TFDi_MD-11_QA/xkhofmann-tfdidesign-md11-load-manager
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TFDi_MD-11_QA:2024
TFDi_MD-11_QA:Panel
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TFDi_MD-11_QA:2024
TFDi_MD-11_QA:master
TFDi_MD-11_QA:Panel

6 Commits
master ... 2024

Author SHA1 Message Date
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
19 changed files with 1891 additions and 186 deletions
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23
EFB/efb-js.patch
View File

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

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

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

92
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_GE/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/tfdi-design/TFDi_Design_MD-11 GE LOW/config/flight_model.cfg
View File

@ -1,9 +1,9 @@
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25 //TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 1 minor = 2
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
@ -24,21 +24,21 @@ station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2 station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0 station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0 station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0 station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0 station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0 station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0 station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0 station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0 station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0 station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0 station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0 station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0 station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0 station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0 station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0 station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0 station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0 station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0 station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0 station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
//KH END //KH END
@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889 drag_coef_flaps = 0.0789
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -319,19 +319,19 @@ max_gear_extended = 200
[INTERACTIVE POINTS] [INTERACTIVE POINTS]
number_of_interactive_points = 13 number_of_interactive_points = 13
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0 interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33 interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0 interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0 interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0 interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0 interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0 interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33 interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,0 interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,0 interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,0 interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,0 interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,0 interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
[STALL PROTECTION] [STALL PROTECTION]
stall_protection = 1 ; Alpha Protection stall_protection = 1 ; Alpha Protection
@ -348,8 +348,8 @@ type = 1
system_type = 1 system_type = 1
span-outboard = 0.25 span-outboard = 0.25
extending-time = 22 extending-time = 22
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -357,12 +357,12 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.1] [FLAPS.1]
@ -370,8 +370,8 @@ type = 1
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 23 extending-time = 23
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -379,12 +379,12 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.2] [FLAPS.2]
@ -392,8 +392,8 @@ type = 2
system_type = 1 system_type = 1
span-outboard = 0.2 span-outboard = 0.2
extending-time = 8 extending-time = 8
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75
@ -407,8 +407,8 @@ type = 2
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 21 extending-time = 21
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75

418
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/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) vRC1.7.1_GE 24JAN26
[VERSION]
//KH Bump major
major = 4
minor = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 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 = 1.32645
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, 1917.00, 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
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 = 0.0789
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
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, 0.54, 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, 0.54, 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

95
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11_PW/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/tfdi-design/TFDi_Design_MD-11 PW LOW/config/flight_model.cfg
View File

@ -1,9 +1,12 @@
//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25 ; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 1 minor = 2
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
@ -24,21 +27,21 @@ station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2 station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0 station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0 station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0 station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0 station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0 station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0 station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0 station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0 station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0 station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0 station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0 station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0 station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0 station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0 station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0 station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0 station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0 station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0 station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0 station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
//KH END //KH END
@ -175,7 +178,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889 drag_coef_flaps = 0.0789
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -319,19 +322,19 @@ max_gear_extended = 200
[INTERACTIVE POINTS] [INTERACTIVE POINTS]
number_of_interactive_points = 13 number_of_interactive_points = 13
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0 interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33 interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0 interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0 interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0 interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0 interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0 interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33 interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,0 interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-1
interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,0 interactive_point.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-1
interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,0 interactive_point.10 = 0.4,-2.869313,10.049908,-0.566572,0,0,0,90,35,0,35,0,2,33,-1
interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,0 interactive_point.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-1
interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,0 interactive_point.12 = 0.4,-62.995712,8.519092,-0.565611,0,0,0,100,35,0,35,0,2,33,-1
[STALL PROTECTION] [STALL PROTECTION]
stall_protection = 1 ; Alpha Protection stall_protection = 1 ; Alpha Protection
@ -348,8 +351,8 @@ type = 1
system_type = 1 system_type = 1
span-outboard = 0.25 span-outboard = 0.25
extending-time = 22 extending-time = 22
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -357,20 +360,20 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 23 extending-time = 23
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -378,20 +381,20 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2
system_type = 1 system_type = 1
span-outboard = 0.2 span-outboard = 0.2
extending-time = 8 extending-time = 8
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75
@ -405,8 +408,8 @@ type = 2
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 21 extending-time = 21
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75

