot +
payloadLive.firstOfficer +
payloadLive.engineer +
payloadLive.cabinCrewFront +
payloadLive.business1Left +
payloadLive.business1Center +
payloadLive.business1Right +
payloadLive.business2Left +
payloadLive.business2Center +
payloadLive.business2Right +
payloadLive.economy1Left +
payloadLive.economy1Center +
payloadLive.economy1Right +
payloadLive.economy2Left +
payloadLive.economy2Center +
payloadLive.economy2Right +
payloadLive.cabinCrewRear +
payloadLive.forwardCargo +
payloadLive.rearCargo +
payloadLive.leftAuxPax +
payloadLive.rightAuxPax
);
}; };
const ZFWValid = () => { const ZFWValid = () => {
return ZFW() <= PaxConfig.maxZWF[unit]; return ZFW() <= WASMData.limits.maxZFW;
}; };
const GW = () => { const GW = () => {
return fuel + ZFW(); return fuel + ZFW();
}; };
const GWValid = () => { const GWValid = () => {
return GW() <= (isER ? SharedConfig.maxTOW.er[unit] : SharedConfig.maxTOW.norm[unit]); return GW() <= WASMData.limits.maxTOW;
}; };
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => { const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
@@ -128,169 +57,158 @@ const StationEntryPax: FC<StationEntryProps> = ({
} }
}; };
useEffect(() => _updateView(), [business1, business2, economy1, economy2, forwardCargo, rearCargo]); const updateData = () => {
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel);
};
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel]);
useEffect( useEffect(
() => () =>
setFuel((prev) => setFuel((prev) => {
prev > (isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit]) if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
? isER return prev;
? SharedConfig.maxFuel.er[unit] }),
: SharedConfig.maxFuel.norm[unit] [WASMData.userData.isER]
: prev
),
[isER]
); );
const _updateView = () => {
const payload = PaxConfig.generateDistribution(
payloadLive.empty,
business1,
business2,
economy1,
economy2,
forwardCargo,
rearCargo,
unit,
isER
);
updateView(payload);
};
return ( return (
<> <>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label>Business</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={business1}
onChange={(e) => handleInput(e.target.value, PaxConfig.stationMax.business1, setBusiness1)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<label>Premium Economy</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={business2}
onChange={(e) => handleInput(e.target.value, PaxConfig.stationMax.business2, setBusiness2)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<label>Forward Economy</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={economy1}
onChange={(e) => handleInput(e.target.value, PaxConfig.stationMax.economy1, setEconomy1)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<label>Aft Economy</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={economy2}
onChange={(e) => handleInput(e.target.value, PaxConfig.stationMax.economy2, setEconomy2)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<label>Forward Cargo ({unit})</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={forwardCargo}
onChange={(e) => handleInput(e.target.value, SharedConfig.stationMax.forward[unit], setForwardCargo)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<label>Aft Cargo ({unit})</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={rearCargo}
onChange={(e) => handleInput(e.target.value, SharedConfig.stationMax.rear[unit], setRearCargo)}
disabled={loadingState !== 'preview'}
/>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<label>Fuel ({unit})</label> <div className="flex w-full items-center justify-between text-xs">
<input <label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
type="text" <Input
placeholder="" type="text"
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`} placeholder=""
value={fuel} className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
onChange={(e) => value={fuel}
handleInput( onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
e.target.value, disabled={loadingState !== 'preview' || gsxFuelActive}
isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit], />
setFuel </div>
)
}
disabled={loadingState !== 'preview'}
/>
<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', unit === 'kg' ? fuel * 2.20462262185 : fuel);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
}}
disabled={loadingState !== 'preview'}
>
Load Fuel
</button>
</div> </div>
</div> </div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} ZFW ({unit}) <label>Business</label>
</label> <Input
<input type="text"
type="text" placeholder=""
placeholder="" className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} value={business1}
disabled onChange={(value) => handleInput(value, WASMData.limits.business1, setBusiness1)}
value={ZFW()} disabled={loadingState !== 'preview' || gsxActive}
/> />
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Premium Economy</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={business2}
onChange={(value) => handleInput(value, WASMData.limits.business2, setBusiness2)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Forward Economy</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={economy1}
onChange={(value) => handleInput(value, WASMData.limits.economy1, setEconomy1)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Aft Economy</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={economy2}
onChange={(value) => handleInput(value, WASMData.limits.economy2, setEconomy2)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Forward Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
topKeyboard
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={forwardCargo}
onChange={(value) => handleInput(value, WASMData.limits.forwardCargo, setForwardCargo)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div> </div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} GW ({unit}) <label>Aft Cargo ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
</label> <Input
<input type="text"
type="text" topKeyboard
placeholder="" placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} 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"
disabled value={rearCargo}
value={GW()} onChange={(value) => handleInput(value, WASMData.limits.rearCargo, setRearCargo)}
/> disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={ZFW()}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={GW()}
/>
</div>
</div> </div>
</div> </div>
<ActionBar <ActionBar
loadingState={loadingState} loadingState={loadingState}
acceptDisabled={!ZFWValid() || !GWValid()} loadDisabled={!ZFWValid() || !GWValid()}
accept={() => setLoadingState('accepted')} GSXSync={WASMData.options.GSXSync}
reject={() => setLoadingState('preview')}
load={() => { load={() => {
setLoadingState('loaded'); setLoadingState('loaded');
@@ -299,7 +217,7 @@ const StationEntryPax: FC<StationEntryProps> = ({
unload={() => { unload={() => {
setLoadingState('preview'); setLoadingState('preview');
PaxConfig.unload(unit, isER); unloadAircraft();
}} }}
/> />
</> </>
@@ -0,0 +1,51 @@
interface ToggleComponentProps<T> {
optionName: string;
value: T;
leftLabel: {
value: T;
label?: string;
};
rightLabel: {
value: T;
label?: string;
};
backgroundColor: string;
disabled?: boolean;
setValue: (value: T) => void;
}
const ToggleComponentKH = <T,>({
optionName,
value,
leftLabel,
rightLabel,
backgroundColor,
disabled,
setValue,
}: ToggleComponentProps<T>) => {
return (
<div className="flex w-full items-center justify-between text-xs">
<span>{optionName}</span>
<div className="inline-flex w-1/2 rounded-md shadow-sm">
<button
type="button"
className={`${value === leftLabel.value ? 'bg-green-700' : backgroundColor} w-1/2 rounded-l-lg border border-white px-4 py-2 text-white disabled:pointer-events-none disabled:opacity-50`}
onClick={() => setValue(leftLabel.value)}
disabled={disabled}
>
{leftLabel.label || 'Enabled'}
</button>
<button
type="button"
className={`${value === rightLabel.value ? 'bg-green-700' : backgroundColor} w-1/2 rounded-r-md border border-white px-4 py-2 text-white disabled:pointer-events-none disabled:opacity-50`}
onClick={() => setValue(rightLabel.value)}
disabled={disabled}
>
{rightLabel.label || 'Disabled'}
</button>
</div>
</div>
);
};
export default ToggleComponentKH;
@@ -0,0 +1,206 @@
import { FC, useEffect, useState } from 'react';
import { WASMDataF } from '../../types/WASMData';
import { LoadingState } from '../../types/general';
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
interface ZFWEntryProps {
WASMData: WASMDataF;
loadingState: LoadingState;
gsxActive: boolean;
gsxFuelActive: boolean;
setLoadingState: (newState: LoadingState) => void;
}
const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
return Math.round(WASMData.livePayload.total);
};
const ZFWValid = () => {
return ZFW() <= WASMData.limits.maxZFW;
};
const GW = () => {
return fuel + ZFW();
};
const GWValid = () => {
return GW() <= WASMData.limits.maxTOW;
};
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
if (!input) {
setter(0);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < 0) setter(0);
else if (converted > maxValue) setter(maxValue);
else setter(converted);
}
};
const handleInputZFW = (input: string) => {
if (!input) {
setZFWTarget(0);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted <= 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
};
const handleBlurZFW = (input: string) => {
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
if (!input) {
setZFWTarget(minZFW);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < minZFW) setZFWTarget(minZFW);
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
};
const updateData = () => {
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
};
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
useEffect(
() =>
setFuel((prev) => {
if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
return prev;
}),
[WASMData.userData.isER]
);
return (
<>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
value={fuel}
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxFuelActive}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>Target ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
<Input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={ZFWTarget}
onChange={(value) => handleInputZFW(value)}
onBlur={(value) => handleBlurZFW(value)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
</label>
<CGSelect
minCG={WASMData.limits.minCG}
maxCG={WASMData.limits.maxCG}
value={CGTarget}
disabled={loadingState !== 'preview' || gsxActive}
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
return _new;
})
}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={ZFW()}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={GW()}
/>
</div>
</div>
</div>
<ActionBar
loadingState={loadingState}
loadDisabled={!GWValid()}
GSXSync={WASMData.options.GSXSync}
load={() => {
setLoadingState('loaded');
loadAircraft();
}}
unload={() => {
setLoadingState('preview');
unloadAircraft();
}}
/>
</>
);
};
export default ZFWEntryF;
@@ -1,106 +1,37 @@
import { FC, useEffect, useState } from 'react'; import { FC, useEffect, useState } from 'react';
import { PaxConfig, PayloadPax } from '../../configs/pax'; import { WASMDataPax } from '../../types/WASMData';
import { Fuel, SharedConfig } from '../../configs/shared'; import { LoadingState } from '../../types/general';
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';
interface StationEntryProps { interface ZFWEntryProps {
unit: 'kg' | 'lbs'; WASMData: WASMDataPax;
isER: boolean; loadingState: LoadingState;
initialPayload: PayloadPax; gsxActive: boolean;
fuelLive: Fuel; gsxFuelActive: boolean;
payloadLive: PayloadPax; setLoadingState: (newState: LoadingState) => void;
loadingState: 'preview' | 'accepted' | 'loaded';
setLoadingState: (newState: StationEntryProps['loadingState']) => void;
updateView: (payload: PayloadPax) => void;
loadAircraft: () => void;
} }
const ZFWEntryPax: FC<StationEntryProps> = ({ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, gsxFuelActive, setLoadingState }) => {
unit, const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
isER, const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
initialPayload, const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
fuelLive,
payloadLive,
loadingState,
setLoadingState,
updateView,
loadAircraft,
}) => {
const [targetZFWCG, setTargetZFWCG] = useState(SharedConfig.CGLimits.default);
const [fuel, setFuel] = useState(
Math.round(
fuelLive.main1 +
fuelLive.main1Tip +
fuelLive.main2 +
fuelLive.main3 +
fuelLive.main3Tip +
fuelLive.upperAux +
fuelLive.lowerAux +
fuelLive.tail +
fuelLive.forwardAux1 +
fuelLive.forwardAux2
)
);
const [ZFW, setZFW] = useState(
Math.round(
PaxConfig.weights.base[unit].total +
(isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) +
payloadLive.empty +
initialPayload.business1Left +
initialPayload.business1Center +
initialPayload.business1Right +
initialPayload.business2Left +
initialPayload.business2Center +
initialPayload.business2Right +
initialPayload.economy1Left +
initialPayload.economy1Center +
initialPayload.economy1Right +
initialPayload.economy2Left +
