TFDi_MD-11_QA/xkhofmann-tfdidesign-md11-load-manager
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base: TFDi_MD-11_QA:d805d315f88f493f0609402008cf48edfc9f9a46
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TFDi_MD-11_QA:master
TFDi_MD-11_QA:2024
TFDi_MD-11_QA:Panel
..
compare: TFDi_MD-11_QA:122a93461d1835c4d88c9fb1ad10a17f7d688a18
Branches Tags
TFDi_MD-11_QA:master
TFDi_MD-11_QA:2024
TFDi_MD-11_QA:Panel

9 Commits
d805d315f8 ... 122a93461d

Author SHA1 Message Date
Kilian Hofmann
122a93461d Non GSX Fuel setting 2026-02-12 21:27:12 +01:00
Kilian Hofmann
310b5f39dc Update to 1.1.14 2026-02-05 22:16:28 +01:00
Kilian Hofmann
3b003f3363 update to 1.1.14 2026-02-05 01:04:29 +01:00
Kilian Hofmann
818277edcf Build 1.1.0 2026-01-28 20:13:43 +01:00
Kilian Hofmann
73ebaa311b Update configs for flap drag 2026-01-28 15:48:56 +01:00
Kilian Hofmann
d96ea55b31 Fix GSX deboarding 2026-01-24 21:11:40 +01:00
Kilian Hofmann
b379a6dccd Update to 1.1.9 2026-01-24 13:59:54 +01:00
Kilian Hofmann
766d956008 2024 Build an working 2025-12-16 21:30:47 +01:00
Kilian Hofmann
ec9facd4d9 New Configs 2025-12-16 21:02:20 +01:00
49 changed files with 4222 additions and 8453 deletions
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6
.clang-format Normal file
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@ -0,0 +1,6 @@
---
BasedOnStyle: LLVM
ColumnLimit: 130
IndentCaseLabels: true
AllowShortIfStatementsOnASingleLine: Always
AllowShortLoopsOnASingleLine: true

3
.vscode/settings.json vendored
View File

@ -18,5 +18,8 @@
},
"[xml]": {
"editor.defaultFormatter": "redhat.vscode-xml"
},
"[typescriptreact]": {
"editor.defaultFormatter": "esbenp.prettier-vscode"
}
}

23
EFB/efb-js.patch
View File

@ -2,23 +2,26 @@ Index: EFB.js
===================================================================
--- EFB.js
+++ EFB.js
@@ -30203,9 +30203,9 @@
@@ -40265,11 +40265,11 @@
),
/* @__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",
"data-ripple-light": "true",
onClick: () => getOutput(),
- children: "Set Payload"
+ children: "Manage Payload"
- children: "Set payload & fuel"
+ children: "Manage payload & fuel"
}
) }) })
] }) }) });
}
@@ -40556,8 +40556,27 @@
),
/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
"button",
@@ -40767,8 +40767,27 @@
] })
] }) }) });
}
+ // Exports for add. script
+// Exports for add. script
+ window.reactExports = __toESM(require_react());
+ window.reactDomExports = __toESM(require_react_dom());
+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());

10
PackageDefinitions/xkhofmann-tfdidesign-md11-load-manager.xml
View File

@ -1,5 +1,5 @@
<?xml version="1.0" encoding="utf-8"?>
<AssetPackage Version="0.1.0">
<AssetPackage Version="1.1.0">
<ItemSettings>
<ContentType>MISC</ContentType>
<Title>TFDi Design MD-11 Load Manager</Title>
@ -10,9 +10,10 @@
<VisibleInStore>false</VisibleInStore>
<CanBeReferenced>false</CanBeReferenced>
</Flags>
<PackageOrderHint>CUSTOM_SIMOBJECTS_PATCH</PackageOrderHint>
<AssetGroups>
<AssetGroup Name="ContentInfo">
<Type>ContentInfo</Type>
<Type Version="0">ContentInfo</Type>
<Flags>
<FSXCompatibility>false</FSXCompatibility>
</Flags>
@ -20,7 +21,7 @@
<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
</AssetGroup>
<AssetGroup Name="html-ui">
<Type>Copy</Type>
<Type Version="0">Copy</Type>
<Flags>
<FSXCompatibility>false</FSXCompatibility>
</Flags>
@ -31,7 +32,7 @@
</Config>
</AssetGroup>
<AssetGroup Name="md-11-panel-config">
<Type>Copy</Type>
<Type Version="0">Copy</Type>
<Flags>
<FSXCompatibility>false</FSXCompatibility>
</Flags>
@ -40,4 +41,3 @@
</AssetGroup>
</AssetGroups>
</AssetPackage>

0
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/panel/PANEL.CFG → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/common/panel/PANEL.CFG
View File

102
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11 GE LOW/config/flight_model.cfg
View File

@ -1,15 +1,15 @@
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
[VERSION]
//KH Bump major
major = 4
minor = 1
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
@ -24,21 +24,21 @@ station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.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, 0
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 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, 0
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 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
@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 1.32645
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
@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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, 1917.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
@ -265,7 +265,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
@ -319,19 +319,19 @@ 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,-75,33,2,33,2,2,33,0
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,0
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,0
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,0
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,0
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,0
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-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
@ -348,8 +348,8 @@ type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -357,12 +357,12 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1]
@ -370,8 +370,8 @@ type = 1
system_type = 1
span-outboard = 0.7
extending-time = 23
damaging-speed = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -379,12 +379,12 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2]
@ -392,8 +392,8 @@ type = 2
system_type = 1
span-outboard = 0.2
extending-time = 8
damaging-speed = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
@ -407,8 +407,8 @@ type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75

418
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11 GE/config/flight_model.cfg Normal file
View File

