Trying to get the F-14D for FSX:Acceleration by Dino Cattaneo aircraft to launch from a carrier using the FSX acceleration method with no success. I have it working pretty good using COP30. Any suggestions? Seems the launch bar won't work, blast shield doesn't come up therefore, no launch.
F-14D for FSX:Acceleration by Dino Cattaneo
- Thread starter uniform7
- Start date
Dino Cattaneo
Charter Member
@uniform7
...that is pretty strange as it is designed from FSX:Acceleration indeed. I would suggest you check your key assignments. The launch bar control should work (and should also cause the F-14 to kneel).
...that is pretty strange as it is designed from FSX:Acceleration indeed. I would suggest you check your key assignments. The launch bar control should work (and should also cause the F-14 to kneel).
Acceleration
Ya, help me out here if you can. All my other aircraft work as described except this. I even have F-86 and T-38's working. Can you guys take a look at my .cfg? I haven't changed anything else in the download.
[fltsim.0]
title=F-14D Tomcat 159449 Acceleration
sim=F14D
model=
panel=
sound=
texture=159449
kb_checklists=F14D_info
kb_reference=F14D_info
atc_id=Dakota212
atc_airline=NAVY
atc_flight_number=212
ui_manufacturer=MIKE
ui_type="F-14D Tomcat"
ui_variation="159449/AE-212, VF-142 Ghostriders Acceleration"
ui_typerole="Twin Engine Jet"
ui_createdby="Dino Cattaneo"
description="Rendition of scheme originally from F-14A, by Jiri Soukup. Based on original textures by Dino Cattaneo\n\nThe F-14 Tomcat is a supersonic, twin-engine, variable sweep wing, two-place fighter signed to attack and destroy enemy aircraft at night and in all weather conditions. The F-14 can track up to 24 targets simultaneously with its advanced weapons control system and attack six with Phoenix AIM-54A missiles while continuing to scan the airspace. Armament also includes a mix of other air intercept missiles, rockets and bombs."
[General]
atc_type=GRUMMAN
atc_model=F14
editable=0
performance="Function: Carrier-based multi-role strike fighter\nUnit Cost: $38 million\nPropulsion:
Category = airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 74350.0 // (pounds) EXACT VALUE
empty_weight = 43500.0 // (pounds) EXACT VALUE
;Moments of Inertia
empty_weight_pitch_MOI = 93000 // Estimated by coparison to stock Hornet
empty_weight_roll_MOI = 40000 // Estimated by coparison to stock Hornet
empty_weight_yaw_MOI = 100000 // Estimated by coparison to stock Hornet
empty_weight_coupled_MOI = 1000 // Estimated to take account of fuselage
reference_datum_position = 29.00, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -34.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
// Same values of stock Hornet
// Load station section: exact values applied
max_number_of_stations = 50
station_load.0 = 200, -15.0, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_load.1 = 200, -18.5, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.1 = "RIO"
station_load.2 = 190, -33.5, -11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.2 = "1A" // Sidewinder
station_load.3 = 500, -33.5, -9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.3 = "1B" // Sparrow
station_load.4 = 0, -27.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.4 = "3" // Station 3 empty
station_load.5 = 0, -43.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.5 = "4" // Statio 4 empty
station_load.6 = 0, -27.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.6 = "5" // Station 7 empty
station_load.7 = 0, -43.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.7 = "6" // Station 6 empty
station_load.9 = 500, -33.5, 9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.9 = "8A" // LANTIRN
station_load.8 = 190, -33.5, 11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.8 = "8B" // Sidewinder
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.03
aileron_effectiveness = 0.85
rudder_effectiveness = 1.1
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 0.75
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.05
[GeneralEngineData]
// Fixed position
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -45.8, -4.7, -0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -45.8, 4.7, -0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = 0 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
// Dry thrust data used, A/B trust ratio set in .air file
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 13800 //Lbs, max rated static thrust at Sea Level
afterburner_available = 5 //Afterburner stages available?