initialPayload.economy2Center +
initialPayload.economy2Right +
initialPayload.forwardCargo +
initialPayload.rearCargo
)
);
const _ZFW = () => { const ZFW = () => {
if (loadingState !== 'loaded') return ZFW; if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
return Math.round( return Math.round(WASMData.livePayload.total);
payloadLive.empty +
payloadLive.pilot +
payloadLive.firstOfficer +
payloadLive.engineer +
payloadLive.cabinCrewFront +
payloadLive.business1Left +
payloadLive.business1Center +
payloadLive.business1Right +
payloadLive.business2Left +
payloadLive.business2Center +
payloadLive.business2Right +
payloadLive.economy1Left +
payloadLive.economy1Center +
payloadLive.economy1Right +
payloadLive.economy2Left +
payloadLive.economy2Center +
payloadLive.economy2Right +
payloadLive.cabinCrewRear +
payloadLive.forwardCargo +
payloadLive.rearCargo +
payloadLive.leftAuxPax +
payloadLive.rightAuxPax
);
}; };
const ZFWValid = () => { const ZFWValid = () => {
return _ZFW() <= PaxConfig.maxZWF[unit]; return ZFW() <= WASMData.limits.maxZFW;
}; };
const GW = () => { const GW = () => {
return fuel + _ZFW(); return fuel + ZFW();
}; };
const GWValid = () => { const GWValid = () => {
return GW() <= (isER ? SharedConfig.maxTOW.er[unit] : SharedConfig.maxTOW.norm[unit]); return GW() <= WASMData.limits.maxTOW;
}; };
const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => { const handleInput = (input: string, maxValue: number, setter: (value: number) => void) => {
@@ -117,155 +48,146 @@ const ZFWEntryPax: FC<StationEntryProps> = ({
} }
}; };
const handleInputZFW = (input: string) => { const handleInputZFW = (input: string) => {
if (!input) return;
const converted = parseInt(input);
if (converted) {
if (converted < 0)
setZFW(
Math.round(
PaxConfig.weights.base[unit].total + (isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) + payloadLive.empty
)
);
else if (converted > PaxConfig.maxZWF[unit]) setZFW(PaxConfig.maxZWF[unit]);
else setZFW(converted);
}
};
const handleBlur = (input: string) => {
const minZFW = Math.round(
PaxConfig.weights.base[unit].total + (isER ? SharedConfig.erExtraWeight[unit] * 2 : 0) + payloadLive.empty
);
if (!input) { if (!input) {
setZFW(minZFW); setZFWTarget(0);
return; return;
} }
const converted = parseInt(input); const converted = parseInt(input);
if (converted) { if (converted) {
if (converted < minZFW) setZFW(minZFW); if (converted < 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
else if (converted > PaxConfig.maxZWF[unit]) setZFW(PaxConfig.maxZWF[unit]); else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFW(converted); else setZFWTarget(converted);
} }
updateView(PaxConfig.distribute(converted, targetZFWCG, payloadLive.empty, fuelLive, unit, isER));
}; };
const handleBlurZFW = (input: string) => {
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
if (!input) {
setZFWTarget(minZFW);
return;
}
const converted = parseInt(input);
if (converted) {
if (converted < minZFW) setZFWTarget(minZFW);
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
};
const updateData = () => {
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
};
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
useEffect( useEffect(
() => () =>
setFuel((prev) => setFuel((prev) => {
prev > (isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit]) if (prev > WASMData.limits.maxFuel) return WASMData.limits.maxFuel;
? isER return prev;
? SharedConfig.maxFuel.er[unit] }),
: SharedConfig.maxFuel.norm[unit] [WASMData.userData.isER]
: prev
),
[isER]
); );
return ( return (
<> <>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label>Target ZFW ({unit})</label>
<input
type="text"
placeholder=""
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={ZFW}
onChange={(e) => handleInputZFW(e.target.value)}
onBlur={(e) => handleBlur(e.target.value)}
disabled={loadingState !== 'preview'}
/>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<label>
Target ZFWCG ({SharedConfig.CGLimits.min} - {SharedConfig.CGLimits.max})
</label>
<CGSelect
value={targetZFWCG}
disabled={loadingState !== 'preview'}
increase={() =>
setTargetZFWCG((prev) => {
const _new = prev + 0.1;
updateView(PaxConfig.distribute(ZFW, _new, payloadLive.empty, fuelLive, unit, isER));
return _new;
})
}
decrease={() =>
setTargetZFWCG((prev) => {
const _new = prev - 0.1;
updateView(PaxConfig.distribute(ZFW, _new, payloadLive.empty, fuelLive, unit, isER));
return _new;
})
}
/>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-md bg-zinc-600 p-2 px-4">
<label>Fuel ({unit})</label> <div className="flex w-full items-center justify-between text-xs">
<input <label>Fuel ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
type="text" <Input
placeholder="" type="text"
className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`} placeholder=""
value={fuel} className={`w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right`}
onChange={(e) => value={fuel}
handleInput( onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
e.target.value, disabled={loadingState !== 'preview' || gsxFuelActive}
isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit], />
setFuel </div>
)
}
disabled={loadingState !== 'preview'}
/>
<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', unit === 'kg' ? fuel * 2.20462262185 : fuel);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
}}
disabled={loadingState !== 'preview'}
>
Load Fuel
</button>
</div> </div>
</div> </div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4"> <div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} ZFW ({unit}) <label>Target ZFW ({WASMData.userData.isImperial ? 'lbs' : 'kg'})</label>
</label> <Input
<input type="text"
type="text" placeholder=""
placeholder="" className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} value={ZFWTarget}
disabled onChange={(value) => handleInputZFW(value)}
value={_ZFW()} onBlur={(value) => handleBlurZFW(value)}
/> disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
</div> </div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4"> <div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<label> <div className="flex w-full items-center justify-between text-xs">
{loadingState !== 'loaded' ? 'Expected' : 'Actual'} GW ({unit}) <label>
</label> Target ZFWCG ({WASMData.limits.minCG} - {WASMData.limits.maxCG})
<input </label>
type="text" <CGSelect
placeholder="" minCG={WASMData.limits.minCG}
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`} maxCG={WASMData.limits.maxCG}
disabled value={CGTarget}
value={GW()} disabled={loadingState !== 'preview' || gsxActive}
/> increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
return _new;
})
}
/>
</div>
</div>
</div>
<div className="block flex w-full flex-col opacity-100 transition-opacity duration-150 ease-linear mb-4">
<div className="relative flex w-full items-center justify-between rounded-t-md bg-zinc-600 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} ZFW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${ZFWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={ZFW()}
/>
</div>
</div>
<div className="relative flex w-full items-center justify-between rounded-b-md bg-zinc-700 p-2 px-4">
<div className="flex w-full items-center justify-between text-xs">
<label>
{loadingState !== 'loaded' && !gsxActive ? 'Expected' : 'Actual'} GW (
{WASMData.userData.isImperial ? 'lbs' : 'kg'})
</label>
<input
type="text"
placeholder=""
className={`w-1/2 rounded-lg border ${GWValid() ? 'border-white' : 'border-red-500 text-red-500'} bg-zinc-700 px-3 py-2 text-right`}
disabled
value={GW()}
/>
</div>
</div> </div>
</div> </div>
<ActionBar <ActionBar
loadingState={loadingState} loadingState={loadingState}
acceptDisabled={!GWValid()} loadDisabled={!GWValid()}
accept={() => setLoadingState('accepted')} GSXSync={WASMData.options.GSXSync}
reject={() => setLoadingState('preview')}
load={() => { load={() => {
setLoadingState('loaded'); setLoadingState('loaded');
@@ -274,7 +196,7 @@ const ZFWEntryPax: FC<StationEntryProps> = ({
unload={() => { unload={() => {
setLoadingState('preview'); setLoadingState('preview');
PaxConfig.unload(unit, isER); unloadAircraft();
}} }}
/> />
</> </>
@@ -1,153 +0,0 @@
import { ArmsFuel, Fuel, toPercentMAC } from './shared';
// TODO: Extract from CFG at runtime.
const ArmsFreight = {
empty: -159.6,
pilot: 984,
firstOfficer: 984,
engineer: 960,
upper1Left: 660,
upper1Right: 660,
upper2Left: 240,
upper2Right: 240,
upper3Left: -240,
upper3Right: -240,
upper4Left: -600,
upper4Right: -600,
lowerForward: 360,
lowerRear: -360,
leftAuxF: 60,
rightAuxF: 60,
};
export interface PayloadFreight {
empty: number;
pilot: number;
firstOfficer: number;
engineer: number;
upper1Left: number;
upper1Right: number;
upper2Left: number;
upper2Right: number;
upper3Left: number;
upper3Right: number;
upper4Left: number;
upper4Right: number;
lowerForward: number;
lowerRear: number;
leftAuxF: number;
rightAuxF: number;
}
//PMC pallet
export const maxUpperStationWeight = {
lbs: (26 / 8) * 15000,
kg: (26 / 8) * 6804,
};
export const baseWeightFreight = {
pilot: {
lbs: 190,
kg: 86,
},
firstOfficer: {
lbs: 190,
kg: 86,
},
};
export const maxZFWFreight = {
lbs: 451300,
kg: 204706,
};
export const calculateCGsFreight = (payload: PayloadFreight, fuel: Fuel): [number, number] => {
let totalMoment =
payload.empty * ArmsFreight.empty +
payload.pilot * ArmsFreight.pilot +
payload.firstOfficer * ArmsFreight.firstOfficer +
payload.engineer * ArmsFreight.engineer +
payload.upper1Left * ArmsFreight.upper1Left +
payload.upper1Right * ArmsFreight.upper1Right +
payload.upper2Left * ArmsFreight.upper2Left +
payload.upper2Right * ArmsFreight.upper2Right +
payload.upper3Left * ArmsFreight.upper3Left +
payload.upper3Right * ArmsFreight.upper3Right +
payload.upper4Left * ArmsFreight.upper4Left +
payload.upper4Right * ArmsFreight.upper4Right +
payload.lowerForward * ArmsFreight.lowerForward +
payload.lowerRear * ArmsFreight.lowerRear +
payload.leftAuxF * ArmsFreight.leftAuxF +
payload.rightAuxF * ArmsFreight.rightAuxF;
let totalWeight =
payload.empty +
payload.pilot +
payload.firstOfficer +
payload.engineer +
payload.upper1Left +
payload.upper1Right +
payload.upper2Left +
payload.upper2Right +
payload.upper3Left +
payload.upper3Right +
payload.upper4Left +
payload.upper4Right +
payload.lowerForward +
payload.lowerRear +
payload.leftAuxF +
payload.rightAuxF;
const ZFWCG = toPercentMAC(totalMoment / totalWeight);
totalMoment +=
fuel.main1 * ArmsFuel.main1 +
fuel.main3 * ArmsFuel.main3 +
fuel.main2 * ArmsFuel.main2 +
fuel.upperAux * ArmsFuel.upperAux +
fuel.lowerAux * ArmsFuel.lowerAux +
fuel.main1Tip * ArmsFuel.main1Tip +
fuel.main3Tip * ArmsFuel.main3Tip +
fuel.tail * ArmsFuel.tail +
fuel.forwardAux1 * ArmsFuel.forwardAux1 +
fuel.forwardAux2 * ArmsFuel.forwardAux2;
totalWeight +=
fuel.main1 +
fuel.main3 +
fuel.main2 +
fuel.upperAux +
fuel.lowerAux +
fuel.main1Tip +
fuel.main3Tip +
fuel.tail +
fuel.forwardAux1 +
fuel.forwardAux2;
const TOCG = toPercentMAC(totalMoment / totalWeight);
return [ZFWCG, TOCG];
};
export const getWeightsFreight = (unit: 'kg' | 'lbs') => {
const payload: PayloadFreight = {
empty: SimVar.GetSimVarValue('EMPTY WEIGHT', unit),
pilot: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:1', unit),
firstOfficer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:2', unit),
engineer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:3', unit),
upper1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:4', unit),
upper1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:5', unit),
upper2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:6', unit),
upper2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:7', unit),
upper3Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:8', unit),
upper3Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:9', unit),
upper4Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:10', unit),
upper4Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:11', unit),
lowerForward: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:12', unit),
lowerRear: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:13', unit),
leftAuxF: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:14', unit),
rightAuxF: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:15', unit),
};
return payload;
};
-598
View File
@@ -1,598 +0,0 @@
import { ArmsFuel, Fuel, SharedConfig, toPercentMAC } from './shared';
export interface PayloadPax {
empty: number;
pilot: number;
firstOfficer: number;
engineer: number;
cabinCrewFront: number;
business1Left: number;
business1Center: number;
business1Right: number;
business2Left: number;
business2Center: number;
business2Right: number;
economy1Left: number;
economy1Center: number;
economy1Right: number;
economy2Left: number;
economy2Center: number;
economy2Right: number;
cabinCrewRear: number;
forwardCargo: number;
rearCargo: number;
leftAuxPax: number;
rightAuxPax: number;
paxCount: {
business1: number;
business2: number;
economy1: number;
economy2: number;
total: number;
};
}
export const PaxConfig = {
// TODO: Extract from CFG at runtime.