@ -0,0 +1,418 @@
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
[VERSION]
//KH Bump major
major = 4
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
empty_weight_roll_MOI = 6368555
empty_weight_yaw_MOI = 40761191
empty_weight_coupled_MOI = 0
activate_mach_limit_based_on_cg = 0
activate_cg_limit_based_on_mach = 0
max_number_of_stations = 21
//KH START Empty default
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
//KH END
[CONTACT_POINTS]
static_pitch = 0
static_cg_height = 16.4
gear_system_type = 1
tailwheel_lock = 0
max_number_of_points = 16
gear_locked_on_ground = 0
gear_locked_above_speed = -1
max_speed_full_steering = 25
min_available_steering_angle_pct = 0.2
max_speed_decreasing_steering = 45
max_speed_full_steering_castering = 20
max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 3.142
allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
point.2 = 1, -19.00, 17.15, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 53, 54, 3, 200, 250, 8
point.3 = 1, -19.00, 0.00, -18.02, 2000, 2, 2.25, 0, 1.60, 1.116, 0.9, 55, 56, 3, 200, 250, 8
point.4 = 2, 93.0, 0.0, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.5 = 2, -48, -82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0, 0, 1
point.6 = 2, -48, 82.5, 0.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0, 0, 1
point.7 = 2, 60, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.8 = 2, 60, 0.0, 11.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
point.9 = 2, 16.0, -28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.10 = 2, 16.0, 28.00, -13.00, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.11 = 2, -110.0, 0.00, 14.20, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.12 = 2, -96.5, 0.0, 42.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.13 = 2, -94.5, -30.0, 8.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.14 = 2, -94.5, 30.0, 8.05, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0, 0, 1
point.15 = 2, -52.0, 0.0, -9.0, 787, 0, 0.0, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0, 0, 1
[FUEL]
LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
RightMain = -20.00, 38.00, -1.0, 8938, 10.00
Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
engine_driven_pump = 1
manual_transfer_pump = 0
manual_pump = 0
anemometer_pump = 0
fuel_dump_rate = 0.02
default_fuel_tank_selector.1 = 1
default_fuel_tank_selector.2 = 1
default_fuel_tank_selector.3 = 1
[AIRPLANE_GEOMETRY]
wing_area = 3648
wing_span = 170.5
wing_root_chord = 34.68
wing_camber = 1
wing_thickness_ratio = 0.04
wing_dihedral = 2.2
wing_incidence = 1.5
wing_twist = -0.5
oswald_efficiency_factor = 0.72
wing_winglets_flag = 1
wing_sweep = 38
wing_pos_apex_lon = 1
wing_pos_apex_vert = -2.75
htail_area = 920
htail_span = 59.5
htail_pos_lon = -88
htail_pos_vert = 5.0
htail_incidence = 0.8
htail_sweep = 36.5
htail_thickness_ratio = 0.02
vtail_area = 760
vtail_span = 28.1
vtail_sweep = 43
vtail_pos_lon = -79.5
vtail_pos_vert = 28
vtail_thickness_ratio = 0.03
fuselage_length = 202.16
fuselage_diameter = 19.75
fuselage_center_pos = 10, 0, 1.0
elevator_area = 327.0
aileron_area = 225.0
rudder_area = 190.0
elevator_up_limit = 25
elevator_down_limit = 15
aileron_up_limit = 25
aileron_down_limit = 15
rudder_limit = 23
rudder_trim_limit = 20
elevator_trim_limit = 30
spoiler_limit = 60
spoilerons_available = 1
aileron_to_spoileron_gain = 3
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoiler_extension_time = 2.0
spoiler_handle_available = 1
auto_spoiler_available = 1
auto_spoiler_auto_retracts = 0
auto_spoiler_min_speed = 72
positive_g_limit_flaps_up = 5.0
positive_g_limit_flaps_down = 4.0
negative_g_limit_flaps_up = -4.0
negative_g_limit_flaps_down = -3.0
load_safety_factor = 1.5
elevator_trim_neutral = -1
aileron_to_rudder_scale = 0
flap_to_aileron_scale = 0
fly_by_wire = 0
elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
[AERODYNAMICS]
lift_coef_pitch_rate = -8.09375
lift_coef_daoa = 2.68359
lift_coef_delta_elevator = -0.28906
lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
side_force_roll_rate = 0.15478
side_force_yaw_rate = 0
side_force_delta_rudder = -0.14746
pitch_moment_horizontal_incidence = 4.24755
pitch_moment_delta_elevator = -2.37011
pitch_moment_delta_trim = 0
pitch_moment_pitch_damping = -214.1455
pitch_moment_aoa_0 = 0.11621
pitch_moment_daoa = 8.87255
pitch_moment_flaps = 0.0105
pitch_moment_gear = 0.0171
pitch_moment_spoilers = 0
pitch_moment_delta_elevator_propwash = -2.37011
pitch_moment_pitch_propwash = -214.1455
roll_moment_slip_angle = 0.26855
roll_moment_roll_damping = -3.40869
roll_moment_yaw_rate = -0.27197
roll_moment_spoilers = 0.07
roll_moment_delta_aileron = -0.34521
roll_moment_delta_rudder = 0.01660
roll_moment_delta_aileron_trim_scalar = -0.2
yaw_moment_slip_angle = 0.18066
yaw_moment_roll = 0.07470
yaw_moment_yaw_damping = -2.49023
yaw_moment_yaw_propwash = 0
yaw_moment_delta_aileron = -0.00683
yaw_moment_delta_rudder = 0.07128
yaw_moment_delta_rudder_propwash = 0.075
yaw_moment_delta_rudder_trim_scalar = -0.2
compute_aero_center = 0
aero_center_lift = -13.75
lift_coef_aoa_table = -3.15:0, -2.36:0.36, -1.57:0, -0.349:-1.2, 0:-0.022, 0.0314:0.6082, 0.221:2.049, 0.244:1.15, 0.349:0.6, 0.436:0.5, 0.698:0.1, 1.963:-0.359, 2.356:-0.5, 3.15:0
lift_coef_ground_effect_mach_table = 0.06:0.50, 0.227:0.80, 0.242:0.80, 0.3:1.0, 0.9:1.0
lift_coef_mach_table = 0:1
lift_coef_delta_elevator_mach_table = 0:0
lift_coef_daoa_mach_table = 0:0
lift_coef_pitch_rate_mach_table = 0:0
lift_coef_horizontal_incidence_mach_table = 0:0
drag_coef_zero_lift_mach_tab = 0:0, 0.4:0.0054, 0.5:0.0056, 0.6:0.0059, 0.7:0.0062, 0.72:0.0062, 0.8:0.0063, 0.8:0.0063, 1:0.0337, 1.2:0.0337, 1.4:0.0337, 1.6:0.0337, 1.8:0.0337, 2.0:0.0337
side_force_slip_angle_mach_table = 0:0
side_force_delta_rudder_mach_table = 0:0
side_force_yaw_rate_mach_table = 0:0
side_force_roll_rate_mach_table = 0:0
pitch_moment_aoa_table = -3.15:-2, -0.436:-0.626, -0.262:-0.434, 0:-0.146, 0.087:-0.05, 0.175:0.0466, 0.262:0.143, 0.314:0.2, 0.349:0.1, 0.436:0.15, 3.15:2
pitch_moment_delta_elevator_aoa_table = -180:-1, -40:0.05, -20:0.455, -14:0.853, -7:1.007, 0:1, 7:0.839, 14:0.693, 20:0.381, 40:-0.08, 180:-1
pitch_moment_horizontal_incidence_aoa_table = 0:1
pitch_moment_daoa_aoa_table = 0:1
pitch_moment_pitch_alpha_table = 0:1
pitch_moment_delta_elevator_mach_table = 0:0
pitch_moment_daoa_mach_table = 0:0
pitch_moment_pitch_rate_mach_table = 0:0
pitch_moment_horizontal_incidence_mach_table = 0:0
pitch_moment_aoa_0_mach_table = 0:0
roll_moment_aoa_table = 0:0
roll_moment_slip_angle_aoa_table = 0:1
roll_moment_roll_rate_aoa_table = 0:1
roll_moment_delta_aileron_aoa_table = 0:1
roll_moment_slip_angle_mach_table = 0:0
roll_moment_delta_rudder_mach_table = 0:0
roll_moment_delta_aileron_mach_table = 0:0
roll_moment_yaw_rate_mach_table = 0:0
roll_moment_roll_rate_mach_table = 0:0
yaw_moment_aoa_table = 0:0
yaw_moment_slip_angle_aoa_table = 0:1
yaw_moment_yaw_rate_aoa_table = 0:1
yaw_moment_delta_rudder_aoa_table = 0:1
yaw_moment_slip_angle_mach_table = 0:0
yaw_moment_delta_rudder_mach_table = 0:0
yaw_moment_delta_aileron_mach_table = 0:0
yaw_moment_yaw_rate_mach_table = 0:0
yaw_moment_roll_rate_mach_table = 0:0
elevator_scaling_table = -0.785:0.5, -0.524:0.85, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.85, 0.785:0.5 ; 0:1
aileron_scaling_table = -0.785:1 ;0:1
rudder_scaling_table = -0.785:0.5, -0.524:0.6, -0.175:0.9, 0:1, 0.175:0.9, 0.524:0.6, 0.785:0.5 ;0:1
elevator_lift_coef=3
rudder_lift_coef=2
aileron_load_factor_effectiveness_table = 0:1
lift_coef_at_drag_zero = 0.1
lift_coef_at_drag_zero_flaps = 0.1
[FLIGHT_TUNING]
modern_fm_only = 1
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
rudder_maxangle_scalar = 1
pitch_stability = 5
roll_stability = 1
yaw_stability = 1
pitch_gyro_stability = 1
roll_gyro_stability = 1
yaw_gyro_stability = 1
empty_CG_deviation_limit=0
elevator_trim_effectiveness = 1.5
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 0
hi_alpha_on_yaw = 0
p_factor_on_yaw = 0
torque_on_roll = 0
gyro_precession_on_roll = 0
gyro_precession_on_yaw = 0
engine_wash_on_roll = 0
wingflex_scalar = 2
wingflex_offset = 0
stall_coef_at_min_weight = 0.71
ground_crosswind_effect_zero_speed=10
ground_crosswind_effect_max_speed=150
ground_high_speed_steeringwheel_static_friction_scalar=1.5
ground_high_speed_otherwheel_static_friction_scalar=1.2
[REFERENCE SPEEDS]
full_flaps_stall_speed = 115
flaps_up_stall_speed = 149
cruise_speed = 345
cruise_mach = 0.85
crossover_speed = 330
max_mach = 0.9
max_indicated_speed = 395
max_flaps_extended = 170
normal_operating_speed = 325
airspeed_indicator_max = 562.5
rotation_speed_min = 145
climb_speed = 250
cruise_alt = 41000
takeoff_speed = 165
spawn_cruise_altitude = 5000
spawn_descent_altitude = 500
best_angle_climb_speed = 0
approach_speed = 0
best_glide = 0
max_gear_extended = 200
[INTERACTIVE POINTS]
number_of_interactive_points = 13
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
[STALL PROTECTION]
stall_protection = 1 ; Alpha Protection
off_limit = 11.5 ; Alpha below which the Alpha Protection can be disabled (If also below off_yoke_limit)
off_yoke_limit = 1 ; Yoke position (in Pct) below which the Alpha Protection can be disabled (If also below off_limit)
on_limit = 14 ; Alpha above which the Alpha Protection timer starts
on_goal = 10 ; The alpha that the Alpha Protection will attempt to reach when triggered
timer_trigger = 1.0 ; Duration (in Sec) the alpha must be above on_limit before the Alpha Protection is triggered
;===================== FLAPS =====================
[FLAPS.0]
type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
pitch_scalar = 1
max_on_ground_position = 7
flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1]
type = 1
system_type = 1
span-outboard = 0.7
extending-time = 23
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
pitch_scalar = 1
max_on_ground_position = 7
flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2]
type = 2
system_type = 1
span-outboard = 0.2
extending-time = 8
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, 215, 0.5, 0.5
[FLAPS.3]
type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
pitch_scalar = 1
max_on_ground_position = 1
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, 215, 0.5, 0.5

417
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11 PW LOW/config/flight_model.cfg Normal file
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@ -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

105
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11 PW/config/flight_model.cfg
View File

@ -1,15 +1,18 @@
//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25
; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 1
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
@ -24,21 +27,21 @@ station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.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, 0
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 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, 0
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 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
@ -59,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 1.32645
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
@ -88,9 +91,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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, 1917.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
@ -175,7 +178,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
@ -265,7 +268,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
@ -319,19 +322,19 @@ 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,-75,33,2,33,2,2,33,0
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,0
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,0
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,0
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,0
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,0
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-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
@ -348,8 +351,8 @@ type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -357,20 +360,20 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -378,20 +381,20 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
@ -405,8 +408,8 @@ type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75

74
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11F GE LOW/config/flight_model.cfg
View File

@ -1,15 +1,18 @@
//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 1
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 248567
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
@ -20,9 +23,9 @@ 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, 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.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
@ -53,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 1.32645
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
@ -82,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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, 1917.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
@ -259,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
@ -313,14 +316,14 @@ 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,-75,33,2,33,2,2,33,0
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-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
@ -337,8 +340,8 @@ type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -346,20 +349,21 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -367,20 +371,20 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
@ -394,8 +398,8 @@ type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75