419
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/tfdi-design/TFDi_Design_MD-11 PW/config/flight_model.cfg Normal file
View File

@ -0,0 +1,419 @@
; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 283975
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 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 = 1.32645
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, 1917.00, 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
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 = 0.0789
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
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, 0.54, 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, 0.54, 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

64
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/tfdi-design/TFDi_Design_MD-11F GE LOW/config/flight_model.cfg
View File

@ -1,9 +1,12 @@
//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25 ; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 1 minor = 2
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
@ -20,9 +23,9 @@ activate_mach_limit_based_on_cg = 0
activate_cg_limit_based_on_mach = 0 activate_cg_limit_based_on_mach = 0
max_number_of_stations = 15 max_number_of_stations = 15
//KH START Empty default //KH START Empty default
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1 station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2 station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0 station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0 station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0 station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0 station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889 drag_coef_flaps = 0.0789
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -313,14 +316,14 @@ max_gear_extended = 200
[INTERACTIVE POINTS] [INTERACTIVE POINTS]
number_of_interactive_points = 8 number_of_interactive_points = 8
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0 interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33 interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0 interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0 interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0 interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0 interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0 interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0 interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
[STALL PROTECTION] [STALL PROTECTION]
stall_protection = 1 ; Alpha Protection stall_protection = 1 ; Alpha Protection
@ -337,8 +340,8 @@ type = 1
system_type = 1 system_type = 1
span-outboard = 0.25 span-outboard = 0.25
extending-time = 22 extending-time = 22
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -346,20 +349,21 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 23 extending-time = 23
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -367,20 +371,20 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2
system_type = 1 system_type = 1
span-outboard = 0.2 span-outboard = 0.2
extending-time = 8 extending-time = 8
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75
@ -394,8 +398,8 @@ type = 2
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 21 extending-time = 21
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75

409
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/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) vRC1.7.1_GE_F 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 248567
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 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 = 1.32645
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, 1917.00, 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
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 = 0.0789
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
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, 0.54, 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, 0.54, 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

63
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_PW/flight_model.cfg → PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/tfdi-design/TFDi_Design_MD-11F PW LOW/config/flight_model.cfg
View File

@ -1,9 +1,12 @@
//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25 ; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 1 minor = 2
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
@ -20,9 +23,9 @@ activate_mach_limit_based_on_cg = 0
activate_cg_limit_based_on_mach = 0 activate_cg_limit_based_on_mach = 0
max_number_of_stations = 15 max_number_of_stations = 15
//KH START Empty default //KH START Empty default
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1 station_load.0=190.0, 82.0, -2.0, 4.0, Pilot, 1
station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2 station_load.1=190.0, 82.0, 2.0, 4.0, First Officer, 2
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0 station_load.2=190.0, 80.0, 3.3, 4.0, Engineer, 0
station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0 station_load.3=0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0 station_load.4=0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0 station_load.5=0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
@ -169,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.1889 drag_coef_flaps = 0.0789
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -313,14 +316,14 @@ max_gear_extended = 200
[INTERACTIVE POINTS] [INTERACTIVE POINTS]
number_of_interactive_points = 8 number_of_interactive_points = 8
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0 interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,-1
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33 interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0 interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,0 interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-1
interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0 interactive_point.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,-1
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,0 interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-1
interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,0 interactive_point.6 = 0,85.062134,3.882079,4.412694,2,-0,29.85655,-42.814491,0,0,0,0,0,0,-1
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0 interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
[STALL PROTECTION] [STALL PROTECTION]
stall_protection = 1 ; Alpha Protection stall_protection = 1 ; Alpha Protection
@ -337,8 +340,8 @@ type = 1
system_type = 1 system_type = 1
span-outboard = 0.25 span-outboard = 0.25
extending-time = 22 extending-time = 22
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -346,20 +349,20 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 23 extending-time = 23
damaging-speed = 250 damaging-speed = 280
blowout-speed = 300 blowout-speed = 310
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.1 lift_scalar = 0.1
drag_scalar = 1.1 drag_scalar = 1.1
@ -367,20 +370,20 @@ pitch_scalar = 1
max_on_ground_position = 7 max_on_ground_position = 7
flaps-position.0 = 0, -1, 0 flaps-position.0 = 0, -1, 0
flaps-position.1 = 0, -1, 0 flaps-position.1 = 0, -1, 0
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1 flaps-position.2 = 15, 215, 0.45, 2, 0, 0, 0, 1
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1 flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.28, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 150, 0.33, 1 flaps-position.7 = 50, 155, 0.54, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2
system_type = 1 system_type = 1
span-outboard = 0.2 span-outboard = 0.2
extending-time = 8 extending-time = 8
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75
@ -394,8 +397,8 @@ type = 2
system_type = 1 system_type = 1
span-outboard = 0.7 span-outboard = 0.7
extending-time = 21 extending-time = 21
damaging-speed = 250 damaging-speed = 300
blowout-speed = 300 blowout-speed = 330
maneuvering_flaps = 0 maneuvering_flaps = 0
lift_scalar = 0.5 lift_scalar = 0.5
drag_scalar = 0.75 drag_scalar = 0.75