arms: {
empty: -159.6,
pilot: 984,
firstOfficer: 984,
engineer: 960,
cabinCrewFront: 792,
business1Left: 540,
business1Center: 540,
business1Right: 540,
business2Left: 300,
business2Center: 300,
business2Right: 300,
economy1Left: -240,
economy1Center: -240,
economy1Right: -240,
economy2Left: -600,
economy2Center: -600,
economy2Right: -600,
cabinCrewRear: -660,
forwardCargo: 360,
rearCargo: -360,
leftAuxPax: 60,
rightAuxPax: 60,
},
// TODO: Make user adjustable
weights: {
pax: {
lbs: 190,
kg: 86,
},
baggage: {
lbs: 50,
kg: 23,
},
base: {
lbs: {
pilot: 190,
firstOfficer: 190,
engineer: 190,
cabinCrewFront: 380,
cabinCrewRear: 950,
total: 190 + 190 + 190 + 380 + 950,
},
kg: {
pilot: 86,
firstOfficer: 86,
engineer: 86,
cabinCrewFront: 172,
cabinCrewRear: 430,
total: 86 + 86 + 86 + 172 + 430,
},
},
},
stationMax: {
business1: 30,
business2: 45,
economy1: 86,
economy2: 137,
total: 30 + 45 + 86 + 137,
},
maxZWF: {
lbs: 400000,
kg: 181437,
},
weightToPax: (weight: number, unit: 'kg' | 'lbs') => {
return Math.round(weight / PaxConfig.weights.pax[unit]);
},
calculateCGs: (payload: PayloadPax, fuel: Fuel): [number, number] => {
let totalMoment =
payload.empty * PaxConfig.arms.empty +
payload.pilot * PaxConfig.arms.pilot +
payload.firstOfficer * PaxConfig.arms.firstOfficer +
payload.engineer * PaxConfig.arms.engineer +
payload.cabinCrewFront * PaxConfig.arms.cabinCrewFront +
payload.business1Left * PaxConfig.arms.business1Left +
payload.business1Center * PaxConfig.arms.business1Center +
payload.business1Right * PaxConfig.arms.business1Right +
payload.business2Left * PaxConfig.arms.business2Left +
payload.business2Center * PaxConfig.arms.business2Center +
payload.business2Right * PaxConfig.arms.business2Right +
payload.economy1Left * PaxConfig.arms.economy1Left +
payload.economy1Center * PaxConfig.arms.economy1Center +
payload.economy1Right * PaxConfig.arms.economy1Right +
payload.economy2Left * PaxConfig.arms.economy2Left +
payload.economy2Center * PaxConfig.arms.economy2Center +
payload.economy2Right * PaxConfig.arms.economy2Right +
payload.cabinCrewRear * PaxConfig.arms.cabinCrewRear +
payload.forwardCargo * PaxConfig.arms.forwardCargo +
payload.rearCargo * PaxConfig.arms.rearCargo +
payload.leftAuxPax * PaxConfig.arms.leftAuxPax +
payload.rightAuxPax * PaxConfig.arms.rightAuxPax;
let totalWeight =
payload.empty +
payload.pilot +
payload.firstOfficer +
payload.engineer +
payload.cabinCrewFront +
payload.business1Left +
payload.business1Center +
payload.business1Right +
payload.business2Left +
payload.business2Center +
payload.business2Right +
payload.economy1Left +
payload.economy1Center +
payload.economy1Right +
payload.economy2Left +
payload.economy2Center +
payload.economy2Right +
payload.cabinCrewRear +
payload.forwardCargo +
payload.rearCargo +
payload.leftAuxPax +
payload.rightAuxPax;
const ZFWCG = toPercentMAC(totalMoment / totalWeight);
totalMoment +=
fuel.main1 * ArmsFuel.main1 +
fuel.main3 * ArmsFuel.main3 +
fuel.main2 * ArmsFuel.main2 +
fuel.upperAux * ArmsFuel.upperAux +
fuel.lowerAux * ArmsFuel.lowerAux +
fuel.main1Tip * ArmsFuel.main1Tip +
fuel.main3Tip * ArmsFuel.main3Tip +
fuel.tail * ArmsFuel.tail +
fuel.forwardAux1 * ArmsFuel.forwardAux1 +
fuel.forwardAux2 * ArmsFuel.forwardAux2;
totalWeight +=
fuel.main1 +
fuel.main3 +
fuel.main2 +
fuel.upperAux +
fuel.lowerAux +
fuel.main1Tip +
fuel.main3Tip +
fuel.tail +
fuel.forwardAux1 +
fuel.forwardAux2;
const toCG = toPercentMAC(totalMoment / totalWeight);
return [ZFWCG, toCG];
},
generateDistribution: (
OEW: number,
business1: number,
business2: number,
economy1: number,
economy2: number,
forwardCargo: number,
rearCargo: number,
unit: 'kg' | 'lbs',
isER: boolean
): PayloadPax => {
const distribution: PayloadPax = {
empty: OEW,
...PaxConfig.weights.base[unit],
business1Left: (business1 / 3) * PaxConfig.weights.pax[unit],
business1Center: (business1 / 3) * PaxConfig.weights.pax[unit],
business1Right: (business1 / 3) * PaxConfig.weights.pax[unit],
business2Left: (business2 / 3) * PaxConfig.weights.pax[unit],
business2Center: (business2 / 3) * PaxConfig.weights.pax[unit],
business2Right: (business2 / 3) * PaxConfig.weights.pax[unit],
economy1Left: (economy1 / 3) * PaxConfig.weights.pax[unit],
economy1Center: (economy1 / 3) * PaxConfig.weights.pax[unit],
economy1Right: (economy1 / 3) * PaxConfig.weights.pax[unit],
economy2Left: (economy2 / 3) * PaxConfig.weights.pax[unit],
economy2Center: (economy2 / 3) * PaxConfig.weights.pax[unit],
economy2Right: (economy2 / 3) * PaxConfig.weights.pax[unit],
forwardCargo: forwardCargo,
rearCargo: rearCargo,
leftAuxPax: isER ? SharedConfig.erExtraWeight[unit] : 0,
rightAuxPax: isER ? SharedConfig.erExtraWeight[unit] : 0,
paxCount: {
business1,
business2,
economy1,
economy2,
total: business1 + business2 + economy1 + economy2,
},
};
return distribution;
},
distribute: (
ZFWTarget: number,
CGTarget: number,
OEW: number,
fuelLive: Fuel,
unit: 'kg' | 'lbs',
isER: boolean,
numPax?: number
) => {
const payload =
ZFWTarget -
OEW -
PaxConfig.weights.base[unit].pilot -
PaxConfig.weights.base[unit].firstOfficer -
PaxConfig.weights.base[unit].engineer -
PaxConfig.weights.base[unit].cabinCrewFront -
PaxConfig.weights.base[unit].cabinCrewRear -
(isER ? SharedConfig.erExtraWeight[unit] * 2 : 0);
let _numPax =
numPax ??
Math.max(
0,
Math.min(
PaxConfig.stationMax.total,
Math.floor(payload / (PaxConfig.weights.pax[unit] + PaxConfig.weights.baggage[unit]))
)
);
let cargo = Math.round(payload - _numPax * PaxConfig.weights.pax[unit] - _numPax * PaxConfig.weights.baggage[unit]);
let business1 = 0;
let business2 = 0;
let economy1 = 0;
let economy2 = 0;
let forwardCargo = 0;
let rearCargo = 0;
let __numPax = 0;
let count = PaxConfig.stationMax.economy2;
// initial distribution
while (_numPax > 0 && count > 0) {
if (_numPax >= 4) {
if (business1 < PaxConfig.stationMax.business1) {
business1++;
__numPax++;
}
if (business2 < PaxConfig.stationMax.business2) {
business2++;
__numPax++;
}
if (economy1 < PaxConfig.stationMax.economy1) {
economy1++;
__numPax++;
}
if (economy2 < PaxConfig.stationMax.economy2) {
economy2++;
__numPax++;
}
} else if (_numPax === 3) {
if (business2 < PaxConfig.stationMax.business2) {
business2++;
__numPax++;
}
if (economy1 < PaxConfig.stationMax.economy1) {
economy1++;
__numPax++;
}
if (economy2 < PaxConfig.stationMax.economy2) {
economy2++;
__numPax++;
}
} else if (_numPax === 2) {
if (economy1 < PaxConfig.stationMax.economy1) {
economy1++;
__numPax++;
}
if (economy2 < PaxConfig.stationMax.economy2) {
economy2++;
__numPax++;
}
} else if (_numPax === 1) {
if (economy2 < PaxConfig.stationMax.economy2) {
economy2++;
__numPax++;
}
}
_numPax -= __numPax;
if (__numPax % 2 === 0) {
forwardCargo += (__numPax / 2) * PaxConfig.weights.baggage[unit];
rearCargo += (__numPax / 2) * PaxConfig.weights.baggage[unit];
} else {
__numPax--;
forwardCargo += (__numPax / 2 + 1) * PaxConfig.weights.baggage[unit];
rearCargo += (__numPax / 2) * PaxConfig.weights.baggage[unit];
}
__numPax = 0;
count--;
}
count = SharedConfig.stationMax.forward[unit];
while (cargo > 0 && count > 0) {
if (forwardCargo < SharedConfig.stationMax.forward[unit]) {
forwardCargo++;
cargo--;
}
if (rearCargo < SharedConfig.stationMax.rear[unit]) {
rearCargo++;
cargo--;
}
count--;
}
// Refinement pax
count = PaxConfig.stationMax.total;
while (count > 0) {
const distribution = PaxConfig.generateDistribution(
OEW,
business1,
business2,
economy1,
economy2,
forwardCargo,
rearCargo,
unit,
isER
);
const _CGs = PaxConfig.calculateCGs(distribution, fuelLive);
// in front of target
if (_CGs[0] < CGTarget - SharedConfig.CGLimits.tolerance) {
if (business1 > 0) {
business1--;
} else if (business2 > 0) {
business2--;
} else if (economy1 > 0) {
economy1--;
} else {
break;
}
if (economy2 < PaxConfig.stationMax.economy2) {
economy2++;
} else if (economy1 < PaxConfig.stationMax.economy1) {
economy1++;
} else if (business2 < PaxConfig.stationMax.business2) {
business2++;
} else {
business1++;
}
}
// behind target
else if (_CGs[0] > CGTarget + SharedConfig.CGLimits.tolerance) {
if (economy2 > 0) {
economy2--;
} else if (economy1 > 0) {
economy1--;
} else if (business2 > 0) {
business2--;
} else {
break;
}
if (business1 < PaxConfig.stationMax.business1) {
business1++;
} else if (business2 < PaxConfig.stationMax.business2) {
business2++;
} else if (economy1 < PaxConfig.stationMax.economy1) {
economy1++;
} else {
economy2++;
}
} else {
break;
}
count--;
}
// Refinement cargo
count = SharedConfig.stationMax.forward[unit] + SharedConfig.stationMax.rear[unit];
while (count > 0) {
const distribution = PaxConfig.generateDistribution(
OEW,
business1,
business2,
economy1,
economy2,
forwardCargo,
rearCargo,
unit,
isER
);
const _CGs = PaxConfig.calculateCGs(distribution, fuelLive);
// in front of target
if (_CGs[0] < CGTarget - SharedConfig.CGLimits.tolerance) {
if (forwardCargo > 0 && rearCargo < SharedConfig.stationMax.rear[unit]) {
if (
forwardCargo > PaxConfig.weights.baggage[unit] &&
rearCargo < SharedConfig.stationMax.forward[unit] - PaxConfig.weights.baggage[unit]
) {
forwardCargo -= PaxConfig.weights.baggage[unit];
rearCargo += PaxConfig.weights.baggage[unit];
} else {
forwardCargo--;
rearCargo++;
}
} else {
break;
}
}
// behind target
else if (_CGs[0] > CGTarget + SharedConfig.CGLimits.tolerance) {
if (rearCargo > 0 && forwardCargo < SharedConfig.stationMax.forward[unit]) {
if (
rearCargo > PaxConfig.weights.baggage[unit] &&
forwardCargo < SharedConfig.stationMax.rear[unit] - PaxConfig.weights.baggage[unit]
) {
rearCargo -= PaxConfig.weights.baggage[unit];
forwardCargo += PaxConfig.weights.baggage[unit];
} else {
rearCargo--;
forwardCargo++;
}
} else {
break;
}
} else {
break;
}
count--;
}
const distribution = PaxConfig.generateDistribution(
OEW,
business1,
business2,
economy1,
economy2,
forwardCargo,
rearCargo,
unit,
isER
);
return distribution;
},
// SIM access
getWeights: (unit: 'kg' | 'lbs') => {
const payload: PayloadPax = {
empty: SimVar.GetSimVarValue('EMPTY WEIGHT', unit),
pilot: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:1', unit),
firstOfficer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:2', unit),
engineer: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:3', unit),
cabinCrewFront: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:4', unit),
business1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:5', unit),
business1Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:6', unit),
business1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:7', unit),
business2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:8', unit),
business2Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:9', unit),
business2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:10', unit),
economy1Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:11', unit),
economy1Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:12', unit),
economy1Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:13', unit),
economy2Left: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:14', unit),
economy2Center: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:15', unit),
economy2Right: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:16', unit),
cabinCrewRear: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:17', unit),
forwardCargo: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:18', unit),
rearCargo: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:19', unit),
leftAuxPax: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:20', unit),
rightAuxPax: SimVar.GetSimVarValue('PAYLOAD STATION WEIGHT:21', unit),
paxCount: {
business1: 0,
business2: 0,
economy1: 0,
economy2: 0,
total: 0,
},
};
return payload;
},
setBaseWeight: (unit: 'kg' | 'lbs', isER: boolean) => {