409
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11F GE/config/flight_model.cfg Normal file
View File

@ -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

73
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11F PW LOW/config/flight_model.cfg
View File

@ -1,15 +1,18 @@
//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 1
minor = 8
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 248567
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0
empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12
CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456
@ -20,9 +23,9 @@ 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, 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.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
@ -53,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2
hyd_need_power_to_function= 0
min_castering_angle = 0.05236
max_castering_angle = 1.32645
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
@ -82,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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, 1917.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 0
@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1
lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889
drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392
@ -259,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
elevator_effectiveness = 1
elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
@ -313,14 +316,14 @@ 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,-75,33,2,33,2,2,33,0
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-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
@ -337,8 +340,8 @@ type = 1
system_type = 1
span-outboard = 0.25
extending-time = 22
damaging-speed = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -346,20 +349,20 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 280
blowout-speed = 310
maneuvering_flaps = 0
lift_scalar = 0.1
drag_scalar = 1.1
@ -367,20 +370,20 @@ 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, 0.25, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1
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, 150, 0.33, 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 = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75
@ -394,8 +397,8 @@ type = 2
system_type = 1
span-outboard = 0.7
extending-time = 21
damaging-speed = 250
blowout-speed = 300
damaging-speed = 300
blowout-speed = 330
maneuvering_flaps = 0
lift_scalar = 0.5
drag_scalar = 0.75

408
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/presets/tfdi-design/TFDi_Design_MD-11F PW/config/flight_model.cfg Normal file
View File

@ -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

2
PackageSources/js-bundle/package.json
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@ -1,6 +1,6 @@
{
"name": "tfdidesign-md11-load-manager",
"version": "0.1.186",
"version": "0.2.8",
"description": "",
"main": "index.js",
"type": "module",

17
PackageSources/js-bundle/src/assets/licenses_node.md
View File

@ -1,7 +1,8 @@
| Department | Related to | Name | License period | Material not material | License type | Link | Remote version | Installed version | Defined version | Author |
| :--------- | :--------- | :------------------------------- | :------------- | :-------------------- | :----------- | :------------------------------------------------------------------------ | :------------- | :---------------- | :-------------- | :---------------------------------------------------------- |
| kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.0 | 19.1.0 | ^19.1.0 | n/a |
| kessler | stuff | react-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.0 | 19.1.0 | ^19.1.0 | n/a |
| kessler | stuff | lucide-react | perpetual | material | ISC | git+https://github.com/lucide-icons/lucide.git | 0.555.0 | 0.555.0 | ^0.555.0 | Eric Fennis |
| kessler | stuff | react | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.4 | 19.1.0 | ^19.1.0 | n/a |
| kessler | stuff | react-dom | perpetual | material | MIT | git+https://github.com/facebook/react.git | 19.2.4 | 19.1.0 | ^19.1.0 | n/a |
| kessler | stuff | uuid | perpetual | material | MIT | git+https://github.com/uuidjs/uuid.git | 11.1.0 | 11.1.0 | ^11.1.0 | n/a |
| kessler | stuff | @microsoft/msfs-types | perpetual | material | MIT | git+https://github.com/microsoft/msfs-avionics-mirror.git | 1.14.6 | 1.14.6 | ^1.14.6 | Asobo Studio / Working Title Simulations |
| kessler | stuff | @rollup/plugin-commonjs | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 28.0.9 | 28.0.3 | ^28.0.3 | Rich Harris <richard.a.harris@gmail.com> |
@ -10,13 +11,13 @@
| kessler | stuff | @rollup/plugin-replace | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 6.0.3 | 6.0.2 | ^6.0.2 | Rich Harris <richard.a.harris@gmail.com> |
| kessler | stuff | @rollup/plugin-terser | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 0.4.4 | 0.4.4 | ^0.4.4 | Peter Placzek <peter.placzek1996@gmail.com> |
| kessler | stuff | @rollup/plugin-typescript | perpetual | material | MIT | git+https://github.com/rollup/plugins.git | 12.3.0 | 12.1.2 | ^12.1.2 | Oskar Segersvärd |
| kessler | stuff | @types/node | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 24.10.1 | 24.3.1 | ^24.3.1 | n/a |
| kessler | stuff | @types/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.7 | 19.1.6 | ^19.1.6 | n/a |
| kessler | stuff | @types/node | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 24.10.11 | 24.3.1 | ^24.3.1 | n/a |
| kessler | stuff | @types/react | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.13 | 19.1.6 | ^19.1.6 | n/a |
| kessler | stuff | @types/react-dom | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 19.2.3 | 19.1.6 | ^19.1.6 | n/a |
| kessler | stuff | @types/uuid | perpetual | material | MIT | https://github.com/DefinitelyTyped/DefinitelyTyped.git | 10.0.0 | 10.0.0 | ^10.0.0 | n/a |
| kessler | stuff | @typescript-eslint/eslint-plugin | perpetual | material | MIT | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.21.0 | n/a |
| kessler | stuff | @typescript-eslint/parser | perpetual | material | BSD-2-Clause | git+https://github.com/typescript-eslint/typescript-eslint.git | 6.21.0 | 6.21.0 | ^6.21.0 | n/a |
| kessler | stuff | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.22 | 10.4.21 | ^10.4.21 | Andrey Sitnik <andrey@sitnik.ru> |
| kessler | stuff | autoprefixer | perpetual | material | MIT | git+https://github.com/postcss/autoprefixer.git | 10.4.24 | 10.4.21 | ^10.4.21 | Andrey Sitnik <andrey@sitnik.ru> |
| kessler | stuff | cross-env | perpetual | material | MIT | git+https://github.com/kentcdodds/cross-env.git | 7.0.3 | 7.0.3 | ^7.0.3 | Kent C. Dodds <me@kentcdodds.com> (https://kentcdodds.com) |
| kessler | stuff | eslint | perpetual | material | MIT | git+https://github.com/eslint/eslint.git | 8.57.1 | 8.57.1 | ^8.57.1 | Nicholas C. Zakas <nicholas+npm@nczconsulting.com> |
| kessler | stuff | eslint-plugin-import | perpetual | material | MIT | git+https://github.com/import-js/eslint-plugin-import.git | 2.32.0 | 2.31.0 | ^2.31.0 | Ben Mosher <me@benmosher.com> |
@ -25,15 +26,15 @@
| kessler | stuff | license-report | perpetual | material | MIT | git+https://github.com/kessler/license-report.git | 6.8.1 | 6.7.2 | ^6.7.2 | Yaniv Kessler |
| kessler | stuff | postcss | perpetual | material | MIT | git+https://github.com/postcss/postcss.git | 8.5.6 | 8.5.4 | ^8.5.4 | Andrey Sitnik <andrey@sitnik.ru> |
| kessler | stuff | postcss-import | perpetual | material | MIT | git+https://github.com/postcss/postcss-import.git | 16.1.1 | 16.1.0 | ^16.1.0 | Maxime Thirouin |
| kessler | stuff | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.7.3 | 3.5.3 | ^3.5.3 | James Long |
| kessler | stuff | prettier | perpetual | material | MIT | git+https://github.com/prettier/prettier.git | 3.8.1 | 3.5.3 | ^3.5.3 | James Long |
| kessler | stuff | prettier-plugin-organize-imports | perpetual | material | MIT | git+https://github.com/simonhaenisch/prettier-plugin-organize-imports.git | 4.3.0 | 4.1.0 | ^4.1.0 | Simon Haenisch (https://github.com/simonhaenisch) |
| kessler | stuff | rimraf | perpetual | material | ISC | git+ssh://git@github.com/isaacs/rimraf.git | 6.1.2 | 6.0.1 | ^6.0.1 | Isaac Z. Schlueter <i@izs.me> (http://blog.izs.me/) |
| kessler | stuff | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.53.3 | 4.42.0 | ^4.42.0 | Rich Harris |
| kessler | stuff | rollup | perpetual | material | MIT | git+https://github.com/rollup/rollup.git | 4.57.1 | 4.42.0 | ^4.42.0 | Rich Harris |
| kessler | stuff | rollup-plugin-copy | perpetual | material | MIT | git+https://github.com/vladshcherbin/rollup-plugin-copy.git | 3.5.0 | 3.5.0 | ^3.5.0 | Vlad Shcherbin <vlad.shcherbin@gmail.com> |
| kessler | stuff | rollup-plugin-postcss | perpetual | material | MIT | git+https://github.com/egoist/rollup-plugin-postcss.git | 4.0.2 | 4.0.2 | ^4.0.2 | EGOIST <0x142857@gmail.com> |
| kessler | stuff | rollup-plugin-react-svg | perpetual | material | MIT | git+https://github.com/boopathi/react-svg-loader.git | 3.0.3 | 3.0.3 | ^3.0.3 | boopathi |
| kessler | stuff | rollup-plugin-version-injector | perpetual | material | ISC | git+https://github.com/djhouseknecht/rollup-plugin-version-injector.git | 1.3.3 | 1.3.3 | ^1.3.3 | David Houseknecht <david.j.houseknecht@gmail.com> |
| kessler | stuff | sass | perpetual | material | MIT | git+https://github.com/sass/dart-sass.git | 1.94.2 | 1.89.1 | ^1.89.1 | Natalie Weizenbaum nweiz@google.com https://github.com/nex3 |
| kessler | stuff | sass | perpetual | material | MIT | git+https://github.com/sass/dart-sass.git | 1.97.3 | 1.89.1 | ^1.89.1 | Natalie Weizenbaum nweiz@google.com https://github.com/nex3 |
| kessler | stuff | tslib | perpetual | material | 0BSD | git+https://github.com/Microsoft/tslib.git | 2.8.1 | 2.8.1 | ^2.8.1 | Microsoft Corp. |
| kessler | stuff | typed-scss-modules | perpetual | material | MIT | git+https://github.com/skovy/typed-scss-modules.git | 8.1.1 | 8.1.1 | ^8.1.1 | Spencer Miskoviak <smiskoviak@gmail.com> |
| kessler | stuff | typescript | perpetual | material | Apache-2.0 | git+https://github.com/microsoft/TypeScript.git | 5.8.3 | 5.8.3 | 5.8.3 | Microsoft Corp. |