408
PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11/preset/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) vRC1.7.1_PW_F 24JAN26
[MODULAR_MERGE]
auto = true
[VERSION]
//KH Bump major
major = 4
minor = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 630500
empty_weight = 248567
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 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 = 1.32645
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, 1917.00, 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
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 = 0.0789
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
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, 0.54, 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, 0.54, 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
View File

@ -1,6 +1,6 @@
{ {
"name": "tfdidesign-md11-load-manager", "name": "tfdidesign-md11-load-manager",
"version": "0.1.186", "version": "0.1.187",
"description": "", "description": "",
"main": "index.js", "main": "index.js",
"type": "module", "type": "module",

35
PackageSources/wasm-module/load-manager.cpp
View File

@ -356,32 +356,32 @@ extern "C" MSFS_CALLBACK void module_init(void) {
log(stdout, "Data definitions created.\n"); log(stdout, "Data definitions created.\n");
// SimConnect Requests // SimConnect Requests
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_EMPTY_WEIGHT, DATA_DEFINITION_EMPTY_WEIGHT, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_EMPTY_WEIGHT, DATA_DEFINITION_EMPTY_WEIGHT, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request empty weight, terminating.\n"); log(stderr, "Could not request empty weight, terminating.\n");
return; return;
} }
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_PAX, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_PAX, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request payload pax, terminating.\n"); log(stderr, "Could not request payload pax, terminating.\n");
return; return;
} }
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_F, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_F, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request payload f, terminating.\n"); log(stderr, "Could not request payload f, terminating.\n");
return; return;
} }
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_FUEL, DATA_DEFINITION_FUEL, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_FUEL, DATA_DEFINITION_FUEL, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request fuel, terminating.\n"); log(stderr, "Could not request fuel, terminating.\n");
return; return;
} }
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_GSX, DATA_DEFINITION_GSX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_GSX, DATA_DEFINITION_GSX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request GSX, terminating.\n"); log(stderr, "Could not request GSX, terminating.\n");
return; return;
} }
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_USER_DATA, DATA_DEFINITION_USER_DATA, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_SECOND); hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_USER_DATA, DATA_DEFINITION_USER_DATA, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
if (hr != S_OK) { if (hr != S_OK) {
log(stderr, "Could not request user data, terminating.\n"); log(stderr, "Could not request user data, terminating.\n");
return; return;
@ -924,6 +924,12 @@ void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContex
liveFPayloadData->lowerForward + liveFPayloadData->lowerRear + liveFPayloadData->leftAux + liveFPayloadData->lowerForward + liveFPayloadData->lowerRear + liveFPayloadData->leftAux +
liveFPayloadData->rightAux; liveFPayloadData->rightAux;
if (UserData->isCargo && AircraftLoaded && abs(liveFPayloadData->total - TO_POUNDS(UserData->isImperial, targetFPayloadData->total)) > 100) {
log(stdout, "F AC loaded, Payload mismatch, resetting target\n");
load(targetFPayloadData, simConnect, UserData->isImperial);
}
break; break;
} }
case DATA_REQUEST_PAYLOAD_PAX: { case DATA_REQUEST_PAYLOAD_PAX: {
@ -939,6 +945,15 @@ void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContex
livePaxPayloadData->forwardCargo + livePaxPayloadData->rearCargo + livePaxPayloadData->leftAux + livePaxPayloadData->forwardCargo + livePaxPayloadData->rearCargo + livePaxPayloadData->leftAux +
livePaxPayloadData->rightAux; livePaxPayloadData->rightAux;
double curr = livePaxPayloadData->total;
double target = TO_POUNDS(UserData->isImperial, targetPaxPayloadData->total);
double diff = livePaxPayloadData->total - TO_POUNDS(UserData->isImperial, targetPaxPayloadData->total);
if (!UserData->isCargo && AircraftLoaded && abs(livePaxPayloadData->total - TO_POUNDS(UserData->isImperial, targetPaxPayloadData->total)) > 100) {
log(stdout, "PAX AC loaded, Payload mismatch, resetting target\n");
load(targetPaxPayloadData, simConnect, UserData->isImperial);
}
break; break;
} }
case DATA_REQUEST_FUEL: { case DATA_REQUEST_FUEL: {
@ -974,6 +989,8 @@ void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContex
case GSX_SERVICE_ACTIVE: { case GSX_SERVICE_ACTIVE: {
GSXData->loadingState = LOADING_STATE_BOARDING; GSXData->loadingState = LOADING_STATE_BOARDING;
AircraftLoaded = false;
double cargoBoarded = GSXData->cargoBoarded; double cargoBoarded = GSXData->cargoBoarded;
if (UserData->isCargo) { if (UserData->isCargo) {
fPayloadData_t localPayload = {}; fPayloadData_t localPayload = {};
@ -1014,6 +1031,8 @@ void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContex
case GSX_SERVICE_FINISHED: { case GSX_SERVICE_FINISHED: {
GSXData->loadingState = LOADING_STATE_BOARDED; GSXData->loadingState = LOADING_STATE_BOARDED;
AircraftLoaded = true;
if (UserData->isCargo) { if (UserData->isCargo) {
fPayloadData_t localPayload = {}; fPayloadData_t localPayload = {};
memcpy(&localPayload, targetFPayloadData, sizeof(localPayload)); memcpy(&localPayload, targetFPayloadData, sizeof(localPayload));
@ -1037,10 +1056,12 @@ void CALLBACK MyDispatchProc(SIMCONNECT_RECV* pData, DWORD cbData, void* pContex
switch ((char)GSXData->deboardingState) { switch ((char)GSXData->deboardingState) {
case GSX_SERVICE_ACTIVE: { case GSX_SERVICE_ACTIVE: {
// Exit if not boarded // Exit if not boarded
if (GSXData->loadingState != LOADING_STATE_BOARDED) break; if (GSXData->loadingState != LOADING_STATE_BOARDED && GSXData->loadingState != LOADING_STATE_DEBOARDING) break;
GSXData->loadingState = LOADING_STATE_DEBOARDING; GSXData->loadingState = LOADING_STATE_DEBOARDING;
AircraftLoaded = false;
double cargoDeboarded = GSXData->cargoDeboarded; double cargoDeboarded = GSXData->cargoDeboarded;
if (UserData->isCargo) { if (UserData->isCargo) {
fPayloadData_t localPayload = {}; fPayloadData_t localPayload = {};

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

@ -32,7 +32,7 @@
/******************************** Constants ********************************/ /******************************** Constants ********************************/
// Module identification // Module identification
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] " #define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
#define VERSION_STRING "1.6" #define VERSION_STRING "1.14"
// COMM BUS // COMM BUS
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data" #define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target" #define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"

2
copy-debug.ps1
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@ -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
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@ -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": { "devDependencies": {
"diff": "^8.0.2" "diff": "^8.0.2"
} }

2
xkhofmann-tfdidesign-md11-load-manager.code-workspace
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@ -10,8 +10,10 @@
"DEBOARDED", "DEBOARDED",
"deboarding", "deboarding",
"khofmann", "khofmann",
"SIMOBJECTS",
"tfdi", "tfdi",
"TFDI", "TFDI",
"tfdidesign",
"TOCG", "TOCG",
"ZFWCG" "ZFWCG"
] ]

11
xkhofmann-tfdidesign-md11-load-manager.xml.user Normal file
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@ -0,0 +1,11 @@
<UserSettings>
<CheckedOutPackages>
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
</CheckedOutPackages>
<SelectedPackages>
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
</SelectedPackages>
<Filter/>
<ShowOnlyEdited>false</ShowOnlyEdited>
</UserSettings>