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:1', unit, PaxConfig.weights.base[unit].pilot); // Pilot
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:2', unit, PaxConfig.weights.base[unit].firstOfficer); // First officer
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:3', unit, PaxConfig.weights.base[unit].engineer); // Engineer
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:4', unit, PaxConfig.weights.base[unit].cabinCrewFront); // Cabin Crew front
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:17', unit, PaxConfig.weights.base[unit].cabinCrewRear); // Cabin Crew rear
if (isER) {
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:20', unit, SharedConfig.erExtraWeight[unit]); // Forward Aux 1
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:21', unit, SharedConfig.erExtraWeight[unit]); // Forward Aux 2
}
},
setWeights: (payload: PayloadPax, unit: 'kg' | 'lbs') => {
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:4', unit, payload.cabinCrewFront); // Cabin Crew front
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:5', unit, payload.business1Left); // Business 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:6', unit, payload.business1Center); // Business 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:7', unit, payload.business1Right); // Business 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:8', unit, payload.business2Left); // Business 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:9', unit, payload.business2Center); // Business 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:10', unit, payload.business2Right); // Business 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:11', unit, payload.economy1Left); // Economy 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:12', unit, payload.economy1Center); // Economy 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:13', unit, payload.economy1Right); // Economy 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:14', unit, payload.economy2Left); // Economy 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:15', unit, payload.economy2Center); // Economy 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:16', unit, payload.economy2Right); // Economy 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:17', unit, payload.cabinCrewRear); //Cabin Crew rear
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:18', unit, payload.forwardCargo); // Forward Cargo
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:19', unit, payload.rearCargo); // Rear Cargo
},
setWeightsProgressive: (payload: PayloadPax, paxNum: number, cargoPercent: number, unit: 'kg' | 'lbs') => {
const business1Scalar = Math.min(1, paxNum / payload.paxCount.business1);
paxNum -= payload.paxCount.business1 * business1Scalar;
const business2Scalar = Math.min(1, paxNum / payload.paxCount.business2);
paxNum -= payload.paxCount.business2 * business2Scalar;
const economy1Scalar = Math.min(1, paxNum / payload.paxCount.economy1);
paxNum -= payload.paxCount.economy1 * economy1Scalar;
const economy2Scalar = Math.min(1, paxNum / payload.paxCount.economy2);
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:4', unit, payload.cabinCrewFront); // Cabin Crew front
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:5', unit, payload.business1Left * business1Scalar); // Business 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:6', unit, payload.business1Center * business1Scalar); // Business 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:7', unit, payload.business1Right * business1Scalar); // Business 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:8', unit, payload.business2Left * business2Scalar); // Business 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:9', unit, payload.business2Center * business2Scalar); // Business 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:10', unit, payload.business2Right * business2Scalar); // Business 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:11', unit, payload.economy1Left * economy1Scalar); // Economy 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:12', unit, payload.economy1Center * economy1Scalar); // Economy 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:13', unit, payload.economy1Right * economy1Scalar); // Economy 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:14', unit, payload.economy2Left * economy2Scalar); // Economy 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:15', unit, payload.economy2Center * economy2Scalar); // Economy 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:16', unit, payload.economy2Right * economy2Scalar); // Economy 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:17', unit, payload.cabinCrewRear); //Cabin Crew rear
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:18', unit, payload.forwardCargo * (cargoPercent / 100)); // Forward Cargo
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:19', unit, payload.rearCargo * (cargoPercent / 100)); // Rear Cargo
},
unload: (unit: 'kg' | 'lbs', isER: boolean) => {
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:1', unit, 0); // Pilot
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:2', unit, 0); // First officer
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:3', unit, 0); // Engineer
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:4', unit, 0); // Cabin Crew front
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:17', unit, 0); // Cabin Crew rear
if (!isER) {
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:20', unit, 0); // Forward Aux 1
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:21', unit, 0); // Forward Aux 2
}
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:4', unit, 0); // Cabin Crew front
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:5', unit, 0); // Business 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:6', unit, 0); // Business 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:7', unit, 0); // Business 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:8', unit, 0); // Business 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:9', unit, 0); // Business 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:10', unit, 0); // Business 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:11', unit, 0); // Economy 1L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:12', unit, 0); // Economy 1C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:13', unit, 0); // Economy 1R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:14', unit, 0); // Economy 2L
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:15', unit, 0); // Economy 2C
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:16', unit, 0); // Economy 2R
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:17', unit, 0); //Cabin Crew rear
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:18', unit, 0); // Forward Cargo
SimVar.SetSimVarValue('PAYLOAD STATION WEIGHT:19', unit, 0); // Rear Cargo
},
};
@@ -1,166 +0,0 @@
export interface Fuel {
main1: number;
main3: number;
main2: number;
upperAux: number;
lowerAux: number;
main1Tip: number;
main3Tip: number;
tail: number;
forwardAux1: number;
forwardAux2: number;
}
// TODO: Extract from CFG at runtime.
export const ArmsFuel = {
main1: -240,
main3: -240,
main2: 120,
upperAux: 0,
lowerAux: 0,
main1Tip: -468,
main3Tip: -468,
tail: -840,
forwardAux1: 60,
forwardAux2: 60,
};
// TODO: Extract following four from CFG at runtime
const rootChord = 34.68;
const wingSpan = 170.5;
const wingArea = 3648;
const quarterMAC = -165; //aero_center
const tipChord = (2 * wingArea) / wingSpan - rootChord;
const taperRatio = tipChord / rootChord;
const MAC = (2 / 3) * rootChord * ((1 + taperRatio + taperRatio ** 2) / (1 + taperRatio)) * 12;
const LEMAC = quarterMAC + (1 / 4) * MAC;
export const toPercentMAC = (positionInInches: number) => {
return ((positionInInches - LEMAC) / MAC) * -100;
};
export const SharedConfig = {
stationMax: {
//PMC pallet due to 104in door
forward: {
lbs: 6 * 15000,
kg: 6 * 6804,
},
//LD3s due to 70in door
rear: {
lbs: 14 * 3500,
kg: 14 * 1588,
},
},
maxTOW: {
er: {
lbs: 630500,
kg: 285990,
},
norm: {
lbs: 625500,
kg: 283722,
},
},
maxFuel: {
er: {
lbs: 282619,
kg: 128193,
},
norm: {
lbs: 256207,
kg: 116213,
},
},
erExtraWeight: {
lbs: 200,
kg: 91,
},
CGLimits: {
min: 12,
default: 20.5,
max: 34,
tolerance: 0.05,
},
};
export const initialPayload = {
empty: 0,
pilot: 0,
firstOfficer: 0,
engineer: 0,
cabinCrewFront: 0,
business1Left: 0,
business1Center: 0,
business1Right: 0,
business2Left: 0,
business2Center: 0,
business2Right: 0,
economy1Left: 0,
economy1Center: 0,
economy1Right: 0,
economy2Left: 0,
economy2Center: 0,
economy2Right: 0,
cabinCrewRear: 0,
forwardCargo: 0,
rearCargo: 0,
leftAuxPax: 0,
rightAuxPax: 0,
upper1Left: 0,
upper1Right: 0,
upper2Left: 0,
upper2Right: 0,
upper3Left: 0,
upper3Right: 0,
upper4Left: 0,
upper4Right: 0,
lowerForward: 0,
lowerRear: 0,
leftAuxF: 0,
rightAuxF: 0,
paxCount: {
business1: 0,
business2: 0,
economy1: 0,
economy2: 0,
total: 0,
},
};
export const initialFuel = {
main1: 0,
main3: 0,
main2: 0,
upperAux: 0,
lowerAux: 0,
main1Tip: 0,
main3Tip: 0,
tail: 0,
forwardAux1: 0,
forwardAux2: 0,
};
// SIM access
export const getFuel = (unit: 'kg' | 'lbs') => {
const conversion = SimVar.GetSimVarValue('FUEL WEIGHT PER GALLON', unit);
const fuel = {
main1: SimVar.GetSimVarValue('FUEL TANK LEFT MAIN QUANTITY', 'gal') * conversion,
main3: SimVar.GetSimVarValue('FUEL TANK RIGHT MAIN QUANTITY', 'gal') * conversion,
main2: SimVar.GetSimVarValue('FUEL TANK CENTER QUANTITY', 'gal') * conversion,
upperAux: SimVar.GetSimVarValue('FUEL TANK CENTER2 QUANTITY', 'gal') * conversion,
lowerAux: SimVar.GetSimVarValue('FUEL TANK CENTER3 QUANTITY', 'gal') * conversion,
main1Tip: SimVar.GetSimVarValue('FUEL TANK LEFT TIP QUANTITY', 'gal') * conversion,
main3Tip: SimVar.GetSimVarValue('FUEL TANK RIGHT TIP QUANTITY', 'gal') * conversion,
tail: SimVar.GetSimVarValue('FUEL TANK EXTERNAL1 QUANTITY', 'gal') * conversion,
forwardAux1: SimVar.GetSimVarValue('FUEL TANK LEFT AUX QUANTITY', 'gal') * conversion,
forwardAux2: SimVar.GetSimVarValue('FUEL TANK RIGHT AUX QUANTITY', 'gal') * conversion,
};
return fuel;
};
+3 -6
View File
@@ -1,6 +1,3 @@
export const COMMANDS = 'KHOFMANN_PDF_READER_COMMANDS'; export const COHERENT_COMM_BUS_WASM_CALL = 'COMM_BUS_WASM_CALLBACK';
export const DATA = 'KHOFMANN_PDF_READER_DATA';
export const LIST = 'LIST'; export const CG_ADJUST = 0.05;
export const LOAD = 'LOAD';
export const SAVE = 'SAVE';
export const MAX_LIST = 10;
@@ -1,15 +0,0 @@
@font-face {
font-family: 'Roboto';
font-style: normal;
font-display: swap;
font-weight: 300;
src: url(assets/fonts/Roboto-Light.ttf) format('truetype');
}
@font-face {
font-family: 'Roboto';
font-style: italic;
font-display: swap;
font-weight: 300;
src: url(assets/fonts/Roboto-LightItalic.ttf) format('truetype');
}
@@ -1,15 +0,0 @@
@font-face {
font-family: 'Roboto';
font-style: normal;
font-display: swap;
font-weight: 400;
src: url(assets/fonts/Roboto-Regular.ttf) format('truetype');
}
@font-face {
font-family: 'Roboto';
font-style: italic;
font-display: swap;
font-weight: 400;
src: url(assets/fonts/Roboto-Italic.ttf) format('truetype');
}
@@ -1,15 +0,0 @@
@font-face {
font-family: 'Roboto';
font-style: normal;
font-display: swap;
font-weight: 500;
src: url(assets/fonts/Roboto-Medium.ttf) format('truetype');
}
@font-face {
font-family: 'Roboto';
font-style: italic;
font-display: swap;
font-weight: 500;
src: url(assets/fonts/Roboto-MediumItalic.ttf) format('truetype');
}
@@ -1,15 +0,0 @@
@font-face {
font-family: 'Roboto';
font-style: normal;
font-display: swap;
font-weight: 700;
src: url(assets/fonts/Roboto-Bold.ttf) format('truetype');
}
@font-face {
font-family: 'Roboto';
font-style: italic;
font-display: swap;
