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@ -2,26 +2,23 @@ Index: EFB.js
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===================================================================
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===================================================================
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||||||
--- EFB.js
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--- EFB.js
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+++ EFB.js
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+++ EFB.js
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||||||
@@ -40265,11 +40265,11 @@
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@@ -30203,9 +30203,9 @@
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),
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{
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/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
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className: "middle none center rounded-lg bg-green-700 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none",
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"button",
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"data-ripple-light": "true",
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{
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onClick: () => getOutput(),
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- onClick: loadPayload,
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- children: "Set Payload"
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+ onClick: () => dispatch(setRoute({ path: "/payload" })),
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+ children: "Manage Payload"
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className: "middle none center rounded-lg bg-green-700 px-6 py-3 font-sans text-xs font-bold uppercase text-white shadow-md shadow-green-500/20 transition-all hover:shadow-lg hover:shadow-green-500/40 focus:opacity-[0.85] focus:shadow-none active:opacity-[0.85] active:shadow-none disabled:pointer-events-none disabled:opacity-50 disabled:shadow-none",
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}
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- children: "Set payload & fuel"
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) }) })
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+ children: "Manage payload & fuel"
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] }) }) });
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}
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}
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),
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@@ -40556,8 +40556,27 @@
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/* @__PURE__ */ (0, import_jsx_runtime13.jsx)(
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"button",
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@@ -40767,8 +40767,27 @@
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] })
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] })
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] }) }) });
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] }) }) });
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}
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}
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+// Exports for add. script
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+ // Exports for add. script
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+ window.reactExports = __toESM(require_react());
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+ window.reactExports = __toESM(require_react());
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+ window.reactDomExports = __toESM(require_react_dom());
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+ window.reactDomExports = __toESM(require_react_dom());
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+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
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+ window.jsxRuntimeExports = __toESM(require_jsx_runtime());
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@ -1,5 +1,5 @@
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<?xml version="1.0" encoding="utf-8"?>
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<?xml version="1.0" encoding="utf-8"?>
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<AssetPackage Version="1.1.0">
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<AssetPackage Version="0.1.0">
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||||||
<ItemSettings>
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<ItemSettings>
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<ContentType>MISC</ContentType>
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<ContentType>MISC</ContentType>
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<Title>TFDi Design MD-11 Load Manager</Title>
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<Title>TFDi Design MD-11 Load Manager</Title>
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@ -10,10 +10,9 @@
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<VisibleInStore>false</VisibleInStore>
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<VisibleInStore>false</VisibleInStore>
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||||||
<CanBeReferenced>false</CanBeReferenced>
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<CanBeReferenced>false</CanBeReferenced>
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</Flags>
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</Flags>
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||||||
<PackageOrderHint>CUSTOM_SIMOBJECTS_PATCH</PackageOrderHint>
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||||||
<AssetGroups>
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<AssetGroups>
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||||||
<AssetGroup Name="ContentInfo">
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<AssetGroup Name="ContentInfo">
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||||||
<Type Version="0">ContentInfo</Type>
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<Type>ContentInfo</Type>
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||||||
<Flags>
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<Flags>
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||||||
<FSXCompatibility>false</FSXCompatibility>
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<FSXCompatibility>false</FSXCompatibility>
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</Flags>
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</Flags>
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@ -21,7 +20,7 @@