42
PackageSources/js-bundle/src/components/SBEntry/SBEntryF.tsx
View File

@ -2,7 +2,7 @@ import { FC, useEffect, useState } from 'react';
import { WASMDataF } from '../../types/WASMData';
import { LoadingState, SimBrief } from '../../types/general';
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
import { CoherentCallSBEntryF, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallSBEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -16,8 +16,7 @@ interface SBEntryProps {
const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
const [fuelEnabled, setFuelEnabled] = useState(true);
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [SBInFlight, setSBInFlight] = useState(false);
// FROM EFB
@ -52,6 +51,11 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
}
};
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
CoherentCallSBEntryF(CGTarget, _fuel ?? fuel, SBPlan);
};
useEffect(() => updateData(), [CGTarget, fuel]);
useEffect(() => {
if (!simBrief || gsxActive) return;
@ -70,12 +74,13 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
return;
}
updateData(undefined, SBResponse.message as SimBrief);
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
updateData(SBResponse.message as SimBrief, _fuel);
setFuel(_fuel);
setSBInFlight(false);
}, [simBrief, gsxActive]);
useEffect(
() =>
setFuel((prev) => {
@ -84,13 +89,6 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
const updateData = (_CGTarget?: number, SBPlan?: SimBrief) => {
CoherentCallSBEntryF(_CGTarget ?? CGTarget, SBPlan);
};
return (
<>
@ -106,22 +104,6 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>
@ -164,14 +146,12 @@ const SBEntryF: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoad
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
updateData(_new);
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
updateData(_new);
return _new;
})
}

40
PackageSources/js-bundle/src/components/SBEntry/SBEntryPax.tsx
View File

@ -2,7 +2,7 @@ import { FC, useEffect, useState } from 'react';
import { WASMDataPax } from '../../types/WASMData';
import { LoadingState, SimBrief } from '../../types/general';
import { ImportFlightPlanKH } from '../../utils/TFDISBImport';
import { CoherentCallSBEntryPax, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallSBEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -16,7 +16,7 @@ interface SBEntryProps {
const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [fuelEnabled, setFuelEnabled] = useState(true);
const [SBInFlight, setSBInFlight] = useState(false);
@ -52,6 +52,10 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
}
};
const updateData = (SBPlan?: SimBrief, _fuel?: number) => {
CoherentCallSBEntryPax(CGTarget, _fuel ?? fuel, SBPlan);
};
useEffect(() => {
if (!simBrief || gsxActive) return;
@ -70,12 +74,17 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
return;
}
updateData(undefined, SBResponse.message as SimBrief);
const _fuel = parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0;
updateData(SBResponse.message as SimBrief, _fuel);
setFuel(_fuel);
setFuel(parseFloat((SBResponse.message as SimBrief).fuel as unknown as string) ?? 0);
setSBInFlight(false);
}, [simBrief, gsxActive]);
useEffect(() => updateData(), [CGTarget, fuel]);
useEffect(
() =>
setFuel((prev) => {
@ -84,13 +93,6 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
const updateData = (_CGTarget?: number, SBPlan?: SimBrief) => {
CoherentCallSBEntryPax(_CGTarget ?? CGTarget, SBPlan);
};
return (
<>
@ -106,22 +108,6 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>
@ -164,14 +150,12 @@ const SBEntryPax: FC<SBEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
updateData(_new);
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
updateData(_new);
return _new;
})
}

4
PackageSources/js-bundle/src/components/input/Input.tsx
View File

@ -5,11 +5,11 @@ import Keyboard from '../keyboard/Keyboard';
export default function Input(props: {
type?: string;
topKeyboard?: boolean;
value: any;
value: number | string;
min?: number;
max?: number;
step?: number;
placeholder?: any;
placeholder?: string;
className?: string;
disabled?: boolean;
onChange?: (value: string) => void;

1
PackageSources/js-bundle/src/components/keyboard/Keyboard.tsx
View File

@ -103,5 +103,6 @@ const Keyboard = forwardRef<
document.body
);
});
Keyboard.displayName = "Keyboard"
export default Keyboard;

4
PackageSources/js-bundle/src/components/options/OptionsF.tsx
View File

@ -48,7 +48,7 @@ const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight</td>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249537 lbs' : '113188 kg'}</td>
</tr>
<tr>
@ -84,7 +84,7 @@ const OptionsF: FC<OptionsFProps> = ({ WASMData, loadingState, gsxActive }) => {
<td className="p-1 px-2">0 {WASMData.userData.isImperial ? 'lbs' : 'kg'}</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight</td>
<td className="p-1 px-2">Empty Weight (inc. crew)</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '249137 lbs' : '113006 kg'}</td>
</tr>
<tr>

10
PackageSources/js-bundle/src/components/options/OptionsPax.tsx
View File

@ -2,8 +2,8 @@ import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataPax } from '../../types/WASMData';
import { CoherentCallGSXReset, CoherentCallOptionsSet } from '../../utils/utils';
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
import Input from '../input/Input';
import ToggleComponentKH from '../toggleComponent/ToggleComponent';
interface OptionsPaxProps {
WASMData: WASMDataPax;
@ -105,8 +105,8 @@ const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive })
</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '284375 lbs' : '128991 kg'}</td>
<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>
@ -145,8 +145,8 @@ const OptionsPax: FC<OptionsPaxProps> = ({ WASMData, loadingState, gsxActive })
</td>
</tr>
<tr>
<td className="p-1 px-2">Empty Weight</td>
<td className="p-1 px-2">{WASMData.userData.isImperial ? '283975 lbs' : '128809 kg'}</td>
<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>

28
PackageSources/js-bundle/src/components/stationEntry/StationEntryF.tsx
View File

@ -1,7 +1,7 @@
import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataF } from '../../types/WASMData';
import { CoherentCallStationEntryF, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallStationEntryF, loadAircraft, unloadAircraft } from '../../utils/utils';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -19,8 +19,7 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
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.livePayload.fuel));
const [fuelEnabled, setFuelEnabled] = useState(true);
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
@ -52,10 +51,10 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
};
const updateData = () => {
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear);
CoherentCallStationEntryF(upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel);
};
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear]);
useEffect(() => updateData(), [upper1, upper2, upper3, upper4, lowerForward, lowerRear, fuel]);
useEffect(
() =>
setFuel((prev) => {
@ -64,9 +63,6 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
return (
<>
@ -82,22 +78,6 @@ const StationEntryF: FC<StationEntryProps> = ({ WASMData, loadingState, gsxActiv
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>

26
PackageSources/js-bundle/src/components/stationEntry/StationEntryPax.tsx
View File

@ -1,7 +1,7 @@
import { FC, useEffect, useState } from 'react';
import { LoadingState } from '../../types/general';
import { WASMDataPax } from '../../types/WASMData';
import { CoherentCallStationEntryPax, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallStationEntryPax, loadAircraft, unloadAircraft } from '../../utils/utils';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -20,7 +20,6 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
const [forwardCargo, setForwardCargo] = useState(WASMData.targetPayload.forwardCargo);
const [rearCargo, setRearCargo] = useState(WASMData.targetPayload.rearCargo);
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
const [fuelEnabled, setFuelEnabled] = useState(true);
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return Math.round(WASMData.targetPayload.total);
@ -52,10 +51,10 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
};
const updateData = () => {
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo);
CoherentCallStationEntryPax(business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel);
};
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo]);
useEffect(() => updateData(), [business1, business2, economy1, economy2, forwardCargo, rearCargo, fuel]);
useEffect(
() =>
setFuel((prev) => {
@ -64,9 +63,6 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
return (
<>
@ -82,22 +78,6 @@ const StationEntryPax: FC<StationEntryProps> = ({ WASMData, loadingState, gsxAct
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>

44
PackageSources/js-bundle/src/components/zfwEntry/ZFWEntryF.tsx
View File

@ -1,7 +1,7 @@
import { FC, useEffect, useState } from 'react';
import { WASMDataF } from '../../types/WASMData';
import { LoadingState } from '../../types/general';
import { CoherentCallZFWEntry, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -15,9 +15,8 @@ interface ZFWEntryProps {
const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
const [fuelEnabled, setFuelEnabled] = useState(true);
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
@ -55,12 +54,13 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
const converted = parseInt(input);
if (converted) {
if (converted < 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
if (converted <= 0) setZFWTarget(Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew));
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
};
const handleBlur = (input: string) => {
const handleBlurZFW = (input: string) => {
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
if (!input) {
@ -74,10 +74,13 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
updateData(converted);
};
const updateData = () => {
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
};
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
useEffect(
() =>
setFuel((prev) => {
@ -86,13 +89,6 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
const updateData = (_ZFWTarget?: number, _CGTarget?: number) => {
CoherentCallZFWEntry(_ZFWTarget ?? ZFWTarget, _CGTarget ?? CGTarget);
};
return (
<>
@ -108,22 +104,6 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>
@ -138,7 +118,7 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={ZFWTarget}
onChange={(value) => handleInputZFW(value)}
onBlur={(value) => handleBlur(value)}
onBlur={(value) => handleBlurZFW(value)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
@ -156,14 +136,12 @@ const ZFWEntryF: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLo
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
updateData(undefined, _new);
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
updateData(undefined, _new);
return _new;
})
}