font-weight: 700;
src: url(assets/fonts/Roboto-BoldItalic.ttf) format('truetype');
}
-42
View File
@@ -1,42 +0,0 @@
<!doctype html>
<html>
<!-- prettier-ignore -->
<head>
<title></title>
<meta charset="utf-8" />
<meta name="viewport" content="width=device-width, initial-scale=1.0" />
<link rel="stylesheet" href="/SCSS/common.css" />
<link rel="stylesheet" href="assets/efb.css" />
<link rel="stylesheet" href="index.css" />
<script type="text/javascript" src="/JS/coherent.js"></script>
<script type="text/javascript" src="/JS/common.js"></script>
<script type="text/javascript" src="/Pages/VCockpit/Instruments/Shared/BaseInstrument.js"></script>
<script type="text/javascript" src="/JS/dataStorage.js"></script>
<script type="text/javascript" src="/JS/buttons.js"></script>
<script type="text/javascript" src="/JS/Services/ToolBarPanels.js"></script>
<script type="text/javascript" src="/JS/simvar.js"></script>
<link rel="import" href="/templates/NewPushButton/NewPushButton.html" />
<link rel="import" href="/templates/ingameUi/ingameUi.html" />
<link rel="import" href="/templates/ingameUiHeader/ingameUiHeader.html" />
<link rel="import" href="/templates/virtualScroll/virtualScroll.html" />
</head>
<body class="border-box">
<tfdidesign-md11-load-manager-panel>
<ingame-ui
id="tfdidesign-md11-load-manager"
panel-id="TFDIDESIGN_MD11_LOAD_MANAGER_PANEL"
title="TFDi Design MD-11 Load Manager"
class="ingameUiFrame panelInvisible"
content-fit="true"
>
<virtual-scroll direction="y">
<div id="react" style="display: flex"></div>
</virtual-scroll>
</ingame-ui>
</tfdidesign-md11-load-manager-panel>
<script src="index.js" type="text/javascript"></script>
</body>
</html>
-32
View File
@@ -1,32 +0,0 @@
import { createElement } from 'react';
import { createRoot } from 'react-dom/client';
import App from './App';
class TFDiDesignMD11LoadManagerPanel extends TemplateElement {
private commBus: ViewListener.ViewListener | undefined;
constructor() {
super();
}
connectedCallback() {
super.connectedCallback();
this.commBus = RegisterViewListener('JS_LISTENER_COMM_BUS');
const container = document.getElementById('react');
if (container) {
const root = createRoot(container);
root.render(createElement(App, { commBus: this.commBus }));
}
}
disconnectedCallback() {
super.disconnectedCallback();
this.commBus?.unregister();
}
}
window.customElements.define('tfdidesign-md11-load-manager-panel', TFDiDesignMD11LoadManagerPanel);
checkAutoload();
@@ -0,0 +1,115 @@
interface WASMData {
GSX: GSX;
userData: UserData;
options: Options;
sbPlanned: {
ZFW: number;
GW: number;
fuel: number;
};
loaded: boolean;
}
export interface WASMDataPax extends WASMData {
livePayload: LivePayloadPax;
targetPayload: TargetPayloadPax;
limits: LimitsPax;
}
export interface WASMDataF extends WASMData {
livePayload: LivePayloadF;
targetPayload: TargetPayloadF;
limits: LimitsF;
}
interface TargetPayload {
CGTarget: number;
ZFWCG: number;
TOCG: number;
total: number;
fuel: number;
}
interface TargetPayloadPax extends TargetPayload {
empty: number;
crew: number;
business1: number;
business2: number;
economy1: number;
economy2: number;
forwardCargo: number;
rearCargo: number;
}
type LivePayloadPax = TargetPayloadPax;
interface TargetPayloadF extends TargetPayload {
empty: number;
crew: number;
upper1: number;
upper2: number;
upper3: number;
upper4: number;
lowerForward: number;
lowerRear: number;
}
type LivePayloadF = TargetPayloadF;
interface GSX {
couatlStarted: boolean;
loadingState: GSXLoadingState;
fuelingState: GSXFuelingState;
}
interface Limits {
minCG: number;
maxCG: number;
maxFuel: number;
maxTOW: number;
maxZFW: number;
minZFW: number;
}
interface LimitsPax extends Limits {
business1: number;
business2: number;
economy1: number;
economy2: number;
forwardCargo: number;
rearCargo: number;
}
interface LimitsF extends Limits {
upper1: number;
upper2: number;
upper3: number;
upper4: number;
lowerForward: number;
lowerRear: number;
}
interface UserData {
isCargo: boolean;
isER: boolean;
isImperial: boolean;
}
interface Options {
GSXSync: boolean;
paxWeight: number;
bagWeight: number;
}
export enum GSXLoadingState {
IDLE = 0,
BOARDING = 1,
BOARDED = 2,
DEBOARDING = 3,
DEBOARDED = 4,
}
export enum GSXFuelingState {
IDLE = 0,
FUELING = 1,
}
@@ -0,0 +1,29 @@
export type LoadingState = 'preview' | 'loaded';
export interface SimBrief {
plannedZFW: number;
plannedGW: number;
pax: number;
cargo: number;
fuel: number;
}
export enum CallMode {
SB_SET = 0,
ZFW_SET = 1,
STATION_SET = 2,
LOAD_SET = 3,
UNLOAD_SET = 4,
OPTIONS_SET = 5,
GSX_RESET = 6,
}
export enum CommBusCall {
TFDI_SIMBRIEF_USERNAME = 'requestSimBriefUsername',
}
export enum CommBusEvent {
TFDI_SIMBRIEF_USERNAME = 'receiveSimBriefUsername',
LIVE_DATA = 'khofmann_tfdi_md-11_load_manager_live_data',
UPDATE_TARGET = 'khofmann_tfdi_md-11_load_manager_update_target',
}
-10
View File
@@ -1,10 +0,0 @@
import '@mui/material';
declare module '@mui/material/styles' {
interface Theme {
screenHeight: number;
}
interface ThemeOptions {
screenHeight: number;
}
}
-11
View File
@@ -1,11 +0,0 @@
import { CSSProperties, DOMAttributes, ReactNode } from 'react';
type CustomElement<T> = Partial<T & DOMAttributes<T> & { children: ReactNode }>;
declare global {
namespace JSX {
interface IntrinsicElements {
['virtual-scroll']: CustomElement<{ class?: string; direction: 'x' | 'y'; style?: CSSProperties }>;
}
}
}
@@ -1,63 +1,41 @@
import { PaxConfig } from '../configs/pax'; import { SimBrief } from '../types/general';
import { SharedConfig } from '../configs/shared';
const getSimBriefFlightPlan = async (simBriefUsername: string) => { type Plan = {
const flightPlanURL = `https://www.simbrief.com/api/xml.fetcher.php?username=${simBriefUsername}&json=1`; params: {
let response: Response; units: 'kgs' | 'lbs';
let success = false; };
try { weights: {
response = await fetch(flightPlanURL); est_zfw: number;
success = true; est_ramp: number;
} catch (e: any) { pax_count_actual: number;
response = e.response; freight_added: number;
} };
return { fuel: {
success, plan_ramp: number;
data: await response.json(),
}; };
}; };
export const ImportFlightPlan = async ( export const ImportFlightPlanKH = (
username: string, plan: Plan,
config: typeof PaxConfig, maxZFW: number,
unit: 'kg' | 'lbs', maxTOW: number,
isER: boolean maxFuel: number,
isImperial: boolean
) => { ) => {
const flightPlan = await getSimBriefFlightPlan(username); if (!plan) return { type: 'error', message: 'Empty plan' };
if (!flightPlan.success) {
return {
type: 'error',
message: flightPlan.data.status,
};
}
const data = flightPlan.data;
if (!['MD11', 'MD1F'].includes(data.aircraft.icao_code)) {
return {
type: 'error',
message: `Your SimBrief plan is not for a MD-11`,
};
}
let convFactor = 1; let convFactor = 1;
if (data.params.units === 'kgs' && unit === 'lbs') convFactor = 2.20462262185; if (plan.params.units === 'kgs' && isImperial) convFactor = 2.20462262185;
if (data.params.units === 'lbs' && unit === 'kg') convFactor = 1 / 2.20462262185; if (plan.params.units === 'lbs' && !isImperial) convFactor = 1 / 2.20462262185;
return { return {
type: 'data', type: 'data',
message: { message: {
plannedZFW: Math.min(config.maxZWF[unit], Math.round(data.weights.est_zfw * convFactor)), plannedZFW: Math.min(maxZFW, Math.round(plan.weights.est_zfw * convFactor)),
plannedGW: Math.min( plannedGW: Math.min(maxTOW, Math.round(plan.weights.est_ramp * convFactor)),
isER ? SharedConfig.maxTOW.er[unit] : SharedConfig.maxTOW.norm[unit], pax: plan.weights.pax_count_actual,
Math.round(data.weights.est_ramp * convFactor) cargo: Math.round(plan.weights.freight_added * convFactor),
), fuel: Math.min(maxFuel, Math.round(plan.fuel.plan_ramp * convFactor)),
pax: data.weights.pax_count_actual, } as SimBrief,
cargo: Math.round(data.weights.freight_added * convFactor),
fuel: Math.min(
isER ? SharedConfig.maxFuel.er[unit] : SharedConfig.maxFuel.norm[unit],
Math.round(data.fuel.plan_ramp * convFactor)
),
},
}; };
}; };
+143
View File
@@ -0,0 +1,143 @@
import { COHERENT_COMM_BUS_WASM_CALL } from '../constants';
import { CallMode, CommBusEvent, SimBrief } from '../types/general';
export const loadAircraft = () => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.LOAD_SET,
})
);
};
export const unloadAircraft = () => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.UNLOAD_SET,
})
);
};
export const inRangeOf = (value: number, target: number, tolerance: number = 10) => {
return Math.abs(value - target) < tolerance;
};
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number, fuelTarget: number) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.ZFW_SET,
ZFWTarget: ZFWTarget,
CGTarget: CGTarget,
fuelTarget: fuelTarget,
})
);
};
export const CoherentCallStationEntryPax = (
business1: number,
business2: number,
economy1: number,
economy2: number,
forwardCargo: number,
rearCargo: number,
fuelTarget: number
) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.STATION_SET,
business1,
business2,
economy1,
economy2,
forwardCargo,
rearCargo,
fuelTarget,
})
);
};
export const CoherentCallStationEntryF = (
upper1: number,
upper2: number,
upper3: number,
upper4: number,
lowerForward: number,
lowerRear: number,
fuelTarget: number
) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.STATION_SET,
upper1,
upper2,
upper3,
upper4,
lowerForward,
lowerRear,
fuelTarget,
})
);
};
export const CoherentCallSBEntryPax = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.SB_SET,
cargo: SBPlan?.cargo,
numPax: SBPlan ? parseInt(SBPlan.pax as unknown as string) : undefined,
CGTarget: CGTarget,
plannedZFW: SBPlan?.plannedZFW,
plannedGW: SBPlan?.plannedGW,
fuel: fuel,
})
);
};
export const CoherentCallSBEntryF = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.SB_SET,
cargo: SBPlan?.cargo,
CGTarget: CGTarget,
plannedZFW: SBPlan?.plannedZFW,
plannedGW: SBPlan?.plannedGW,
fuel: SBPlan?.fuel,
})
);
};
export const CoherentCallOptionsSet = (GSXSync?: boolean, paxWeight?: number, bagWeight?: number) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.OPTIONS_SET,
GSXSync,
paxWeight,
bagWeight,
})
);
};
export const CoherentCallGSXReset = () => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
JSON.stringify({
mode: CallMode.GSX_RESET,
})
);
};
+3 -3
View File
@@ -12,7 +12,7 @@
// "disableReferencedProjectLoad": true, /* Reduce the number of projects loaded automatically by TypeScript. */ // "disableReferencedProjectLoad": true, /* Reduce the number of projects loaded automatically by TypeScript. */
/* Language and Environment */ /* Language and Environment */
"target": "es6", "target": "es2017",
/* Set the JavaScript language version for emitted JavaScript and include compatible library declarations. */ /* Set the JavaScript language version for emitted JavaScript and include compatible library declarations. */
"lib": ["es2017", "dom"], "lib": ["es2017", "dom"],
/* Specify a set of bundled library declaration files that describe the target runtime environment. */ /* Specify a set of bundled library declaration files that describe the target runtime environment. */
@@ -29,7 +29,7 @@
// "moduleDetection": "auto", /* Control what method is used to detect module-format JS files. */ // "moduleDetection": "auto", /* Control what method is used to detect module-format JS files. */
/* Modules */ /* Modules */
"module": "es6", "module": "es2015",
/* Specify what module code is generated. */ /* Specify what module code is generated. */
// "rootDir": "./", /* Specify the root folder within your source files. */ // "rootDir": "./", /* Specify the root folder within your source files. */
"moduleResolution": "node", "moduleResolution": "node",
@@ -65,7 +65,7 @@
// "sourceMap": true, /* Create source map files for emitted JavaScript files. */ // "sourceMap": true, /* Create source map files for emitted JavaScript files. */