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<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
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<OutputDir>ContentInfo\xkhofmann-tfdidesign-md11-load-manager\</OutputDir>
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||||||
</AssetGroup>
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</AssetGroup>
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||||||
<AssetGroup Name="html-ui">
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<AssetGroup Name="html-ui">
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||||||
<Type Version="0">Copy</Type>
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<Type>Copy</Type>
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||||||
<Flags>
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<Flags>
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||||||
<FSXCompatibility>false</FSXCompatibility>
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<FSXCompatibility>false</FSXCompatibility>
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||||||
</Flags>
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</Flags>
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@ -32,7 +31,7 @@
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</Config>
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</Config>
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</AssetGroup>
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</AssetGroup>
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||||||
<AssetGroup Name="md-11-panel-config">
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<AssetGroup Name="md-11-panel-config">
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||||||
<Type Version="0">Copy</Type>
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<Type>Copy</Type>
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||||||
<Flags>
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<Flags>
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||||||
<FSXCompatibility>false</FSXCompatibility>
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<FSXCompatibility>false</FSXCompatibility>
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||||||
</Flags>
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</Flags>
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@ -41,3 +40,4 @@
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</AssetGroup>
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</AssetGroup>
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||||||
</AssetGroups>
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</AssetGroups>
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||||||
</AssetPackage>
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</AssetPackage>
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@ -1,418 +0,0 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26
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[VERSION]
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||||||
//KH Bump major
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major = 4
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minor = 2
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[WEIGHT_AND_BALANCE]
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max_gross_weight = 630500
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empty_weight = 283975
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reference_datum_position = 0, 0, 0
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empty_weight_CG_position = -13.3, 0, 0
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||||||
CG_forward_limit = 0.12
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CG_aft_limit = 0.34
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||||||
empty_weight_pitch_MOI = 20897456
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||||||
empty_weight_roll_MOI = 6368555
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||||||
empty_weight_yaw_MOI = 40761191
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empty_weight_coupled_MOI = 0
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activate_mach_limit_based_on_cg = 0
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activate_cg_limit_based_on_mach = 0
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max_number_of_stations = 21
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//KH START Empty default
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station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
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station_load.1=190, 82.0, 2.0, 4.0, First Officer, 2
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||||||
station_load.2=190, 80.0, 3.3, 4.0, Engineer, 0
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||||||
station_load.3=760, 66.0, 0.0, 4.0, Cabin crew 1, 0
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||||||
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 4
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||||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
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station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
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||||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
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||||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
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||||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
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||||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
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||||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
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||||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
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||||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
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||||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
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||||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
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|
||||||
station_load.16=760, -55.0, 0.0, 4.0, Cabin crew 2, 0
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||||||
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 6
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||||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
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||||||
station_load.19=0, 5.0, -2.0, -4.5, Left aux tank, 0
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||||||