42
PackageSources/js-bundle/src/components/zfwEntry/ZFWEntryPax.tsx
View File

@ -1,7 +1,7 @@
import { FC, useEffect, useState } from 'react';
import { WASMDataPax } from '../../types/WASMData';
import { LoadingState } from '../../types/general';
import { CoherentCallZFWEntry, inRangeOf, loadAircraft, unloadAircraft } from '../../utils/utils';
import { CoherentCallZFWEntry, loadAircraft, unloadAircraft } from '../../utils/utils';
import CGSelect from '../CGSelect/CGSelect';
import ActionBar from '../actionbar/ActionBar';
import Input from '../input/Input';
@ -15,9 +15,8 @@ interface ZFWEntryProps {
const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, setLoadingState }) => {
const [CGTarget, setCGTarget] = useState(WASMData.targetPayload.CGTarget);
const [fuel, setFuel] = useState(Math.round(WASMData.livePayload.fuel));
const [fuel, setFuel] = useState(Math.round(WASMData.targetPayload.fuel));
const [ZFWTarget, setZFWTarget] = useState(Math.round(WASMData.targetPayload.total));
const [fuelEnabled, setFuelEnabled] = useState(true);
const ZFW = () => {
if (loadingState !== 'loaded' && !gsxActive) return ZFWTarget;
@ -60,7 +59,8 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
else setZFWTarget(converted);
}
};
const handleBlur = (input: string) => {
const handleBlurZFW = (input: string) => {
const minZFW = Math.round(WASMData.targetPayload.empty + WASMData.targetPayload.crew);
if (!input) {
@ -74,10 +74,13 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
else if (converted > WASMData.limits.maxZFW) setZFWTarget(WASMData.limits.maxZFW);
else setZFWTarget(converted);
}
updateData(converted);
};
const updateData = () => {
CoherentCallZFWEntry(ZFWTarget, CGTarget, fuel);
};
useEffect(() => updateData(), [ZFWTarget, CGTarget, fuel]);
useEffect(
() =>
setFuel((prev) => {
@ -86,13 +89,6 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
}),
[WASMData.userData.isER]
);
useEffect(() => {
setFuelEnabled((prev) => (!prev ? inRangeOf(Math.round(WASMData.livePayload.fuel), fuel) : prev));
}, [WASMData.livePayload.fuel]);
const updateData = (_ZFWTarget?: number, _CGTarget?: number) => {
CoherentCallZFWEntry(_ZFWTarget ?? ZFWTarget, _CGTarget ?? CGTarget);
};
return (
<>
@ -108,22 +104,6 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
onChange={(value) => handleInput(value, WASMData.limits.maxFuel, setFuel)}
disabled={loadingState !== 'preview' || gsxActive}
/>
<button
className="middle none center rounded-lg bg-green-600 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none"
data-ripple-light="true"
onClick={() => {
SimVar.SetSimVarValue(
'L:MD11_EFB_PAYLOAD_FUEL',
'lbs',
WASMData.userData.isImperial ? fuel : fuel * 2.20462262185
);
SimVar.SetSimVarValue('L:MD11_EFB_READ_READY', 'bool', true);
setFuelEnabled(WASMData.livePayload.fuel === fuel);
}}
disabled={loadingState !== 'preview' || !fuelEnabled || gsxActive}
>
Load Fuel
</button>
</div>
</div>
</div>
@ -138,7 +118,7 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
className="w-1/2 rounded-lg border border-white bg-zinc-700 px-3 py-2 text-right focus:border-blue-600 focus:ring-blue-600"
value={ZFWTarget}
onChange={(value) => handleInputZFW(value)}
onBlur={(value) => handleBlur(value)}
onBlur={(value) => handleBlurZFW(value)}
disabled={loadingState !== 'preview' || gsxActive}
/>
</div>
@ -156,14 +136,12 @@ const ZFWEntryPax: FC<ZFWEntryProps> = ({ WASMData, loadingState, gsxActive, set
increase={() =>
setCGTarget((prev) => {
const _new = prev + 0.1;
updateData(undefined, _new);
return _new;
})
}
decrease={() =>
setCGTarget((prev) => {
const _new = prev - 0.1;
updateData(undefined, _new);
return _new;
})
}

10
PackageSources/js-bundle/src/types/WASMData.ts
View File

@ -5,6 +5,7 @@ interface WASMData {
sbPlanned: {
ZFW: number;
GW: number;
fuel: number;
};
loaded: boolean;
}
@ -26,6 +27,7 @@ interface TargetPayload {
ZFWCG: number;
TOCG: number;
total: number;
fuel: number;
}
interface TargetPayloadPax extends TargetPayload {
@ -39,9 +41,7 @@ interface TargetPayloadPax extends TargetPayload {
rearCargo: number;
}
interface LivePayloadPax extends TargetPayloadPax {
fuel: number;
}
type LivePayloadPax = TargetPayloadPax;
interface TargetPayloadF extends TargetPayload {
empty: number;
@ -54,9 +54,7 @@ interface TargetPayloadF extends TargetPayload {
lowerRear: number;
}
interface LivePayloadF extends TargetPayloadF {
fuel: number;
}
type LivePayloadF = TargetPayloadF;
interface GSX {
couatlStarted: boolean;

17
PackageSources/js-bundle/src/utils/utils.ts
View File

@ -25,7 +25,7 @@ export const inRangeOf = (value: number, target: number, tolerance: number = 10)
return Math.abs(value - target) < tolerance;
};
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number) => {
export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number, fuelTarget: number) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
@ -33,6 +33,7 @@ export const CoherentCallZFWEntry = (ZFWTarget: number, CGTarget: number) => {
mode: CallMode.ZFW_SET,
ZFWTarget: ZFWTarget,
CGTarget: CGTarget,
fuelTarget: fuelTarget,
})
);
};
@ -43,7 +44,8 @@ export const CoherentCallStationEntryPax = (
economy1: number,
economy2: number,
forwardCargo: number,
rearCargo: number
rearCargo: number,
fuelTarget: number
) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
@ -56,6 +58,7 @@ export const CoherentCallStationEntryPax = (
economy2,
forwardCargo,
rearCargo,
fuelTarget,
})
);
};
@ -66,7 +69,8 @@ export const CoherentCallStationEntryF = (
upper3: number,
upper4: number,
lowerForward: number,
lowerRear: number
lowerRear: number,
fuelTarget: number
) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
@ -79,11 +83,12 @@ export const CoherentCallStationEntryF = (
upper4,
lowerForward,
lowerRear,
fuelTarget,
})
);
};
export const CoherentCallSBEntryPax = (CGTarget: number, SBPlan?: SimBrief) => {
export const CoherentCallSBEntryPax = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
@ -94,11 +99,12 @@ export const CoherentCallSBEntryPax = (CGTarget: number, SBPlan?: SimBrief) => {
CGTarget: CGTarget,
plannedZFW: SBPlan?.plannedZFW,
plannedGW: SBPlan?.plannedGW,
fuel: fuel,
})
);
};
export const CoherentCallSBEntryF = (CGTarget: number, SBPlan?: SimBrief) => {
export const CoherentCallSBEntryF = (CGTarget: number, fuel: number, SBPlan?: SimBrief) => {
Coherent.call(
COHERENT_COMM_BUS_WASM_CALL,
CommBusEvent.UPDATE_TARGET,
@ -108,6 +114,7 @@ export const CoherentCallSBEntryF = (CGTarget: number, SBPlan?: SimBrief) => {
CGTarget: CGTarget,
plannedZFW: SBPlan?.plannedZFW,
plannedGW: SBPlan?.plannedGW,
fuel: SBPlan?.fuel,
})
);
};