// "inlineSourceMap": true, /* Include sourcemap files inside the emitted JavaScript. */ // "inlineSourceMap": true, /* Include sourcemap files inside the emitted JavaScript. */
// "outFile": "./", /* Specify a file that bundles all outputs into one JavaScript file. If 'declaration' is true, also designates a file that bundles all .d.ts output. */ // "outFile": "./", /* Specify a file that bundles all outputs into one JavaScript file. If 'declaration' is true, also designates a file that bundles all .d.ts output. */
"outDir": "../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel", // "outDir": "../html_ui/InGamePanels/tfdidesign-md11-load-manager-panel",
/* Specify an output folder for all emitted files. */ /* Specify an output folder for all emitted files. */
// "removeComments": true, /* Disable emitting comments. */ // "removeComments": true, /* Disable emitting comments. */
// "noEmit": true, /* Disable emitting files from a compilation. */ // "noEmit": true, /* Disable emitting files from a compilation. */
File diff suppressed because it is too large Load Diff
@@ -1,17 +0,0 @@
<SimBase.Document Type="InGamePanels" version="1,0">
<Filename>tfdidesign-md11-load-manager.spb</Filename>
<InGamePanels.InGamePanelDefinition
id="TFDIDESIGN_MD11_LOAD_MANAGER_PANEL"
Name="tfdidesign-md11-load-manager"
url="html_UI/InGamePanels/tfdidesign-md11-load-manager-panel/index.html"
resizeDirections="both"
minWidth="100"
minHeight="70"
defaultWidth="100"
defaultHeight="70"
defaultTop="10"
defaultLeft="10"
icon="ICON_TFDIDESIGN_MD11_LOAD_MANAGER"
buttonVisible="true">
</InGamePanels.InGamePanelDefinition>
</SimBase.Document>
@@ -0,0 +1,119 @@
#pragma once
#ifndef __INTELLISENSE__
#define MODULE_EXPORT __attribute__((visibility("default")))
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#else
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
// MSFS headers
#include <MSFS/MSFS_WindowsTypes.h>
#include <SimConnect.h>
// C headers
#include <math.h>
// C++ headers
#include <algorithm>
// Own headers
#include "fuel.h"
#include "log.h"
#include "shared.h"
/******************************** Constants ********************************/
// PMC pallet due to 104in door
#define MAX_UPPER_CARGO(IS_IMPERIAL) ((IS_IMPERIAL) ? (6.5 * 15000.0) : (6.5 * 6804.0))
// Max ZFW
#define MAX_F_ZFW(IS_IMPERIAL) ((IS_IMPERIAL) ? (451300) : (204706))
// Arms
#define ARM_F_UPPER1_LEFT 660
#define ARM_F_UPPER1_RIGHT 660
#define ARM_F_UPPER2_LEFT 240
#define ARM_F_UPPER2_RIGHT 240
#define ARM_F_UPPER3_LEFT -240
#define ARM_F_UPPER3_RIGHT -240
#define ARM_F_UPPER4_LEFT -600
#define ARM_F_UPPER4_RIGHT -600
/***************************** Data structures *****************************/
typedef struct {
// SimConnect mapped
double pilot;
double firstOfficer;
double engineer;
double upper1Left;
double upper1Right;
double upper2Left;
double upper2Right;
double upper3Left;
double upper3Right;
double upper4Left;
double upper4Right;
double lowerForward;
double lowerRear;
double leftAux;
double rightAux;
double _ZFWCG; // DO NOT USE
// Additional properties
double empty;
double total;
double CGTarget;
double ZFWCG;
double TOCG;
struct stations {
unsigned int upper1;
unsigned int upper2;
unsigned int upper3;
unsigned int upper4;
unsigned int total;
} stations;
struct sbPlanned {
double ZFW;
double GW;
double fuel;
unsigned int cargo;
} sbPlanned;
} fPayloadData_t;
typedef struct {
// SimConnect mapped
double pilot;
double firstOfficer;
double engineer;
double upper1Left;
double upper1Right;
double upper2Left;
double upper2Right;
double upper3Left;
double upper3Right;
double upper4Left;
double upper4Right;
double lowerForward;
double lowerRear;
double leftAux;
double rightAux;
double ZFWCG;
} fPayloadDataSet_t;
/******************************** Functions ********************************/
// ZFW Entry
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
const UserData_t *const userData);
// SimBrief Entry
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned int cargo,
const UserData_t *const userData);
// Updates pax stations with their respective weights
// Used internally and used for Station Entry (pax only, cargo is ste directly)
// STATION WEIGHTS ARE NOT NORMALISED TO POUNDS
void generatePayload(fPayloadData_t *const targetPayload);
// Normalise to Pounds
// For Station Entry: CALL AFTER `generatePayload`
void normalisePayload(fPayloadData_t *const targetPayload, const bool isImperial);
void calculateCGs(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial);
void load(const fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
const bool isImperial);
void unloadF(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER);
+94
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#pragma once
#ifndef __INTELLISENSE__
#define MODULE_EXPORT __attribute__((visibility("default")))
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#else
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
// MSFS headers
#include <MSFS/MSFS_WindowsTypes.h>
#include <SimConnect.h>
// C headers
#include <math.h>
// C++ headers
#include <algorithm>
// Own headers
#include "shared.h"
/******************************** Constants ********************************/
// Pounds to gallons conversion
#define LBS_PER_GAL 6.699999809
// Fueling rate
#define FUELING_RATE ((LBS_PER_GAL * 1000) / 60)
// Max tank capacity gallons
#define MAX_TANK_1_3_MAIN_GAL 5167.907
#define MAX_TANK_1_3_TIP_GAL 874.5
#define MAX_TANK_1_3_GAL (5167.907 + 874.5)
#define MAX_TANK_2_GAL 9556.95
#define MAX_UPR_AUX_GAL 12998.58
#define MAX_LWR_AUX_GAL 1641.82
#define MAX_TAIL_GAL 1957.779
#define MAX_FWD_AUX_GAL 1970.8
// Max tank capacity pounds
#define MAX_TANK_1_3_MAIN_LBS (LBS_PER_GAL * MAX_TANK_1_3_MAIN_GAL)
#define MAX_TANK_1_3_TIP_LBS (LBS_PER_GAL * MAX_TANK_1_3_TIP_GAL)
#define MAX_TANK_1_3_LBS (LBS_PER_GAL * MAX_TANK_1_3_GAL)
#define MAX_TANK_2_LBS (LBS_PER_GAL * MAX_TANK_2_GAL)
#define MAX_UPR_AUX_LBS (LBS_PER_GAL * MAX_UPR_AUX_GAL)
#define MAX_LWR_AUX_LBS (LBS_PER_GAL * MAX_LWR_AUX_GAL)
#define MAX_TAIL_LBS (LBS_PER_GAL * MAX_TAIL_GAL)
#define MAX_FWD_AUX_LBS (LBS_PER_GAL * MAX_FWD_AUX_GAL)
// Max Fuel
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
// Arms Fuel
#define ARM_MAIN1 -240.0
#define ARM_MAIN3 -240.0
#define ARM_MAIN2 120.0
#define ARM_UPPER_AUX 0.0
#define ARM_LOWER_AUX 0.0
#define ARM_MAIN1_TIP -468.0
#define ARM_MAIN3_TIP -468.0
#define ARM_TAIL -840.0
#define ARM_FORWARD_AUX1 60.0
#define ARM_FORWARD_AUX2 60.0
/***************************** Data structures *****************************/
typedef struct {
// SimConnect mapped
double main1;
double main3;
double main2;
double upperAux;
double lowerAux;
double main1Tip;
double main3Tip;
double tail;
double forwardAux1;
double forwardAux2;
// Additional properties
double total;
} FuelData_t;
typedef struct {
double main1;
double main3;
double main2;
double upperAux;
double lowerAux;
double tail;
double forwardAux1;
double forwardAux2;
} FuelDataSet_t;
/******************************** Functions ********************************/
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const bool isImperial, const bool isER);
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const UserData_t *const userData);
void fuel(const FuelData_t *const targetFuel, const HANDLE simConnect);
@@ -0,0 +1,43 @@
#pragma once
#ifndef __INTELLISENSE__
#define MODULE_EXPORT __attribute__((visibility("default")))
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#else
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
// MSFS headers
#include "rapidjson/filewritestream.h"
#include <MSFS/MSFS.h>
#include <MSFS/MSFS_CommBus.h>
#include <MSFS/MSFS_Core.h>
#include <MSFS/MSFS_GaugeContext.h>
#include <MSFS/MSFS_WindowsTypes.h>
#include <SimConnect.h>
#include <rapidjson/document.h>
#include <rapidjson/filereadstream.h>
#include <rapidjson/writer.h>
// Own headers
#include "freighter.h"
#include "fuel.h"
#include "log.h"
#include "pax.h"
#include "shared.h"
/******************************** Constants ********************************/
// Module identification
// COMM BUS
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
/******************************** Functions ********************************/
void commBusUpdateTargetCallback(const char *args, unsigned int size, void *ctx);
int receiveData(const char *buf);
void sendData();
void CALLBACK MyDispatchProc(SIMCONNECT_RECV *pData, DWORD cbData, void *pContext);
+25
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#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);
+156
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#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);
+131
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#pragma once
#ifndef __INTELLISENSE__
#define MODULE_EXPORT __attribute__((visibility("default")))
#define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#else
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/******************************** Constants ********************************/
// 190lbs default
#define PILOT_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (190.0) : (86.0))
// 200lbs per tank (one LD3)
#define AUX_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (200.0) : (91.0))
// PMC pallet due to 104in door
#define MAX_FRONT_CARGO(IS_IMPERIAL) ((IS_IMPERIAL) ? (6.0 * 15000.0) : (6.0 * 6804.0))
// LD3s due to 70in door, ER option takes up two slots
#define MAX_REAR_CARGO(IS_IMPERIAL, IS_ER) ((IS_IMPERIAL) ? ((IS_ER ? 12.0 : 14.0) * 3500.0) : ((IS_ER ? 12.0 : 14.0) * 1588.0))
// Max TOW
#define MAX_TOW(IS_IMPERIAL) ((IS_IMPERIAL) ? (625500) : (283722))
#define MAX_TOW_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (630500) : (285990))
// Arms Shared
#define ARM_EMPTY -120.0
#define ARM_PILOT 984.0
#define ARM_FIRST_OFFICER 984.0
#define ARM_ENGINEER 960.0
#define ARM_FORWARD_CARGO 360.0
#define ARM_REAR_CARGO -360.0
#define ARM_LEFT_AUX 60.0
#define ARM_RIGHT_AUX 60.0
// MAC
#define ROOT_CHORD 34.68
#define WING_SPAN 170.5
#define WING_AREA 3648.0
#define QUARTER_MAC -165.0 // aero_center
#define TIP_CHORD ((2.0 * WING_AREA) / WING_SPAN - ROOT_CHORD)
#define TAPER_RATIO (TIP_CHORD / ROOT_CHORD)
#define MAC ((2.0 / 3.0) * ROOT_CHORD * ((1.0 + TAPER_RATIO + (TAPER_RATIO * TAPER_RATIO)) / (1.0 + TAPER_RATIO)) * 12.0)
#define LEMAC (QUARTER_MAC + (1.0 / 4.0) * MAC)
// CG Limits
#define MIN_CG 12.0
#define MAX_CG 34.0
#define CG_TOLERANCE 0.05
// GSX States
#define GSX_SERVICE_IDLE 1
#define GSX_SERVICE_CALLED 4
#define GSX_SERVICE_ACTIVE 5
#define GSX_SERVICE_FINISHED 6
/********************************* Macros **********************************/
// Conversions
#define TO_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE)*2.20462262185)
#define FROM_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE) * (1.0 / 2.20462262185))
// MAC
#define TO_PERCENT_MAC(POS) ((((POS)-LEMAC) / MAC) * -100.0)
/********************************** ENUMS **********************************/
enum DATA_DEFINITIONS {
DATA_DEFINITION_EMPTY_WEIGHT,
DATA_DEFINITION_PAYLOAD_PAX,
DATA_DEFINITION_PAYLOAD_F,
DATA_DEFINITION_FUEL,
DATA_DEFINITION_FUEL_SET,
DATA_DEFINITION_GSX,
DATA_DEFINITION_USER_DATA,
};
enum DATA_REQUESTS {
DATA_REQUEST_EMPTY_WEIGHT,
DATA_REQUEST_PAYLOAD_PAX,
DATA_REQUEST_PAYLOAD_F,
DATA_REQUEST_FUEL,
DATA_REQUEST_FUEL_SET,
DATA_REQUEST_GSX,
DATA_REQUEST_USER_DATA,
};
enum LOADING_STATES {
LOADING_STATE_IDLE,
LOADING_STATE_BOARDING,
LOADING_STATE_BOARDED,
LOADING_STATE_DEBOARDING,
LOADING_STATE_DEBOARDED,
};
enum FUELING_STATES { FUELING_STATE_IDLE, FUELING_STATE_CALLED, FUELING_STATE_FUELING, FUELING_STATE_FUELED };
enum CALL_MODES {
CALL_MODE_SB_SET,
CALL_MODE_ZFW_SET,
CALL_MODE_STATION_SET,
CALL_MODE_LOAD_SET,