station_load.20=0, 5.0, 2.0, -4.5, Right aux tank, 0
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||||||
//KH END
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||||||
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||||||
[CONTACT_POINTS]
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||||||
static_pitch = 0
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|
||||||
static_cg_height = 16.4
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||||||
gear_system_type = 1
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||||||
tailwheel_lock = 0
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||||||
max_number_of_points = 16
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|
||||||
gear_locked_on_ground = 0
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|
||||||
gear_locked_above_speed = -1
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|
||||||
max_speed_full_steering = 25
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||||||
min_available_steering_angle_pct = 0.2
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|
||||||
max_speed_decreasing_steering = 45
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|
||||||
max_speed_full_steering_castering = 20
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|
||||||
max_speed_decreasing_steering_castering = 35
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|
||||||
emergency_extension_type = 2
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|
||||||
hyd_need_power_to_function= 0
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|
||||||
min_castering_angle = 0.05236
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|
||||||
max_castering_angle = 1.32645
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||||||
allow_stopped_steering = 1
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|
||||||
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
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||||||
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
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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
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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
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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
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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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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
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||||||
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[FUEL]
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LeftMain = -20.00, -38.00, -1.0, 8938, 10.00
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RightMain = -20.00, 38.00, -1.0, 8938, 10.00
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Center1 = 10.00, 0.00, -3.00, 13000.00, 10.00
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||||||
Center2 = 0.00, 0.00, -1.00, 1642.00, 10.00
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||||||
Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
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LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
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RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
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External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
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//KH From 5.00, -2.00, -3.00, 0.00, 10.00
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LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00
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//KH From 5.00, 2.00, -3.00, 0.00, 10.0
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RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
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fuel_type = 2
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number_of_tank_selectors = 3
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electric_pump = 0
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|
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engine_driven_pump = 1
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|
||||||
manual_transfer_pump = 0
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manual_pump = 0
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anemometer_pump = 0
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|
||||||
fuel_dump_rate = 0.02
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default_fuel_tank_selector.1 = 1
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default_fuel_tank_selector.2 = 1
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default_fuel_tank_selector.3 = 1
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[AIRPLANE_GEOMETRY]
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|
||||||
wing_area = 3648
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wing_span = 170.5
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|
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wing_root_chord = 34.68
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wing_camber = 1
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wing_thickness_ratio = 0.04
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wing_dihedral = 2.2
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wing_incidence = 1.5
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wing_twist = -0.5
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oswald_efficiency_factor = 0.72
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wing_winglets_flag = 1
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|
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wing_sweep = 38
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|
||||||
wing_pos_apex_lon = 1
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|
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wing_pos_apex_vert = -2.75
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|
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htail_area = 920
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||||||
htail_span = 59.5
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||||||
htail_pos_lon = -88
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||||||
htail_pos_vert = 5.0
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||||||
htail_incidence = 0.8
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||||||
htail_sweep = 36.5
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|
||||||
htail_thickness_ratio = 0.02
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||||||
vtail_area = 760
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|