afterburner_throttle_threshold = 0.85 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.83 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 1.85 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 1.0
[contact_points]
// Checked correct
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
;Gear
point.0=1, -15.00, 0.00, -6.4, 1600, 0, 0.6349, 70.0, 0.3000, 5, 0.500, 9.5, 9.5, 0, 0.0, 280
point.1=1, -37.50, -7.4, -6.3, 1800, 1, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 2, 0.0, 280
point.2=1, -37.50, 7.4, -6.3, 1800, 2, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 3, 0.0, 280
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
static_pitch = 1.0
static_cg_height = 5.5
gear_system_type=1 //Hydraulic
emergency_extension_type=1 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 0 //Normal
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 2.5 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
//eyepoint = -14.0, 0.0, 4.82 // original by Dino
eyepoint = -13.8, 0.0, 4.84 // recommended
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Lights encoded into MDL file
light.1 = 10, -13.50, 0.00, 4.00, fx_f14d_vclight_dino
light.2 = 10, -19.00, 0.00, 4.00, fx_f14d_vclight_dino
light.3 = 6, -15.00, 0.00, -1.20, fx_landing
[Flaps.0] //Animations only
type=1
span-outboard=0.5
extending-time= 10
system_type=0
damaging-speed=450
blowout-speed=450
lift_scalar=0
drag_scalar=0
pitch_scalar=0
flaps-position.0=0 // Wings 0% (back), Flaps up, DLC Off
flaps-position.1=10 // Wings 16% , Flaps up, DLC Off
flaps-position.2=20 // Wings 33% , Flaps up, DLC Off
flaps-position.3=30 // Wings 50% , Flaps up, DLC Off
flaps-position.4=40 // Wings 66% , Flaps up, DLC Off
flaps-position.5=50 // Wings 83% , Flaps up, DLC Off
flaps-position.6=60 // Wings 100% (fully forward), Flaps up, DLC Off
flaps-position.7=75 // Wings 100%, Flaps 50% , DLC Off
flaps-position.8=90 // Wings back, Flaps 100% (fully down), DLC Off
flaps-position.9=100 // Wings 100%, Flaps 100% , DLC ON
[Flaps.1] // Lift/Drag Scalar only
type= 2
span-outboard= 0
extending-time= 10
system_type= 0
damaging-speed= 450 //300
blowout-speed= 450 //300
lift_scalar= 1
drag_scalar= 1
pitch_scalar= 1
flaps-position.0= 0
flaps-position.1= 2 //5
flaps-position.2= 5 //10
flaps-position.3= 8 //15
flaps-position.4= 12 //20
flaps-position.5= 16 //25
flaps-position.6= 20 //35
flaps-position.7= 40 //40
flaps-position.8= 65 //55
flaps-position.9= 60 //50
[Radios]
// Radio Type = available, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2
[altimeters]
altimeter.0 = 1
altimeter.1 = 1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m, 1
EngineFire=fx_engfire_f18
vaportrail_l= fx_dummy // blocks FSX wingtip vapor
vaportrail_r= fx_dummy // blocks FSX wingtip vapor
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, 1.00,1054.00, 0.00
LeftAux = -34.5, -4.6, -4.0, 575, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -27.0, 0.0, 2.5, 700, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -32.0, 0.0, 2.5, 700, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -34.5, 4.6, -4.0, 575, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
fuel_dump_rate = 0.00142 //Percent of max quantity per second
[airplane_geometry]
wing_area = 610.0 //Nominal 565 - increased to take account of body lift effect
wing_span = 64.0 //Feet
wing_root_chord = 21.5 //Feet
wing_dihedral = 2.9 //Degrees
wing_incidence = -1.0 //Degrees
wing_twist = -2 //Degrees
oswald_efficiency_factor= 0.80 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 144 //Square feet
htail_span = 33.0 //Feet
htail_pos_lon = -50.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 50.0 //Degrees, horizontal tail leading edge
vtail_area = 200 //Square feet
vtail_span = 16 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -45.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 185.0 //Square feet
aileron_area = 44.5 //Square feet
rudder_area = 40.0 //Square feet
elevator_up_limit = 25.0 //Degrees
elevator_down_limit = 12.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 8.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 0.7 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 1.8 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 6.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 5.2 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -2.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= 0.0 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 134.0 //Knots True (KTAS)