CALL_MODE_UNLOAD_SET,
CALL_MODE_OPTIONS_SET,
CALL_MODE_GSX_RESET,
};
/***************************** Data structures *****************************/
typedef struct {
double isCargo;
double isER;
double isImperial;
} UserData_t;
typedef struct {
// SimConnect mapped
double couatlStarted; // boolean
double boardingState; // See manual, 5 => active
double deboardingState; // See manual, 5 => active
double refuelingState; // See manual, 5 => active
double passengersBoarded; // Num pax
double passengersDeboarded; // Num pax
double cargoBoarded; // In percent
double cargoDeboarded; // In percent
double fuelConnected; // boolean
// Additional properties
enum LOADING_STATES loadingState;
enum FUELING_STATES fuelingState;
} GSXData_t;
typedef struct {
bool GSXSync;
double paxWeightKG;
double bagWeightKG;
double paxWeightLBS;
double bagWeightLBS;
} UserOptions_t;
@@ -0,0 +1,25 @@

Microsoft Visual Studio Solution File, Format Version 12.00
# Visual Studio Version 17
VisualStudioVersion = 17.13.36105.23
MinimumVisualStudioVersion = 10.0.40219.1
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager", "load-manager.vcxproj", "{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}"
EndProject
Global
GlobalSection(SolutionConfigurationPlatforms) = preSolution
Debug|MSFS = Debug|MSFS
Release|MSFS = Release|MSFS
EndGlobalSection
GlobalSection(ProjectConfigurationPlatforms) = postSolution
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|MSFS.ActiveCfg = Debug|MSFS
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Debug|MSFS.Build.0 = Debug|MSFS
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.ActiveCfg = Release|MSFS
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.Build.0 = Release|MSFS
EndGlobalSection
GlobalSection(SolutionProperties) = preSolution
HideSolutionNode = FALSE
EndGlobalSection
GlobalSection(ExtensibilityGlobals) = postSolution
SolutionGuid = {835CA9EE-0C67-4B32-B910-3F3A40943047}
EndGlobalSection
EndGlobal
@@ -0,0 +1,4 @@
<?xml version="1.0" encoding="utf-8"?>
<Project ToolsVersion="Current" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
<PropertyGroup />
</Project>
@@ -0,0 +1,174 @@
<?xml version="1.0" encoding="utf-8"?>
<Project DefaultTargets="Build" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
<ItemGroup Label="ProjectConfigurations">
<ProjectConfiguration Include="Debug|MSFS">
<Configuration>Debug</Configuration>
<Platform>MSFS</Platform>
</ProjectConfiguration>
<ProjectConfiguration Include="Release|MSFS">
<Configuration>Release</Configuration>
<Platform>MSFS</Platform>
</ProjectConfiguration>
</ItemGroup>
<PropertyGroup Label="Globals">
<VCProjectVersion>16.0</VCProjectVersion>
<ProjectGuid>{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}</ProjectGuid>
<RootNamespace>Module</RootNamespace>
<WindowsTargetPlatformVersion>10.0</WindowsTargetPlatformVersion>
<ProjectName>load-manager</ProjectName>
</PropertyGroup>
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.Default.props" />
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="Configuration">
<ConfigurationType>Application</ConfigurationType>
<UseDebugLibraries>true</UseDebugLibraries>
<PlatformToolset>MSFS2024</PlatformToolset>
<CharacterSet>MultiByte</CharacterSet>
</PropertyGroup>
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="Configuration">
<ConfigurationType>Application</ConfigurationType>
<UseDebugLibraries>false</UseDebugLibraries>
<PlatformToolset>MSFS2024</PlatformToolset>
<WholeProgramOptimization>true</WholeProgramOptimization>
<CharacterSet>MultiByte</CharacterSet>
</PropertyGroup>
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.props" />
<ImportGroup Label="ExtensionSettings">
</ImportGroup>
<ImportGroup Label="Shared">
</ImportGroup>
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'" Label="PropertySheets">
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
</ImportGroup>
<ImportGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'" Label="PropertySheets">
<Import Project="$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props" Condition="exists('$(UserRootDir)\Microsoft.Cpp.$(Platform).user.props')" Label="LocalAppDataPlatform" />
</ImportGroup>
<PropertyGroup Label="UserMacros" />
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
<TargetExt>.wasm</TargetExt>
<GenerateManifest />
<LinkIncremental />
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
<TargetName>$(ProjectName)</TargetName>
</PropertyGroup>
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
<TargetExt>.wasm</TargetExt>
<IncludePath>$(MSFS_IncludePath);$(ProjectDir)include</IncludePath>
</PropertyGroup>
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Debug|MSFS'">
<ClCompile>
<WarningLevel>Level3</WarningLevel>
<Optimization>Disabled</Optimization>
<SDLCheck>
</SDLCheck>
<ConformanceMode>true</ConformanceMode>
<BufferSecurityCheck>false</BufferSecurityCheck>
<AdditionalIncludeDirectories>
</AdditionalIncludeDirectories>
<PreprocessorDefinitions>__wasi__;_STRING_H_CPLUSPLUS_98_CONFORMANCE_;_WCHAR_H_CPLUSPLUS_98_CONFORMANCE_;_LIBCPP_HAS_NO_THREADS;_WINDLL;%(PreprocessorDefinitions)</PreprocessorDefinitions>
<ShowIncludes>false</ShowIncludes>
<ExceptionHandling>false</ExceptionHandling>
<RuntimeTypeInfo>
</RuntimeTypeInfo>
<SupportJustMyCode>
</SupportJustMyCode>
<DebugInformationFormat>ProgramDatabase</DebugInformationFormat>
<BasicRuntimeChecks>
</BasicRuntimeChecks>
<LanguageStandard>stdcpp14</LanguageStandard>
<MultiProcessorCompilation>true</MultiProcessorCompilation>
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
</ClCompile>
<Link>
<SubSystem>
</SubSystem>
<AdditionalDependencies>
</AdditionalDependencies>
<IgnoreAllDefaultLibraries>
</IgnoreAllDefaultLibraries>
<NoEntryPoint>true</NoEntryPoint>
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
<RandomizedBaseAddress>
</RandomizedBaseAddress>
<DataExecutionPrevention>
</DataExecutionPrevention>
<GenerateDebugInformation>true</GenerateDebugInformation>
<ProgramDatabaseFile>
</ProgramDatabaseFile>
<ImportLibrary>
</ImportLibrary>
<ProfileGuidedDatabase>
</ProfileGuidedDatabase>
<AdditionalLibraryDirectories>
</AdditionalLibraryDirectories>
</Link>
<PostBuildEvent>
<Command>cd $(SolutionDir)..\..\
Powershell.exe -File .\copy-debug.ps1</Command>
</PostBuildEvent>
</ItemDefinitionGroup>
<ItemDefinitionGroup Condition="'$(Configuration)|$(Platform)'=='Release|MSFS'">
<ClCompile>
<WarningLevel>Level3</WarningLevel>
<Optimization>MaxSpeed</Optimization>
<FunctionLevelLinking>true</FunctionLevelLinking>
<IntrinsicFunctions>true</IntrinsicFunctions>
<SDLCheck>true</SDLCheck>
<ConformanceMode>true</ConformanceMode>
<AdditionalIncludeDirectories>
</AdditionalIncludeDirectories>
<PreprocessorDefinitions>__wasi__;__wasm32__;_STRING_H_CPLUSPLUS_98_CONFORMANCE_;_WCHAR_H_CPLUSPLUS_98_CONFORMANCE_;_LIBCPP_NO_EXCEPTIONS;_LIBCPP_HAS_NO_THREADS;_LIBCPP_STD_VER=14;_WINDLL;%(PreprocessorDefinitions)</PreprocessorDefinitions>
<BufferSecurityCheck>false</BufferSecurityCheck>
<ExceptionHandling>false</ExceptionHandling>
<DebugInformationFormat>false</DebugInformationFormat>
<SupportJustMyCode>
</SupportJustMyCode>
<LanguageStandard>stdcpp14</LanguageStandard>
<AdditionalOptions>/clang:-Wall /clang:-Wextra /clang:-pedantic /clang:-Wno-missing-braces
/clang:-Wno-unused-const-variable /clang:-fstack-usage %(AdditionalOptions)</AdditionalOptions>
</ClCompile>
<Link>
<SubSystem>
</SubSystem>
<AdditionalDependencies>%(AdditionalDependencies)</AdditionalDependencies>
<IgnoreAllDefaultLibraries>
</IgnoreAllDefaultLibraries>
<NoEntryPoint>true</NoEntryPoint>
<OutputFile>$(OutDir)$(TargetName)$(TargetExt)</OutputFile>
<RandomizedBaseAddress>
</RandomizedBaseAddress>
<DataExecutionPrevention>
</DataExecutionPrevention>
<GenerateDebugInformation>false</GenerateDebugInformation>
<ProgramDatabaseFile>
</ProgramDatabaseFile>
<ImportLibrary>
</ImportLibrary>
<ProfileGuidedDatabase>
</ProfileGuidedDatabase>
<AdditionalLibraryDirectories>$(OutDir)</AdditionalLibraryDirectories>
</Link>
<PostBuildEvent>
<Command>cd $(SolutionDir)..\..\
Powershell.exe -File .\copy-release.ps1</Command>
</PostBuildEvent>
</ItemDefinitionGroup>
<ItemGroup>
<ClCompile Include="src/freighter.cpp" />
<ClCompile Include="src/load-manager.cpp" />
<ClCompile Include="src/log.cpp" />
<ClCompile Include="src/pax.cpp" />
<ClCompile Include="src/fuel.cpp" />
</ItemGroup>
<ItemGroup>
<ClInclude Include="include/freighter.h" />
<ClInclude Include="include/load-manager.h" />
<ClInclude Include="include/log.h" />
<ClInclude Include="include/pax.h" />
<ClInclude Include="include/shared.h" />
<ClInclude Include="include/fuel.h" />
</ItemGroup>
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
<ImportGroup Label="ExtensionTargets">
</ImportGroup>
</Project>
@@ -0,0 +1,50 @@
<?xml version="1.0" encoding="utf-8"?>
<Project ToolsVersion="4.0" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
<ItemGroup>
<ClCompile Include="src/freighter.cpp">
<Filter>Source Files</Filter>
</ClCompile>
<ClCompile Include="src/load-manager.cpp">
<Filter>Source Files</Filter>
</ClCompile>
<ClCompile Include="src/log.cpp">
<Filter>Source Files</Filter>
</ClCompile>
<ClCompile Include="src/pax.cpp">
<Filter>Source Files</Filter>
</ClCompile>
<ClCompile Include="src/fuel.cpp">
<Filter>Source Files</Filter>
</ClCompile>
</ItemGroup>
<ItemGroup>
<ClInclude Include="include/freighter.h">
<Filter>Header Files</Filter>
</ClInclude>
<ClInclude Include="include/load-manager.h">
<Filter>Header Files</Filter>
</ClInclude>
<ClInclude Include="include/log.h">
<Filter>Header Files</Filter>
</ClInclude>
<ClInclude Include="include/pax.h">
<Filter>Header Files</Filter>
</ClInclude>
<ClInclude Include="include/shared.h">
<Filter>Header Files</Filter>
</ClInclude>
<ClInclude Include="include/fuel.h">
<Filter>Header Files</Filter>
</ClInclude>
</ItemGroup>
<ItemGroup>
<Filter Include="Header Files">
<UniqueIdentifier>{93995380-89BD-4b04-88EB-625FBE52EBFB}</UniqueIdentifier>
<Extensions>h;hh;hpp;hxx;h++;hm;inl;inc;ipp;xsd</Extensions>
</Filter>
<Filter Include="Source Files">
<UniqueIdentifier>{4FC737F1-C7A5-4376-A066-2A32D752A2FF}</UniqueIdentifier>
<Extensions>cpp;c;cc;cxx;c++;cppm;ixx;def;odl;idl;hpj;bat;asm;asmx</Extensions>
</Filter>
</ItemGroup>
</Project>
@@ -0,0 +1,4 @@
<?xml version="1.0" encoding="utf-8"?>
<Project ToolsVersion="Current" xmlns="http://schemas.microsoft.com/developer/msbuild/2003">
<PropertyGroup />
</Project>
+15
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@@ -0,0 +1,15 @@
{
"name": "wasm-module",
"version": "0.0.16",
"description": "Load Manager WASM module",
"scripts": {
"clean": "rimraf ../SimObjects/Airplanes/TFDi_Design_MD-11/panel/load-manager.wasm && rimraf MSFS",
"build": "MSBuild.exe ./load-manager.sln /p:Platform=MSFS",
"build:rel": "MSBuild.exe ./load-manager.sln /p:Platform=MSFS /p:Configuration=Release",
"release": "pnpm clean && npm version patch && pnpm build:rel && node stack-analysis"
},
"keywords": [],
"author": "Kilian Kurt Hofmann",
"license": "MIT",
"packageManager": "pnpm@10.25.0"
}
@@ -0,0 +1,307 @@
#include "freighter.h"
// ZFW Entry
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const double ZFWTarget,
const UserData_t *const userData) {
// Find payload, num pax and extra cargo
double payload = ZFWTarget - targetPayload->empty - targetPayload->pilot - targetPayload->firstOfficer -
targetPayload->engineer - targetPayload->leftAux - targetPayload->rightAux;
unsigned int cargo = round(payload);
distribute(targetPayload, fuel, cargo, userData);
}
// SimBrief Entry
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned int cargo,
const UserData_t *const userData) {
// Clear
targetPayload->stations.upper1 = targetPayload->stations.upper2 = targetPayload->stations.upper3 =
targetPayload->stations.upper4 = targetPayload->stations.total = 0;