||||||
vtail_span = 28.1
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||||||
vtail_sweep = 43
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||||||
vtail_pos_lon = -79.5
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|
||||||
vtail_pos_vert = 28
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|
||||||
vtail_thickness_ratio = 0.03
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|
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fuselage_length = 202.16
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||||||
fuselage_diameter = 19.75
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fuselage_center_pos = 10, 0, 1.0
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|
||||||
elevator_area = 327.0
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|
||||||
aileron_area = 225.0
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|
||||||
rudder_area = 190.0
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|
||||||
elevator_up_limit = 25
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|
||||||
elevator_down_limit = 15
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|
||||||
aileron_up_limit = 25
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|
||||||
aileron_down_limit = 15
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|
||||||
rudder_limit = 23
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|
||||||
rudder_trim_limit = 20
|
|
||||||
elevator_trim_limit = 30
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|
||||||
spoiler_limit = 60
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|
||||||
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
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|
||||||
aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
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|
||||||
rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
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|
||||||
elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
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|
||||||
|
|
||||||
[AERODYNAMICS]
|
|
||||||
lift_coef_pitch_rate = -8.09375
|
|
||||||
lift_coef_daoa = 2.68359
|
|
||||||
lift_coef_delta_elevator = -0.28906
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|
||||||
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
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|
||||||
drag_coef_spoilers = 0.05207
|
|
||||||
side_force_slip_angle = -0.77392
|
|
||||||
side_force_roll_rate = 0.15478
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|
||||||
side_force_yaw_rate = 0
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|
||||||
side_force_delta_rudder = -0.14746
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|
||||||
pitch_moment_horizontal_incidence = 4.24755
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|
||||||
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
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|
||||||
pitch_moment_spoilers = 0
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|
||||||
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
|
|
||||||
@ -1,419 +0,0 @@
|
|||||||
; 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
|
|
||||||
@ -1,409 +0,0 @@
|
|||||||
; 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
|
|
||||||
@ -1,408 +0,0 @@
|
|||||||
; 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
|
|
||||||
@ -1,12 +1,9 @@
|
|||||||
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26
|
//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
|
||||||
auto = true
|
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 1
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
@ -23,9 +20,9 @@ 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=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||||
station_load.1=190.0, 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=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
station_load.2=190, 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
|
||||||
@ -172,7 +169,7 @@ 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 = 0.0789
|
drag_coef_flaps = 0.1889
|
||||||
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
|
||||||
@ -316,14 +313,14 @@ 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,-1
|
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0
|
||||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
|
||||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
|
||||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-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.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.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
||||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-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.6 = 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.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0
|
||||||
|
|
||||||
[STALL PROTECTION]
|
[STALL PROTECTION]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@ -340,8 +337,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -349,21 +346,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -371,20 +367,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@ -398,12 +394,12 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
pitch_scalar = 1
|
pitch_scalar = 1
|
||||||
max_on_ground_position = 1
|
max_on_ground_position = 1
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||||
@ -1,12 +1,9 @@
|
|||||||
; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26
|
//TFDi Designs MD-11F (P&W PW4660) vRC1.7.0_PW_F 15MAY25
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
|
||||||
auto = true
|
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 1
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
@ -23,9 +20,9 @@ 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=190.0, 82.0, -2.0, 4.0, Pilot, 1
|
station_load.0=190, 82.0, -2.0, 4.0, Pilot, 1
|
||||||
station_load.1=190.0, 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=190.0, 80.0, 3.3, 4.0, Engineer, 0
|
station_load.2=190, 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
|
||||||
@ -172,7 +169,7 @@ 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 = 0.0789
|
drag_coef_flaps = 0.1889
|
||||||
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
|
||||||
@ -316,14 +313,14 @@ 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,-1
|
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,0,0,0,-75,33,2,33,2,2,33,0
|
||||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
|
||||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
|
||||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-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.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.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