full_flaps_stall_speed = 110.0 //Knots True (KTAS)
cruise_speed = 580.0 //Knots True (KTAS)
max_mach = 1.88
max_indicated_speed = 860 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=27,14
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2 =1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[folding_wings]
wing_fold_system_type=1 // Available
fold_rates = 0.25,0.20 // Left,Right: 1/sec
[GPWS]
max_warning_height = -1 //No need for GPWS
[VoiceAlerts]
LowFuelPct = 0.1, -1, 60 //Low Fuel limit (percent), Check BELOW, Check every 60 seconds
OverGLimit = 6.0, 1, 1 //High G limit, Check ABOVE, Check every 1 seconds
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[SMOKESYSTEM]
smoke.0=-53.00, 0, -0.0, fx_smoke_w
[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -3, 4.5, -30.5
InitialPbh = 6, 0, 3.4
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.1]
Title = "Side View (left)"
Guid = {E095506E-D7E4-4d4e-B5D2-923B4F9D08FF}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 18.5, 7.5, -6.0
InitialPbh = 25, 0, 280
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.2]
Title = "Side view (right)"
Guid = {4B6E64F5-D9E2-4f08-9295-BBD59B9F9B56}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = -20.5, 10.5, 5.0
InitialPbh = 27, 0, 107
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.3]
Title = "Cinematic back view 1"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description =Looking forward from over the left wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 3, 6.5, -30.5
InitialPbh = 9, 0, -3.4
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.4]
Title = "Cinematic back view 2"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description =Looking forward from over the right wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 7, 10.0, -21.0
InitialPbh = 27, 0, -20
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.5]
Title = "Cinematic front view 1"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 5, 15.0, 22.0
InitialPbh = 35, 0, 185
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.6]
Title = "Cinematic front view 2"
Guid = {765CCF83-D7CD-4486-8983-A5714310CDD5}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -4, 10.5, 30.5
InitialPbh = 17, 0, 175
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.7]
Title = "Forward to Aft"
Guid = {5e8f370c-da99-41f5-a3e9-d4dc48d09c4e}
Description = Nose looking aft
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz = 0, 1.4, 16
InitialPbh = 10, 0, 180
ClipMode=Minimum
[CameraDefinition.8]
Title = "Left Wing"
Guid = {5d363a6e-3c89-458d-b71d-067380bf0af9}
Description = Left wing looking toward the canopy
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
//left(neg)-right, up-down, fore-aft
InitialXyz = -9, 2.0, -5
InitialPbh = 15, 0, 50
ClipMode=Minimum
[CameraDefinition.9]
Title = "Right Wing"
Guid = {7dd17eaf-057b-406a-ad9f-7c55f61650d8}
Description = Right wing looking toward the canopy
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz = 9, 2.0, -5
InitialPbh = 15, 0, -50
ClipMode=Minimum
[CameraDefinition.10]
Title = "Vstabs"
Guid = {fb1742bd-b41a-4356-bc2e-0dd997e168aa}
Description = Between the vertical stabilizers looking forward
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
HotKeySelect=4
InitialXyz = 0.0, 2.5, -17.0
InitialPbh = 10.0, 0.0, 0.0
ClipMode=Minimum
[CameraDefinition.001]
Title = "RIO cockpit"
Guid = {18EF1F08-7138-4530-948C-07698E51940D}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare= TRUE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz=0.0, 0.2, -1.6
InitialPbh=0.0, 0, 0
[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=0.4
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-50.30, 0.0, -1.23, // longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.4
[launch_assistance]
launch_bar_pivot = 17.6, 0.0, -3.27 //was 15.4, 0.0, -2.17
launch_bar_lug = 18.0, 0.0, -3.33 //was 15.8, 0.0, -2.23
Ya, help me out here if you can. All my other aircraft work as described except this. I even have F-86 and T-38's working. Can you guys take a look at my .cfg? I haven't changed anything else in the download.