6015
PackageSources/js-bundle/yarn.lock
View File

File diff suppressed because it is too large Load Diff

135
PackageSources/wasm-module/freighter.cpp
View File

@ -1,24 +1,27 @@
#include "freighter.h"
// ZFW Entry
void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fuel, const double ZFWTarget, const UserData_t* const userData) {
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;
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) {
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->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);
unsigned int count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
MAX_REAR_CARGO(userData->isImperial, userData->isER);
// Initial distributiob
while (cargo > 0 && count > 0) {
if (cargo >= 6) {
@ -67,8 +70,7 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
targetPayload->lowerForward++;
_cargo++;
}
}
else if (cargo == 4) {
} else if (cargo == 4) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
@ -85,8 +87,7 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
targetPayload->stations.upper4++;
_cargo++;
}
}
else if (cargo == 3) {
} else if (cargo == 3) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
@ -99,8 +100,7 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
targetPayload->stations.upper3++;
_cargo++;
}
}
else if (cargo == 2) {
} else if (cargo == 2) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
@ -109,8 +109,7 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
targetPayload->stations.upper2++;
_cargo++;
}
}
else if (cargo == 1) {
} else if (cargo == 1) {
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
_cargo++;
@ -124,36 +123,31 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
count--;
}
// Refinement
count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
count = MAX_UPPER_CARGO(userData->isImperial) * 4 + MAX_FRONT_CARGO(userData->isImperial) +
MAX_REAR_CARGO(userData->isImperial, userData->isER);
while (count > 0) {
generatePayload(targetPayload, userData->isImperial);
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, userData->isImperial);
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) {
} else if (targetPayload->stations.upper2 > 0) {
targetPayload->stations.upper2--;
}
else if (targetPayload->stations.upper3 > 0) {
} else if (targetPayload->stations.upper3 > 0) {
targetPayload->stations.upper3--;
}
else {
} else {
break;
}
if (targetPayload->stations.upper4 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper4++;
}
else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
}
else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
}
else {
} else {
targetPayload->stations.upper1++;
}
}
@ -161,31 +155,24 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
if (targetPayload->stations.upper4 > 0) {
targetPayload->stations.upper4--;
}
else if (targetPayload->stations.upper3 > 0) {
} else if (targetPayload->stations.upper3 > 0) {
targetPayload->stations.upper3--;
}
else if (targetPayload->stations.upper2 > 0) {
} else if (targetPayload->stations.upper2 > 0) {
targetPayload->stations.upper2--;
}
else {
} else {
break;
}
if (targetPayload->stations.upper1 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper1++;
}
else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
} else if (targetPayload->stations.upper2 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper2++;
}
else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
} else if (targetPayload->stations.upper3 < MAX_UPPER_CARGO(userData->isImperial)) {
targetPayload->stations.upper3++;
}
else {
} else {
targetPayload->stations.upper4++;
}
}
else {
} else {
break;
}
@ -195,15 +182,14 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
count = MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
while (count > 0) {
generatePayload(targetPayload, userData->isImperial);
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, userData->isImperial);
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 {
} else {
break;
}
}
@ -212,12 +198,10 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
if (targetPayload->lowerRear > 0 && targetPayload->lowerForward < MAX_FRONT_CARGO(userData->isImperial)) {
targetPayload->lowerRear--;
targetPayload->lowerForward++;
}
else {
} else {
break;
}
}
else {
} else {
break;
}
@ -227,21 +211,22 @@ void distribute(fPayloadData_t* const targetPayload, const FuelData_t* const fue
// Updates pax stations with their respective weights
// Used internally and used for Station Entry (pax only, cargo is set directly)
void generatePayload(fPayloadData_t* const targetPayload, const bool isImperial) {
void generatePayload(fPayloadData_t *const targetPayload, const bool isImperial) {
targetPayload->upper1Left = targetPayload->upper1Right = (targetPayload->stations.upper1 / 2.0);
targetPayload->upper2Left = targetPayload->upper2Right = (targetPayload->stations.upper2 / 2.0);
targetPayload->upper3Left = targetPayload->upper3Right = (targetPayload->stations.upper3 / 2.0);
targetPayload->upper4Left = targetPayload->upper4Right = (targetPayload->stations.upper4 / 2.0);
targetPayload->total = targetPayload->empty + targetPayload->pilot + targetPayload->firstOfficer + targetPayload->engineer + targetPayload->upper1Left +
targetPayload->upper1Right + targetPayload->upper2Left + targetPayload->upper2Right + targetPayload->upper3Left +
targetPayload->upper3Right + targetPayload->upper4Left + targetPayload->upper4Right + targetPayload->lowerForward +
targetPayload->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) {
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);
@ -260,24 +245,26 @@ void normalisePayload(fPayloadData_t* const targetPayload, const bool isImperial
targetPayload->rightAux = TO_POUNDS(isImperial, targetPayload->rightAux);
}
void calculateCGs(const fPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial) {
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 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;
double totalWeight = localPayload.empty + localPayload.pilot + localPayload.firstOfficer + localPayload.engineer +
localPayload.upper1Left + localPayload.upper1Right + localPayload.upper2Left + localPayload.upper2Right +
localPayload.upper3Left + localPayload.upper3Right + localPayload.upper4Left + localPayload.upper4Right +
localPayload.lowerForward + localPayload.lowerRear + localPayload.leftAux + localPayload.rightAux;
*ZFWCG = TO_PERCENT_MAC(totalMoment / totalWeight);
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 +
@ -285,15 +272,18 @@ void calculateCGs(const fPayloadData_t* const targetPayload, const FuelData_t* c
totalWeight += fuel->total;
*TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
targetPayload->TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
}
void load(const fPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial) {
void load(const fPayloadData_t *const targetPayload, const HANDLE simConnect, const bool isImperial) {
fPayloadData_t localPayload = {};
memcpy(&localPayload, targetPayload, sizeof(localPayload));
normalisePayload(&localPayload, isImperial);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t), &localPayload);
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t),
&localPayload);
}
void unloadF(const HANDLE simConnect, const bool isER) {
@ -302,5 +292,8 @@ void unloadF(const HANDLE simConnect, const bool isER) {
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t), &localPayload);
localPayload._ZFWCG = -1;
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(fPayloadDataSet_t),
&localPayload);
}

32
PackageSources/wasm-module/freighter.h
View File

@ -1,13 +1,13 @@
#pragma once
#ifndef __INTELLISENSE__
# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#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__
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
@ -19,10 +19,11 @@
// C++ headers
#include <algorithm>
// Own headers
#include "fuel.h"
#include "shared.h"
/******************************** Constants ********************************/
//PMC pallet due to 104in door
// 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))
@ -54,6 +55,7 @@ typedef struct {
double lowerRear;
double leftAux;
double rightAux;
double _ZFWCG; // DO NOT USE
// Additional properties
double empty;
@ -71,6 +73,7 @@ typedef struct {
struct sbPlanned {
double ZFW;
double GW;
double fuel;
unsigned int cargo;
} sbPlanned;
} fPayloadData_t;
@ -92,20 +95,23 @@ typedef struct {
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);
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);
void distribute(fPayloadData_t *const targetPayload, const FuelData_t *const fuel, unsigned int cargo,
const UserData_t *const userData);
// Updates pax stations with their respective weights
// Used internally and used for Station Entry (pax only, cargo is ste directly)
// STATION WEIGHTS ARE NOT NORMALISED TO POUNDS
void generatePayload(fPayloadData_t* const targetPayload, const bool isImperial);
void generatePayload(fPayloadData_t *const targetPayload, const bool isImperial);
// Normalise to Pounds
// For Station Entry: CALL AFTER `generatePayload`
void normalisePayload(fPayloadData_t* const targetPayload, const bool isImperial);
void calculateCGs(const fPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial);
void load(const fPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial);
void 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 HANDLE simConnect, const bool isImperial);
void unloadF(const HANDLE simConnect, const bool isER);

135
PackageSources/wasm-module/fuel.cpp Normal file
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@ -0,0 +1,135 @@
#include "fuel.h"
// ZFW Entry
void distribute(FuelData_t *const targetFuel, const double fuelTarget, const UserData_t *const userData) {
double fuelLbs = TO_POUNDS(userData->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 (userData->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 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, 0, 0, sizeof(FuelDataSet_t),
&localFuel);
}

88
PackageSources/wasm-module/fuel.h Normal file
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@ -0,0 +1,88 @@
#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 ********************************/
#define LBS_PER_GAL 6.699999809
#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
#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 UserData_t *const userData);
void fuel(const FuelData_t *const targetFuel, const HANDLE simConnect);

25
PackageSources/wasm-module/load-manager-cli.cpp
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@ -1,25 +0,0 @@
// load-manager-cli.cpp : This file contains the 'main' function. Program execution begins and ends there.
//
#include "../wasm-module/pax.h"
int main()
{
bool isImperial = false;
bool isER = true;
paxPayloadData_t targetPaxPayloadData = paxPayloadData_t();
targetPaxPayloadData.empty = FROM_POUNDS(isImperial, 283975);
targetPaxPayloadData.pilot = PAX_WEIGHT(isImperial);
targetPaxPayloadData.firstOfficer = PAX_WEIGHT(isImperial);
targetPaxPayloadData.engineer = PAX_WEIGHT(isImperial);
targetPaxPayloadData.cabinCrewFront = FRONT_CREW_WEIGHT(isImperial);
targetPaxPayloadData.cabinCrewRear = REAR_CREW_WEIGHT(isImperial);
targetPaxPayloadData.leftAux = isER ? AUX_WEIGHT(isImperial) : 0;
targetPaxPayloadData.rightAux = isER ? AUX_WEIGHT(isImperial) : 0;
FuelData_t liveFuelData = FuelData_t();
distribute(&targetPaxPayloadData, &liveFuelData, 162000.0, 20.5, isImperial);
}