||||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-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.6 = 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.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,-1
|
interactive_point.7 = 0,54.038418,-9.45901,-0.003025,1,0,0,0,0,0,0,0,0,0,0
|
||||||
|
|
||||||
[STALL PROTECTION]
|
[STALL PROTECTION]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@ -340,8 +337,8 @@ type = 1
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.25
|
span-outboard = 0.25
|
||||||
extending-time = 22
|
extending-time = 22
|
||||||
damaging-speed = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -349,20 +346,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -370,20 +367,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@ -397,12 +394,12 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
pitch_scalar = 1
|
pitch_scalar = 1
|
||||||
max_on_ground_position = 1
|
max_on_ground_position = 1
|
||||||
flaps-position.0 = 0, -1, 0
|
flaps-position.0 = 0, -1, 0
|
||||||
flaps-position.1 = 20, 215, 0.5, 0.5
|
flaps-position.1 = 20, 215, 0.5, 0.5
|
||||||
@ -1,9 +1,9 @@
|
|||||||
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26
|
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.0_GE 15MAY25
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 1
|
||||||
|
|
||||||
[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, 4
|
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0
|
||||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0
|
||||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0
|
||||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0
|
||||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0
|
||||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0
|
||||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0
|
||||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0
|
||||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0
|
||||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0
|
||||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0
|
||||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0
|
||||||
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, 6
|
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0
|
||||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0
|
||||||
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 = 0.0789
|
drag_coef_flaps = 0.1889
|
||||||
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,-1
|
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0
|
||||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
|
||||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
|
||||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-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.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.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
||||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-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.6 = 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.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33
|
||||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-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.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-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.10 = 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.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-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.12 = 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
|
||||||
|
|
||||||
[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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
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 = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@ -1,12 +1,9 @@
|
|||||||
; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26
|
//TFDi Designs MD-11 (PW4460) vRC1.7.0_PW 15MAY25
|
||||||
|
|
||||||
[MODULAR_MERGE]
|
|
||||||
auto = true
|
|
||||||
|
|
||||||
[VERSION]
|
[VERSION]
|
||||||
//KH Bump major
|
//KH Bump major
|
||||||
major = 4
|
major = 4
|
||||||
minor = 2
|
minor = 1
|
||||||
|
|
||||||
[WEIGHT_AND_BALANCE]
|
[WEIGHT_AND_BALANCE]
|
||||||
max_gross_weight = 630500
|
max_gross_weight = 630500
|
||||||
@ -27,21 +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, 4
|
station_load.4=0, 45.0, -5.0, 4.0, Business 1 L, 0
|
||||||
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 4
|
station_load.5=0, 45.0, 0.0, 4.0, Business 1 C, 0
|
||||||
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 4
|
station_load.6=0, 45.0, 5.0, 4.0, Business 1 R, 0
|
||||||
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 4
|
station_load.7=0, 25.0, -5.0, 4.0, Business 2 L, 0
|
||||||
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 4
|
station_load.8=0, 25.0, 0.0, 4.0, Business 2 C, 0
|
||||||
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 4
|
station_load.9=0, 25.0, 5.0, 4.0, Business 2 R, 0
|
||||||
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 3
|
station_load.10=0, -20.0, -5.0, 4.0, Economy 3 L, 0
|
||||||
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 3
|
station_load.11=0, -20.0, 0.0, 4.0, Economy 3 C, 0
|
||||||
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 3
|
station_load.12=0, -20.0, 5.0, 4.0, Economy 3 R, 0
|
||||||
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 5
|
station_load.13=0, -50.0, -5.0, 4.0, Economy 4 L, 0
|
||||||
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 5
|
station_load.14=0, -50.0, 0.0, 4.0, Economy 4 C, 0
|
||||||
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 5
|
station_load.15=0, -50.0, 5.0, 4.0, Economy 4 R, 0
|
||||||
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, 6
|
station_load.17=0, 30.0, 0.0, -4.5, Forward cargo, 0
|
||||||
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 6
|
station_load.18=0, -30.0, 0.0, -4.5, Rear cargo, 0
|
||||||
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
|
||||||
@ -178,7 +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 = 0.0789
|
drag_coef_flaps = 0.1889
|
||||||
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
|
||||||
@ -322,19 +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,-1
|
interactive_point.0 = 0.4,75.650002,-7.92,-0.567,2,0,0,-75,33,2,33,2,2,33,0
|
||||||
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33,-1
|
interactive_point.1 = 0.4,75.650002,7.92,-0.567,0,0,0,75,33,2,33,2,2,33
|
||||||
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0,-1
|
interactive_point.2 = 0.4,33.299999,6.28,-7.18,1,0,0,90,0,0,0,0,0,0
|
||||||
interactive_point.3 = 0.4,-51.700363,6.28,-7.180745,1,0,0,90,0,0,0,0,0,0,-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.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.4 = 0.4,-68.277824,-2.822939,-5.923376,1,2.395636,12.258935,79.089348,0,0,0,0,0,0,0