[fltsim.0]
title=F-14D Tomcat 159449 Acceleration
sim=F14D
model=
panel=
sound=
texture=159449
kb_checklists=F14D_info
kb_reference=F14D_info
atc_id=Dakota212
atc_airline=NAVY
atc_flight_number=212
ui_manufacturer=MIKE
ui_type="F-14D Tomcat"
ui_variation="159449/AE-212, VF-142 Ghostriders Acceleration"
ui_typerole="Twin Engine Jet"
ui_createdby="Dino Cattaneo"
description="Rendition of scheme originally from F-14A, by Jiri Soukup. Based on original textures by Dino Cattaneo\n\nThe F-14 Tomcat is a supersonic, twin-engine, variable sweep wing, two-place fighter signed to attack and destroy enemy aircraft at night and in all weather conditions. The F-14 can track up to 24 targets simultaneously with its advanced weapons control system and attack six with Phoenix AIM-54A missiles while continuing to scan the airspace. Armament also includes a mix of other air intercept missiles, rockets and bombs."
[General]
atc_type=GRUMMAN
atc_model=F14
editable=0
performance="Function: Carrier-based multi-role strike fighter\nUnit Cost: $38 million\nPropulsion:
Category = airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 74350.0 // (pounds) EXACT VALUE
empty_weight = 43500.0 // (pounds) EXACT VALUE
;Moments of Inertia
empty_weight_pitch_MOI = 93000 // Estimated by coparison to stock Hornet
empty_weight_roll_MOI = 40000 // Estimated by coparison to stock Hornet
empty_weight_yaw_MOI = 100000 // Estimated by coparison to stock Hornet
empty_weight_coupled_MOI = 1000 // Estimated to take account of fuselage
reference_datum_position = 29.00, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -34.20, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
// Same values of stock Hornet
// Load station section: exact values applied
max_number_of_stations = 50
station_load.0 = 200, -15.0, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_load.1 = 200, -18.5, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.1 = "RIO"
station_load.2 = 190, -33.5, -11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.2 = "1A" // Sidewinder
station_load.3 = 500, -33.5, -9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.3 = "1B" // Sparrow
station_load.4 = 0, -27.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.4 = "3" // Station 3 empty
station_load.5 = 0, -43.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.5 = "4" // Statio 4 empty
station_load.6 = 0, -27.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.6 = "5" // Station 7 empty
station_load.7 = 0, -43.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.7 = "6" // Station 6 empty
station_load.9 = 500, -33.5, 9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.9 = "8A" // LANTIRN
station_load.8 = 190, -33.5, 11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.8 = "8B" // Sidewinder
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.03
aileron_effectiveness = 0.85
rudder_effectiveness = 1.1
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 0.75
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.05
[GeneralEngineData]
// Fixed position
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -45.8, -4.7, -0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -45.8, 4.7, -0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = 0 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
// Dry thrust data used, A/B trust ratio set in .air file
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 13800 //Lbs, max rated static thrust at Sea Level
afterburner_available = 5 //Afterburner stages available?
afterburner_throttle_threshold = 0.85 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.83 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 1.85 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 1.0
[contact_points]
// Checked correct
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
;Gear
point.0=1, -15.00, 0.00, -6.4, 1600, 0, 0.6349, 70.0, 0.3000, 5, 0.500, 9.5, 9.5, 0, 0.0, 280
point.1=1, -37.50, -7.4, -6.3, 1800, 1, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 2, 0.0, 280
point.2=1, -37.50, 7.4, -6.3, 1800, 2, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 3, 0.0, 280
;Wingtips
point.3=2, -43.30, -32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -46.00, -4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -46.00, 4.80, -2.5, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 10.80, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
static_pitch = 1.0
static_cg_height = 5.5
gear_system_type=1 //Hydraulic
emergency_extension_type=1 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 0 //Normal
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 2.5 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