targetPayload->lowerForward = targetPayload->lowerRear = 0;
unsigned short _cargo = 0;
unsigned int count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
MAX_REAR_CARGO(userData->isImperial, userData->isER);
// Initial distribution
while (cargo > 0 && count > 0) {
if (cargo >= 6) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
_cargo++;
}
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
_cargo++;
}
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper4++;
_cargo++;
}
if (targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
targetPayload->lowerForward++;
_cargo++;
}
if (targetPayload->lowerRear < MAX_REAR_CARGO(userData->isImperial, userData->isER)) {
targetPayload->lowerRear++;
_cargo++;
}
} else if (cargo == 5) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
_cargo++;
}
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
_cargo++;
}
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper4++;
_cargo++;
}
if (targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
targetPayload->lowerForward++;
_cargo++;
}
} else if (cargo == 4) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
_cargo++;
}
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
_cargo++;
}
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper4++;
_cargo++;
}
} else if (cargo == 3) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
_cargo++;
}
if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
_cargo++;
}
} else if (cargo == 2) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
_cargo++;
}
} else if (cargo == 1) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
}
}
cargo -= _cargo;
targetPayload->stations.total += _cargo;
_cargo = 0;
count--;
}
// Refinement
count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
MAX_REAR_CARGO(userData->isImperial, userData->isER);
while (count > 0) {
generatePayload(targetPayload);
calculateCGs(targetPayload, fuel, userData->isImperial);
// in front of target
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
if (targetPayload->stations.upper1 > 0) {
targetPayload->stations.upper1--;
} else if (targetPayload->stations.upper2 > 0) {
targetPayload->stations.upper2--;
} else if (targetPayload->stations.upper3 > 0) {
targetPayload->stations.upper3--;
} else {
break;
}
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper4++;
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
} else {
targetPayload->stations.upper1++;
}
}
// behind target
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
if (targetPayload->stations.upper4 > 0) {
targetPayload->stations.upper4--;
} else if (targetPayload->stations.upper3 > 0) {
targetPayload->stations.upper3--;
} else if (targetPayload->stations.upper2 > 0) {
targetPayload->stations.upper2--;
} else {
break;
}
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
} else {
targetPayload->stations.upper4++;
}
} else {
break;
}
count--;
}
// Refinement cargo
count = MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
while (count > 0) {
generatePayload(targetPayload);
calculateCGs(targetPayload, fuel, userData->isImperial);
// in front of target
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
if (targetPayload->lowerForward > 0 && targetPayload->lowerRear < MAX_REAR_CARGO(userData->isImperial, userData->isER)) {
targetPayload->lowerForward--;
targetPayload->lowerRear++;
} else {
break;
}
}
// behind target
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
if (targetPayload->lowerRear > 0 && targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
targetPayload->lowerRear--;
targetPayload->lowerForward++;
} else {
break;
}
} else {
break;
}
count--;
}
}
// Updates pax stations with their respective weights
// Used internally and used for Station Entry (pax only, cargo is set directly)
void generatePayload(fPayloadData_t *const targetPayload) {
targetPayload->upper1Left = targetPayload->upper1Right = (targetPayload->stations.upper1 / 2.0);
targetPayload->upper2Left = targetPayload->upper2Right = (targetPayload->stations.upper2 / 2.0);
targetPayload->upper3Left = targetPayload->upper3Right = (targetPayload->stations.upper3 / 2.0);
targetPayload->upper4Left = targetPayload->upper4Right = (targetPayload->stations.upper4 / 2.0);
targetPayload->total = targetPayload->empty + targetPayload->pilot + targetPayload->firstOfficer + targetPayload->engineer +
targetPayload->upper1Left + targetPayload->upper1Right + targetPayload->upper2Left +
targetPayload->upper2Right + targetPayload->upper3Left + targetPayload->upper3Right +
targetPayload->upper4Left + targetPayload->upper4Right + targetPayload->lowerForward +
targetPayload->lowerRear + targetPayload->leftAux + targetPayload->rightAux;
}
// Normalise to Pounds
// MANDATORY BEFORE SETTING WEIGHTS
// USE ON COPY OF GLOBAL STATE ONLY
void normalisePayload(fPayloadData_t *const targetPayload, const bool isImperial) {
targetPayload->empty = TO_POUNDS(isImperial, targetPayload->empty);
targetPayload->pilot = TO_POUNDS(isImperial, targetPayload->pilot);
targetPayload->firstOfficer = TO_POUNDS(isImperial, targetPayload->firstOfficer);
targetPayload->engineer = TO_POUNDS(isImperial, targetPayload->engineer);
targetPayload->upper1Left = TO_POUNDS(isImperial, targetPayload->upper1Left);
targetPayload->upper1Right = TO_POUNDS(isImperial, targetPayload->upper1Right);
targetPayload->upper2Left = TO_POUNDS(isImperial, targetPayload->upper2Left);
targetPayload->upper2Right = TO_POUNDS(isImperial, targetPayload->upper2Right);
targetPayload->upper3Left = TO_POUNDS(isImperial, targetPayload->upper3Left);
targetPayload->upper3Right = TO_POUNDS(isImperial, targetPayload->upper3Right);
targetPayload->upper4Left = TO_POUNDS(isImperial, targetPayload->upper4Left);
targetPayload->upper4Right = TO_POUNDS(isImperial, targetPayload->upper4Right);
targetPayload->lowerForward = TO_POUNDS(isImperial, targetPayload->lowerForward);
targetPayload->lowerRear = TO_POUNDS(isImperial, targetPayload->lowerRear);
targetPayload->leftAux = TO_POUNDS(isImperial, targetPayload->leftAux);
targetPayload->rightAux = TO_POUNDS(isImperial, targetPayload->rightAux);
}
void calculateCGs(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const bool isImperial) {
fPayloadData_t localPayload = {};
memcpy(&localPayload, targetPayload, sizeof(localPayload));
normalisePayload(&localPayload, isImperial);
double totalMoment = localPayload.empty * ARM_EMPTY + localPayload.pilot * ARM_PILOT +
localPayload.firstOfficer * ARM_FIRST_OFFICER + localPayload.engineer * ARM_ENGINEER +
localPayload.upper1Left * ARM_F_UPPER1_LEFT + localPayload.upper1Right * ARM_F_UPPER1_RIGHT +
localPayload.upper2Left * ARM_F_UPPER2_LEFT + localPayload.upper2Right * ARM_F_UPPER2_RIGHT +
localPayload.upper3Left * ARM_F_UPPER3_LEFT + localPayload.upper3Right * ARM_F_UPPER3_RIGHT +
localPayload.upper4Left * ARM_F_UPPER4_LEFT + localPayload.upper4Right * ARM_F_UPPER4_RIGHT +
localPayload.lowerForward * ARM_FORWARD_CARGO + localPayload.lowerRear * ARM_REAR_CARGO +
localPayload.leftAux * ARM_LEFT_AUX + localPayload.rightAux * ARM_RIGHT_AUX;
double totalWeight = localPayload.empty + localPayload.pilot + localPayload.firstOfficer + localPayload.engineer +
localPayload.upper1Left + localPayload.upper1Right + localPayload.upper2Left + localPayload.upper2Right +
localPayload.upper3Left + localPayload.upper3Right + localPayload.upper4Left + localPayload.upper4Right +
localPayload.lowerForward + localPayload.lowerRear + localPayload.leftAux + localPayload.rightAux;
targetPayload->ZFWCG = TO_PERCENT_MAC(totalMoment / totalWeight);
totalMoment += fuel->main1 * ARM_MAIN1 + fuel->main3 * ARM_MAIN3 + fuel->main2 * ARM_MAIN2 + fuel->upperAux * ARM_UPPER_AUX +
fuel->lowerAux * ARM_LOWER_AUX + fuel->main1Tip * ARM_MAIN1_TIP + fuel->main3Tip * ARM_MAIN3_TIP +
fuel->tail * ARM_TAIL + fuel->forwardAux1 * ARM_FORWARD_AUX1 + fuel->forwardAux2 * ARM_FORWARD_AUX2;
totalWeight += fuel->total;
targetPayload->TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
}
void load(const fPayloadData_t *const targetPayload, const FuelData_t *const fuel, const HANDLE simConnect,
const bool isImperial) {
fPayloadData_t localPayload = {};
memcpy(&localPayload, targetPayload, sizeof(localPayload));
normalisePayload(&localPayload, isImperial);
calculateCGs(&localPayload, fuel, isImperial);
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
sizeof(fPayloadDataSet_t), &localPayload);
}
void unloadF(const HANDLE simConnect, const FuelData_t *const fuel, const double empty, const bool isER) {
fPayloadData_t localPayload = {};
localPayload.empty = empty;
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
calculateCGs(&localPayload, fuel, true);
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
toLog(stdout, "Payload set with ZFWCG: %f.\n", &localPayload.ZFWCG);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER_AIRCRAFT, 0, 0,
sizeof(fPayloadDataSet_t), &localPayload);
}
+138
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#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
+49
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#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);
}
+333
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@@ -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);
});
+7 -1
View File
@@ -1,6 +1,12 @@
# How to build
Build WASM module from VS
`pnpm build` from `js-bundle`
Build in sim
# Sources # Sources
- https://www.boeing.com/content/dam/boeing/boeingdotcom/company/about_bca/startup/pdf/freighters/MD11BCF.pdf - https://www.boeing.com/content/dam/boeing/boeingdotcom/company/about_bca/startup/pdf/freighters/MD11BCF.pdf
- LAMM - LAMM
- https://www.satco-inc.com/product-pallet/?part_number=31086-595 - https://www.satco-inc.com/product-pallet/?part_number=31086-595
- https://www.satco-inc.com/product-container/?part_number=34124-901 - https://www.satco-inc.com/product-container/?part_number=34124-901
View File
+1
View File
@@ -0,0 +1 @@
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
+1
View File
@@ -0,0 +1 @@
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
+40
View File
@@ -0,0 +1,40 @@
const { applyPatch } = require('diff');
const fs = require('fs');
const readline = require('readline');
const outPath = './PackageSources/html_ui/Pages/VCockpit/Instruments/aircraft_efb/KH_TFDi_MD11_efb';
let file1Contents = fs.readFileSync('./EFB/efb.js').toString();
let patch = fs.readFileSync('./EFB/efb-js.patch').toString();
let patchedFile = applyPatch(file1Contents, patch);
fs.writeFileSync(`${outPath}/efb.js`, patchedFile);
file1Contents = fs.readFileSync('./EFB/efb.index.js').toString();
patch = fs.readFileSync('./EFB/efb-index-js.patch').toString();
patchedFile = applyPatch(file1Contents, patch);
fs.writeFileSync(`${outPath}/efb.index.js`, patchedFile);
file1Contents = fs.readFileSync('./EFB/efb.html').toString();
patch = fs.readFileSync('./EFB/efb-html.patch').toString();
patchedFile = applyPatch(file1Contents, patch);
fs.writeFileSync(`${outPath}/efb.html`, patchedFile);
var output = '';
var lineReader = readline.createInterface({
input: fs.createReadStream(`${outPath}/App.js`),
});
lineReader.on('line', (line) => {
if (line.startsWith('import')) {
output += '// ' + line + '\n';
} else if (line.startsWith('export')) {
output += 'window.KH_LM = App;\n';
} else {
output += line + '\n';
}
});
lineReader.on('close', () => {
fs.writeFile(`${outPath}/App.js`, output, (err) => {
if (err) console.log(err);
console.log('Import/Export removed.');
});
});
+26
View File
@@ -0,0 +1,26 @@
{
"name": "xkhofmann-tfdidesign-md11-load-manager",
"version": "0.0.1",
"description": "TFDi MD11 Load Manager project",
"scripts": {
"debugger": "cd \"$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"
}
}

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