109
PackageSources/wasm-module/load-manager-cli.vcxproj
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@ -1,109 +0,0 @@
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<Keyword>Win32Proj</Keyword>
<ProjectGuid>{992caf4b-b3f6-4a86-a1c1-663686082c5e}</ProjectGuid>
<RootNamespace>loadmanagercli</RootNamespace>
<WindowsTargetPlatformVersion>10.0</WindowsTargetPlatformVersion>
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<Import Project="$(VCTargetsPath)\Microsoft.Cpp.Default.props" />
<PropertyGroup Condition="'$(Configuration)|$(Platform)'=='Debug|x64'" Label="Configuration">
<ConfigurationType>Application</ConfigurationType>
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<PlatformToolset>v143</PlatformToolset>
<CharacterSet>Unicode</CharacterSet>
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<PlatformToolset>v143</PlatformToolset>
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34
PackageSources/wasm-module/load-manager-cli.vcxproj.filters
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@ -1,34 +0,0 @@
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4
PackageSources/wasm-module/load-manager-cli.vcxproj.user
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604
PackageSources/wasm-module/load-manager.cpp
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34
PackageSources/wasm-module/load-manager.h
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@ -1,45 +1,47 @@
#pragma once
#ifndef __INTELLISENSE__
# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#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__
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
// MSFS headers
#include "rapidjson/filewritestream.h"
#include <MSFS/Legacy/gauges.h>
#include <MSFS/MSFS.h>
#include <MSFS/MSFS_CommBus.h>
#include <MSFS/Legacy/gauges.h>
#include <SimConnect.h>
#include <rapidjson/document.h>
#include <rapidjson/filereadstream.h>
#include "rapidjson/filewritestream.h"
#include <rapidjson/writer.h>
#include <SimConnect.h>
// C headers
#include <string.h>
// C++ headers
#include <ctime>
// Own headers
#include "shared.h"
#include "pax.h"
#include "freighter.h"
#include "fuel.h"
#include "pax.h"
#include "shared.h"
/******************************** Constants ********************************/
// Module identification
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
#define VERSION_STRING "1.6"
#define VERSION_STRING "2.9-beta"
// 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 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);
void log(FILE* file, const char* format, void* optionalElement = NULL);
void CALLBACK MyDispatchProc(SIMCONNECT_RECV *pData, DWORD cbData, void *pContext);
void log(FILE *file, const char *format, void *optionalElement = NULL);

12
PackageSources/wasm-module/load-manager.sln
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@ -5,28 +5,16 @@ 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
Project("{8BC9CEB8-8B4A-11D0-8D11-00A0C91BC942}") = "load-manager-cli", "load-manager-cli.vcxproj", "{992CAF4B-B3F6-4A86-A1C1-663686082C5E}"
EndProject
Global
GlobalSection(SolutionConfigurationPlatforms) = preSolution
Debug|MSFS = Debug|MSFS
Debug|x64 = Debug|x64
Release|MSFS = Release|MSFS
Release|x64 = Release|x64
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}.Debug|x64.ActiveCfg = Debug|x64
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.ActiveCfg = Release|MSFS
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|MSFS.Build.0 = Release|MSFS
{A5468B35-BBBD-4C55-97ED-81BFE343B0E4}.Release|x64.ActiveCfg = Release|MSFS
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|MSFS.ActiveCfg = Debug|x64
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|x64.ActiveCfg = Debug|x64
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Debug|x64.Build.0 = Debug|x64
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|MSFS.ActiveCfg = Release|x64
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|x64.ActiveCfg = Release|x64
{992CAF4B-B3F6-4A86-A1C1-663686082C5E}.Release|x64.Build.0 = Release|x64
EndGlobalSection
GlobalSection(SolutionProperties) = preSolution
HideSolutionNode = FALSE

2
PackageSources/wasm-module/load-manager.vcxproj
View File

@ -288,12 +288,14 @@ Powershell.exe -File .\copy-release.ps1</Command>
<ClCompile Include="freighter.cpp" />
<ClCompile Include="load-manager.cpp" />
<ClCompile Include="pax.cpp" />
<ClCompile Include="fuel.cpp" />
</ItemGroup>
<ItemGroup>
<ClInclude Include="freighter.h" />
<ClInclude Include="load-manager.h" />
<ClInclude Include="pax.h" />
<ClInclude Include="shared.h" />
<ClInclude Include="fuel.h" />
</ItemGroup>
<Import Project="$(VCTargetsPath)\Microsoft.Cpp.targets" />
<ImportGroup Label="ExtensionTargets">

162
PackageSources/wasm-module/pax.cpp
View File

@ -1,24 +1,26 @@
#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) {
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;
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));
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) {
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->paxCount.business1 = targetPayload->paxCount.business2 = targetPayload->paxCount.economy1 =
targetPayload->paxCount.economy2 = targetPayload->paxCount.total = 0;
targetPayload->forwardCargo = targetPayload->rearCargo = 0;
unsigned short _numPax = 0;
@ -42,8 +44,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
targetPayload->paxCount.economy2++;
_numPax++;
}
}
else if (numPax == 3) {
} else if (numPax == 3) {
if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
targetPayload->paxCount.business2++;
_numPax++;
@ -56,8 +57,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
targetPayload->paxCount.economy2++;
_numPax++;
}
}
else if (numPax == 2) {
} else if (numPax == 2) {
if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
targetPayload->paxCount.economy1++;
_numPax++;
@ -66,8 +66,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
targetPayload->paxCount.economy2++;
_numPax++;
}
}
else if (numPax == 1) {
} else if (numPax == 1) {
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
targetPayload->paxCount.economy2++;
_numPax++;
@ -79,8 +78,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
if (_numPax % 2 == 0) {
targetPayload->forwardCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
targetPayload->rearCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
}
else {
} else {
_numPax--;
targetPayload->forwardCargo += (_numPax / 2 + 1) * BAG_WEIGHT(userData->isImperial, userOptions);
targetPayload->rearCargo += (_numPax / 2) * BAG_WEIGHT(userData->isImperial, userOptions);
@ -91,7 +89,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
count--;
}
count = MAX_FRONT_CARGO(userData->isImperial);
// Initial distibution of remaining cargo
// Initial distribution of remaining cargo
while (cargo > 0 && count > 0) {
if (targetPayload->forwardCargo < MAX_FRONT_CARGO(userData->isImperial)) {
targetPayload->forwardCargo++;
@ -114,33 +112,27 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
while (count > 0) {
generatePayload(targetPayload, userData->isImperial, userOptions);
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, userData->isImperial);
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) {
} else if (targetPayload->paxCount.business2 > minBusiness2) {
targetPayload->paxCount.business2--;
}
else if (targetPayload->paxCount.economy1 > minEconomy1) {
} else if (targetPayload->paxCount.economy1 > minEconomy1) {
targetPayload->paxCount.economy1--;
}
else {
} else {
break;
}
if (targetPayload->paxCount.economy2 < MAX_ECONOMY_2) {
targetPayload->paxCount.economy2++;
}
else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
} else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
targetPayload->paxCount.economy1++;
}
else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
} else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
targetPayload->paxCount.business2++;
}
else {
} else {
targetPayload->paxCount.business1++;
}
}
@ -148,31 +140,24 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
else if (targetPayload->ZFWCG > targetPayload->CGTarget + CG_TOLERANCE) {
if (targetPayload->paxCount.economy2 > minEconomy2) {
targetPayload->paxCount.economy2--;
}
else if (targetPayload->paxCount.economy1 > minEconomy1) {
} else if (targetPayload->paxCount.economy1 > minEconomy1) {
targetPayload->paxCount.economy1--;
}
else if (targetPayload->paxCount.business2 > minBusiness2) {
} else if (targetPayload->paxCount.business2 > minBusiness2) {
targetPayload->paxCount.business2--;
}
else {
} else {
break;
}
if (targetPayload->paxCount.business1 < MAX_BUSINESS_1) {
targetPayload->paxCount.business1++;
}
else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
} else if (targetPayload->paxCount.business2 < MAX_BUSINESS_2) {
targetPayload->paxCount.business2++;
}
else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
} else if (targetPayload->paxCount.economy1 < MAX_ECONOMY_1) {
targetPayload->paxCount.economy1++;
}
else {
} else {
targetPayload->paxCount.economy2++;
}
}
else {
} else {
break;
}
@ -182,7 +167,7 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
count = MAX_FRONT_CARGO(userData->isImperial) + MAX_REAR_CARGO(userData->isImperial, userData->isER);
while (count > 0) {
generatePayload(targetPayload, userData->isImperial, userOptions);
calculateCGs(targetPayload, fuel, &targetPayload->ZFWCG, &targetPayload->TOCG, userData->isImperial);
calculateCGs(targetPayload, fuel, userData->isImperial);
// in front of target
if (targetPayload->ZFWCG < targetPayload->CGTarget - CG_TOLERANCE) {
@ -191,13 +176,11 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
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 {
} else {
targetPayload->forwardCargo--;
targetPayload->rearCargo++;
}
}
else {
} else {
break;
}
}
@ -205,20 +188,18 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
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->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 {
} else {
targetPayload->rearCargo--;
targetPayload->forwardCargo++;
}
}
else {
} else {
break;
}
}
else {
} else {
break;
}
@ -228,22 +209,28 @@ void distribute(paxPayloadData_t* const targetPayload, const FuelData_t* const f
// 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;
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) {
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);
@ -268,12 +255,13 @@ void normalisePayload(paxPayloadData_t* const targetPayload, const bool isImperi
targetPayload->rightAux = TO_POUNDS(isImperial, targetPayload->rightAux);
}
void calculateCGs(const paxPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial) {
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 +
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 +
@ -284,13 +272,15 @@ void calculateCGs(const paxPayloadData_t* const targetPayload, const FuelData_t*
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;
double totalWeight = localPayload.empty + localPayload.pilot + localPayload.firstOfficer + localPayload.engineer +
localPayload.cabinCrewFront + localPayload.business1Left + localPayload.business1Center +
localPayload.business1Right + localPayload.business2Left + localPayload.business2Center +
localPayload.business2Right + localPayload.economy1Left + localPayload.economy1Center +
localPayload.economy1Right + localPayload.economy2Left + localPayload.economy2Center +
localPayload.economy2Right + localPayload.cabinCrewRear + localPayload.forwardCargo +
localPayload.rearCargo + localPayload.leftAux + localPayload.rightAux;
*ZFWCG = TO_PERCENT_MAC(totalMoment / totalWeight);
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 +
@ -298,32 +288,38 @@ void calculateCGs(const paxPayloadData_t* const targetPayload, const FuelData_t*
totalWeight += fuel->total;
*TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
targetPayload->TOCG = TO_PERCENT_MAC(totalMoment / totalWeight);
}
void load(const paxPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial) {
void load(const paxPayloadData_t *const targetPayload, const HANDLE simConnect, const bool isImperial) {
paxPayloadData_t localPayload = {};
memcpy(&localPayload, targetPayload, sizeof(localPayload));
normalisePayload(&localPayload, isImperial);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(paxPayloadDataSet_t), &localPayload);
localPayload._ZFWCG = localPayload.ZFWCG / 100.0;
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0,
sizeof(paxPayloadDataSet_t), &localPayload);
}
void unload(const HANDLE simConnect, const bool isER) {
paxPayloadDataSet_t localPayload = {};
paxPayloadData_t localPayload = {};
localPayload.cabinCrewFront = FRONT_CREW_WEIGHT(true);
localPayload.cabinCrewRear = REAR_CREW_WEIGHT(true);
localPayload.leftAux = localPayload.rightAux = isER ? AUX_WEIGHT(true) : 0;
localPayload.pilot = localPayload.firstOfficer = localPayload.engineer = PILOT_WEIGHT(true);
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0, sizeof(paxPayloadDataSet_t), &localPayload);
localPayload._ZFWCG = -1;
SimConnect_SetDataOnSimObject(simConnect, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, 0, 0,
sizeof(paxPayloadDataSet_t), &localPayload);
}
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t* const options) {
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t *const options) {
return (isImperial) ? (options->paxWeightLBS) : (options->paxWeightKG);
}
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t* const options) {
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t *const options) {
return (isImperial) ? (options->bagWeightLBS) : (options->bagWeightKG);
}