//eyepoint = -14.0, 0.0, 4.82 // original by Dino
eyepoint = -13.8, 0.0, 4.84 // recommended
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Lights encoded into MDL file
light.1 = 10, -13.50, 0.00, 4.00, fx_f14d_vclight_dino
light.2 = 10, -19.00, 0.00, 4.00, fx_f14d_vclight_dino
light.3 = 6, -15.00, 0.00, -1.20, fx_landing
[Flaps.0] //Animations only
type=1
span-outboard=0.5
extending-time= 10
system_type=0
damaging-speed=450
blowout-speed=450
lift_scalar=0
drag_scalar=0
pitch_scalar=0
flaps-position.0=0 // Wings 0% (back), Flaps up, DLC Off
flaps-position.1=10 // Wings 16% , Flaps up, DLC Off
flaps-position.2=20 // Wings 33% , Flaps up, DLC Off
flaps-position.3=30 // Wings 50% , Flaps up, DLC Off
flaps-position.4=40 // Wings 66% , Flaps up, DLC Off
flaps-position.5=50 // Wings 83% , Flaps up, DLC Off
flaps-position.6=60 // Wings 100% (fully forward), Flaps up, DLC Off
flaps-position.7=75 // Wings 100%, Flaps 50% , DLC Off
flaps-position.8=90 // Wings back, Flaps 100% (fully down), DLC Off
flaps-position.9=100 // Wings 100%, Flaps 100% , DLC ON
[Flaps.1] // Lift/Drag Scalar only
type= 2
span-outboard= 0
extending-time= 10
system_type= 0
damaging-speed= 450 //300
blowout-speed= 450 //300
lift_scalar= 1
drag_scalar= 1
pitch_scalar= 1
flaps-position.0= 0
flaps-position.1= 2 //5
flaps-position.2= 5 //10
flaps-position.3= 8 //15
flaps-position.4= 12 //20
flaps-position.5= 16 //25
flaps-position.6= 20 //35
flaps-position.7= 40 //40
flaps-position.8= 65 //55
flaps-position.9= 60 //50
[Radios]
// Radio Type = available, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2
[altimeters]
altimeter.0 = 1
altimeter.1 = 1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m, 1
EngineFire=fx_engfire_f18
vaportrail_l= fx_dummy // blocks FSX wingtip vapor
vaportrail_r= fx_dummy // blocks FSX wingtip vapor
[fuel]
// COG fuel tank estimated for inner tanks
Center1= 0.00, 0.00, 1.00,1054.00, 0.00
LeftAux = -34.5, -4.6, -4.0, 575, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -27.0, 0.0, 2.5, 700, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -32.0, 0.0, 2.5, 700, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -34.5, 4.6, -4.0, 575, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
fuel_dump_rate = 0.00142 //Percent of max quantity per second
[airplane_geometry]
wing_area = 610.0 //Nominal 565 - increased to take account of body lift effect
wing_span = 64.0 //Feet
wing_root_chord = 21.5 //Feet
wing_dihedral = 2.9 //Degrees
wing_incidence = -1.0 //Degrees
wing_twist = -2 //Degrees
oswald_efficiency_factor= 0.80 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 144 //Square feet
htail_span = 33.0 //Feet
htail_pos_lon = -50.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 50.0 //Degrees, horizontal tail leading edge
vtail_area = 200 //Square feet
vtail_span = 16 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -45.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 185.0 //Square feet
aileron_area = 44.5 //Square feet
rudder_area = 40.0 //Square feet
elevator_up_limit = 25.0 //Degrees
elevator_down_limit = 12.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 8.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 0.7 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 1.8 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 6.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 5.2 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -2.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= 0.0 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 134.0 //Knots True (KTAS)
full_flaps_stall_speed = 110.0 //Knots True (KTAS)
cruise_speed = 580.0 //Knots True (KTAS)
max_mach = 1.88
max_indicated_speed = 860 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=27,14
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2 =1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[folding_wings]
wing_fold_system_type=1 // Available
fold_rates = 0.25,0.20 // Left,Right: 1/sec
[GPWS]
max_warning_height = -1 //No need for GPWS
[VoiceAlerts]
LowFuelPct = 0.1, -1, 60 //Low Fuel limit (percent), Check BELOW, Check every 60 seconds
OverGLimit = 6.0, 1, 1 //High G limit, Check ABOVE, Check every 1 seconds
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[SMOKESYSTEM]
smoke.0=-53.00, 0, -0.0, fx_smoke_w
[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -3, 4.5, -30.5
InitialPbh = 6, 0, 3.4
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.1]
Title = "Side View (left)"
Guid = {E095506E-D7E4-4d4e-B5D2-923B4F9D08FF}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 18.5, 7.5, -6.0
InitialPbh = 25, 0, 280
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.2]
Title = "Side view (right)"