|
||||||
interactive_point.5 = 0,85.062134,-3.882079,4.412694,2,-0,-29.85655,42.814491,0,0,0,0,0,0,-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.6 = 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.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33,-1
|
interactive_point.7 = 0.4,44.150002,-10.05,-0.567,0,0,0,-88,35,0,35,0,2,33
|
||||||
interactive_point.8 = 0.4,44.150002,10.05,-0.567,0,0,0,88,35,0,35,0,2,33,-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.9 = 0.4,-2.869313,-10.049908,-0.566572,0,0,0,-90,35,0,35,0,2,33,-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.10 = 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.11 = 0.4,-62.995712,-8.519092,-0.565611,0,0,0,-100,35,0,35,0,2,33,-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.12 = 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
|
||||||
|
|
||||||
[STALL PROTECTION]
|
[STALL PROTECTION]
|
||||||
stall_protection = 1 ; Alpha Protection
|
stall_protection = 1 ; Alpha Protection
|
||||||
@ -351,8 +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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -360,20 +357,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 280
|
damaging-speed = 250
|
||||||
blowout-speed = 310
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.1
|
lift_scalar = 0.1
|
||||||
drag_scalar = 1.1
|
drag_scalar = 1.1
|
||||||
@ -381,20 +378,20 @@ 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, 0.45, 2, 0, 0, 0, 1
|
flaps-position.2 = 15, 215, 0.25, 2, 0, 0, 0, 1
|
||||||
flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
|
flaps-position.3 = 20, 200, 0.26, 1.1, 0, 0, 0, 1
|
||||||
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
|
flaps-position.4 = 24, 185, 0.28, 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, 155, 0.54, 1
|
flaps-position.7 = 50, 150, 0.33, 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 = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@ -408,8 +405,8 @@ type = 2
|
|||||||
system_type = 1
|
system_type = 1
|
||||||
span-outboard = 0.7
|
span-outboard = 0.7
|
||||||
extending-time = 21
|
extending-time = 21
|
||||||
damaging-speed = 300
|
damaging-speed = 250
|
||||||
blowout-speed = 330
|
blowout-speed = 300
|
||||||
maneuvering_flaps = 0
|
maneuvering_flaps = 0
|
||||||
lift_scalar = 0.5
|
lift_scalar = 0.5
|
||||||
drag_scalar = 0.75
|
drag_scalar = 0.75
|
||||||
@ -1,6 +1,6 @@
|
|||||||
{
|
{
|
||||||
"name": "tfdidesign-md11-load-manager",
|
"name": "tfdidesign-md11-load-manager",
|
||||||
"version": "0.1.187",
|
"version": "0.1.186",
|
||||||
"description": "",
|
"description": "",
|
||||||
"main": "index.js",
|
"main": "index.js",
|
||||||
"type": "module",
|
"type": "module",
|
||||||
|
|||||||
@ -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, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_EMPTY_WEIGHT, DATA_DEFINITION_EMPTY_WEIGHT, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME);
|
||||||
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, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_PAX, DATA_DEFINITION_PAYLOAD_PAX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME);
|
||||||
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, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_PAYLOAD_F, DATA_DEFINITION_PAYLOAD_F, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME);
|
||||||
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, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_FUEL, DATA_DEFINITION_FUEL, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME);
|
||||||
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, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_GSX, DATA_DEFINITION_GSX, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_VISUAL_FRAME);
|
||||||
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_VISUAL_FRAME, SIMCONNECT_DATA_REQUEST_FLAG_CHANGED);
|
hr = SimConnect_RequestDataOnSimObject(simConnect, DATA_REQUEST_USER_DATA, DATA_DEFINITION_USER_DATA, SIMCONNECT_OBJECT_ID_USER, SIMCONNECT_PERIOD_SECOND);
|
||||||
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;
|
||||||
@ -924,12 +924,6 @@ 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: {
|
||||||
@ -945,15 +939,6 @@ 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: {
|
||||||
@ -989,8 +974,6 @@ 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 = {};
|
||||||
@ -1031,8 +1014,6 @@ 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));
|
||||||
@ -1056,12 +1037,10 @@ 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 && GSXData->loadingState != LOADING_STATE_DEBOARDING) break;
|
if (GSXData->loadingState != LOADING_STATE_BOARDED) 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 = {};
|
||||||
|
|||||||
@ -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 "1.14"
|
#define VERSION_STRING "1.6"
|
||||||
// COMM BUS
|
// COMM BUS
|
||||||
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
|
||||||
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"
|
||||||
|
|||||||
@ -1 +1 @@
|
|||||||
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
|
Copy-Item .\PackageSources\wasm-module\MSFS\Debug\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
|
||||||
@ -1 +1 @@
|
|||||||
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\common\panel
|
Copy-Item .\PackageSources\wasm-module\MSFS\Release\load-manager.wasm .\PackageSources\SimObjects\Airplanes\TFDi_Design_MD-11\panel
|
||||||
|
|||||||
10
package.json
10
package.json
@ -1,9 +1,5 @@
|
|||||||
{
|
{
|
||||||
"scripts": {
|
"devDependencies": {
|
||||||
"debugger": "cd \"$env:MSFS_SDK/Tools/CoherentGT Debugger\" && ./Debugger.exe",
|
"diff": "^8.0.2"
|
||||||
"locale": "cd \"$env:MSFS_SDK/Tools/MSFS_Localization\" && ./MSFSLocalizationManager.exe"
|
}
|
||||||
},
|
|
||||||
"devDependencies": {
|
|
||||||
"diff": "^8.0.2"
|
|
||||||
}
|
|
||||||
}
|
}
|
||||||
|
|||||||
@ -10,10 +10,8 @@
|
|||||||
"DEBOARDED",
|
"DEBOARDED",
|
||||||
"deboarding",
|
"deboarding",
|
||||||
"khofmann",
|
"khofmann",
|
||||||
"SIMOBJECTS",
|
|
||||||
"tfdi",
|
"tfdi",
|
||||||
"TFDI",
|
"TFDI",
|
||||||
"tfdidesign",
|
|
||||||
"TOCG",
|
"TOCG",
|
||||||
"ZFWCG"
|
"ZFWCG"
|
||||||
]
|
]
|
||||||
|
|||||||
@ -1,11 +0,0 @@
|
|||||||
<UserSettings>
|
|
||||||
<CheckedOutPackages>
|
|
||||||
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
|
|
||||||
</CheckedOutPackages>
|
|
||||||
<SelectedPackages>
|
|
||||||
<Package Name="xkhofmann-tfdidesign-md11-load-manager"/>
|
|
||||||
</SelectedPackages>
|
|
||||||
<Filter/>
|
|
||||||
<ShowOnlyEdited>false</ShowOnlyEdited>
|
|
||||||
</UserSettings>
|
|
||||||
|
|
||||||
Loading…
x
Reference in New Issue
Block a user