40
PackageSources/wasm-module/pax.h
View File

@ -1,13 +1,13 @@
#pragma once
#ifndef __INTELLISENSE__
# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#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__
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/********************************* Headers *********************************/
@ -19,6 +19,7 @@
// C++ headers
#include <algorithm>
// Own headers
#include "fuel.h"
#include "shared.h"
/******************************** Constants ********************************/
@ -81,6 +82,7 @@ typedef struct {
double rearCargo;
double leftAux;
double rightAux;
double _ZFWCG; // DO NOT USE
// Additional properties
double empty;
@ -98,6 +100,7 @@ typedef struct {
struct sbPlanned {
double ZFW;
double GW;
double fuel;
unsigned short pax;
unsigned int cargo;
} sbPlanned;
@ -125,26 +128,27 @@ typedef struct {
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);
// 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);
void generatePayload(paxPayloadData_t *const targetPayload, const bool isImperial, const UserOptions_t *const userOptions);
// Normalise to Pounds
// For Station Entry: CALL AFTER `generatePayload`
void normalisePayload(paxPayloadData_t* const targetPayload, const bool isImperial);
void calculateCGs(const paxPayloadData_t* const targetPayload, const FuelData_t* const fuel, double* const ZFWCG, double* const TOCG, const bool isImperial);
void load(const paxPayloadData_t* const targetPayload, const HANDLE simConnect, const bool isImperial);
void 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 HANDLE simConnect, const bool isImperial);
void unload(const HANDLE simConnect, const bool isER);
// Based on ICAO/LH findings
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t* const options);
const double PAX_WEIGHT(const bool isImperial, const UserOptions_t *const options);
// Based on ICAO/LH findings
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t* const options);
const double BAG_WEIGHT(const bool isImperial, const UserOptions_t *const options);

58
PackageSources/wasm-module/shared.h
View File

@ -1,13 +1,13 @@
#pragma once
#ifndef __INTELLISENSE__
# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
#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__
#define MODULE_EXPORT
#define MODULE_WASM_MODNAME(mod)
#define __attribute__(x)
#define __restrict__
#endif
/******************************** Constants ********************************/
@ -15,18 +15,15 @@
#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
// 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
// LD3s due to 70in door, ER option takes up two slots
#define MAX_REAR_CARGO(IS_IMPERIAL, IS_ER) ((IS_IMPERIAL) ? ((IS_ER ? 12.0 : 14.0) * 3500.0) : ((IS_ER ? 12.0 : 14.0) * 1588.0))
// Max TOW
#define MAX_TOW(IS_IMPERIAL) ((IS_IMPERIAL) ? (625500) : (283722))
#define MAX_TOW_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (630500) : (285990))
// Max Fuel
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
// Arms Shared
#define ARM_EMPTY -159.6
#define ARM_EMPTY -120.0
#define ARM_PILOT 984.0
#define ARM_FIRST_OFFICER 984.0
#define ARM_ENGINEER 960.0
@ -34,22 +31,11 @@
#define ARM_REAR_CARGO -360.0
#define ARM_LEFT_AUX 60.0
#define ARM_RIGHT_AUX 60.0
// Arms Fuel
#define ARM_MAIN1 -240.0
#define ARM_MAIN3 -240.0
#define ARM_MAIN2 120.0
#define ARM_UPPER_AUX 0.0
#define ARM_LOWER_AUX 0.0
#define ARM_MAIN1_TIP -468.0
#define ARM_MAIN3_TIP -468.0
#define ARM_TAIL -840.0
#define ARM_FORWARD_AUX1 60.0
#define ARM_FORWARD_AUX2 60.0
// MAC
#define ROOT_CHORD 34.68
#define WING_SPAN 170.5
#define WING_AREA 3648.0
#define QUARTER_MAC -165.0 //aero_center
#define 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)
@ -64,10 +50,10 @@
/********************************* Macros **********************************/
// Conversions
#define TO_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE) * 2.20462262185)
#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)
#define TO_PERCENT_MAC(POS) ((((POS)-LEMAC) / MAC) * -100.0)
/********************************** ENUMS **********************************/
enum DATA_DEFINITIONS {
@ -75,6 +61,7 @@ enum DATA_DEFINITIONS {
DATA_DEFINITION_PAYLOAD_PAX,
DATA_DEFINITION_PAYLOAD_F,
DATA_DEFINITION_FUEL,
DATA_DEFINITION_FUEL_SET,
DATA_DEFINITION_GSX,
DATA_DEFINITION_USER_DATA,
};
@ -84,6 +71,7 @@ enum DATA_REQUESTS {
DATA_REQUEST_PAYLOAD_PAX,
DATA_REQUEST_PAYLOAD_F,
DATA_REQUEST_FUEL,
DATA_REQUEST_FUEL_SET,
DATA_REQUEST_GSX,
DATA_REQUEST_USER_DATA,
};
@ -127,24 +115,6 @@ typedef struct {
enum LOADING_STATES loadingState;
} GSXData_t;
typedef struct {
// SimConnect mapped
double poundsPerGallon; // DO NOT USE
double main1;
double main3;
double main2;
double upperAux;
double lowerAux;
double main1Tip;
double main3Tip;
double tail;
double forwardAux1;
double forwardAux2;
// Additional properties
double total;
} FuelData_t;
typedef struct {
bool GSXSync;
double paxWeightKG;

20
TODO.md Normal file
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@ -0,0 +1,20 @@
Fuel (once implemented)
ZFWCG for WBS (once implemented) `MD11_EXTCTL_WBS_ZFWCG`
https://discord.com/channels/589851727373795331/1165358675037270066/1469039399961497753
Fuel Schedule
Mains 1/2/3
Upper Aux
Lower Aux
Tail
LEft/Right Forward Aux
Fuel Limits from EFB
GSX Sync
When Fueling is called, fuel progressively using FuelDataSet_t and FUEL_SET enums
Find fueling rate of plane
In JS
Remove Set Fuel
Fuel is set with total load button

2
copy-debug.ps1
View File

@ -1 +1 @@
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel

2
copy-release.ps1
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@ -1 +1 @@
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel

4
package.json
View File

@ -1,4 +1,8 @@
{
"scripts": {
"debugger": "cd \"$env:MSFS_SDK/Tools/CoherentGT Debugger\" && ./Debugger.exe",
"locale": "cd \"$env:MSFS_SDK/Tools/MSFS_Localization\" && ./MSFSLocalizationManager.exe"
},
"devDependencies": {
"diff": "^8.0.2"
}

18
xkhofmann-tfdidesign-md11-load-manager.code-workspace
View File

@ -6,12 +6,30 @@
],
"settings": {
"cSpell.words": [
"AUXLWR",
"AUXUPR",
"bksp",
"couatl",
"Deboarded",
"DEBOARDED",
"deboarding",
"Deinitialized",
"EXTCTL",
"FCOMs",
"FSDT",
"FWDAUXL",
"FWDAUXR",
"HRESULT",
"khofmann",
"LEMAC",
"MSFS",
"NUMPASSENGERS",
"SIMCONNECT",
"SIMOBJECT",
"SIMOBJECTS",
"tfdi",
"TFDI",
"tfdidesign",
"TOCG",
"ZFWCG"
]

9
xkhofmann-tfdidesign-md11-load-manager.xml.user Normal file
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@ -0,0 +1,9 @@
<UserSettings>
<CheckedOutPackages>
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
</CheckedOutPackages>
<SelectedPackages/>
<Filter/>
<ShowOnlyEdited>false</ShowOnlyEdited>
</UserSettings>