Guid = {4B6E64F5-D9E2-4f08-9295-BBD59B9F9B56}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = -20.5, 10.5, 5.0
InitialPbh = 27, 0, 107
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.3]
Title = "Cinematic back view 1"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description =Looking forward from over the left wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 3, 6.5, -30.5
InitialPbh = 9, 0, -3.4
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.4]
Title = "Cinematic back view 2"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description =Looking forward from over the right wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 7, 10.0, -21.0
InitialPbh = 27, 0, -20
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.5]
Title = "Cinematic front view 1"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 5, 15.0, 22.0
InitialPbh = 35, 0, 185
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.6]
Title = "Cinematic front view 2"
Guid = {765CCF83-D7CD-4486-8983-A5714310CDD5}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -4, 10.5, 30.5
InitialPbh = 17, 0, 175
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
ZoomPanScalar = 1.0
[CameraDefinition.7]
Title = "Forward to Aft"
Guid = {5e8f370c-da99-41f5-a3e9-d4dc48d09c4e}
Description = Nose looking aft
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz = 0, 1.4, 16
InitialPbh = 10, 0, 180
ClipMode=Minimum
[CameraDefinition.8]
Title = "Left Wing"
Guid = {5d363a6e-3c89-458d-b71d-067380bf0af9}
Description = Left wing looking toward the canopy
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
//left(neg)-right, up-down, fore-aft
InitialXyz = -9, 2.0, -5
InitialPbh = 15, 0, 50
ClipMode=Minimum
[CameraDefinition.9]
Title = "Right Wing"
Guid = {7dd17eaf-057b-406a-ad9f-7c55f61650d8}
Description = Right wing looking toward the canopy
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz = 9, 2.0, -5
InitialPbh = 15, 0, -50
ClipMode=Minimum
[CameraDefinition.10]
Title = "Vstabs"
Guid = {fb1742bd-b41a-4356-bc2e-0dd997e168aa}
Description = Between the vertical stabilizers looking forward
Origin = Center
Category=Aircraft
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=TRUE
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
HotKeySelect=4
InitialXyz = 0.0, 2.5, -17.0
InitialPbh = 10.0, 0.0, 0.0
ClipMode=Minimum
[CameraDefinition.001]
Title = "RIO cockpit"
Guid = {18EF1F08-7138-4530-948C-07698E51940D}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare= TRUE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=70
PanAcceleratorTime=0
InitialXyz=0.0, 0.2, -1.6
InitialPbh=0.0, 0, 0
[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=0.4
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-50.30, 0.0, -1.23, // longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.4
[launch_assistance]
launch_bar_pivot = 17.6, 0.0, -3.27 //was 15.4, 0.0, -2.17
launch_bar_lug = 18.0, 0.0, -3.33 //was 15.8, 0.0, -2.23
F14 Acceleration
Well, moving the aircraft back, it arms but it doesn't kneel. See picture?
View attachment 95154
Well, moving the aircraft back, it arms but it doesn't kneel. See picture?
View attachment 95154
cortomalteseit
Charter Member
You have to move to the right position, more forward than that image shows. Then apply the parking brakes Ctrl+. and arm the launch bar Ctrl+U, then, finally, arm the catapult pressing Ctrl+i.
press the space bar and you're flying...
press the space bar and you're flying...
fxsttcb
Panel & Gauge Hack!
Odd! I looked thru my Hangar full of Dino's various F-14 releases(Beta thru V2.0), and none of them have [launch_assistance] in their aircraft.cfgs. They have all worked without it...Don
gradyhappyg
Charter Member
Same here I think Dino's launch bar is built into the model so adding it to the aircraft.cfg could be causing a conflict try deleting it from the cfg and giving it a go.
One More Thing
Now that you all have straightened me out on the acceleration launch issue, one more question if I may. I am using the COP30 panel .cfg in one of these Tomcats. Are there any bad conflicting things that could happen with the acceleration launch cfg and the cop30 installed together in the same aircraft?
Now that you all have straightened me out on the acceleration launch issue, one more question if I may. I am using the COP30 panel .cfg in one of these Tomcats. Are there any bad conflicting things that could happen with the acceleration launch cfg and the cop30 installed together in the same aircraft?
Potentially. The gauge based method was designed before FS had native carrier ops functionality. Since Acceleration, there is no need for third party solutions to launch/trap.