[fltsim.0]
title=Hawker Raytheon
sim=Hawker
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=9265
ui_manufacturer=British Aerospace
ui_type="Hawker Raytheon"
ui_variation="Venezuelan Airplane"
description=The HS-125-700 and Hawker 800 are two more recent versions of the world's longest running corporate jet production program.The 125-700 and Hawker 800 are direct developments of the DH-125 (later the HS-125), which first flew in August 1962. This aircraft was developed into a number of variants through to the HS-125-600, all of which are powered by the RollsRoyce Viper turbojet and are described separately under Hawker Siddeley.The 125-800 became the Hawker 800 from mid 1993 when Raytheon purchased BAe's Corporate Jets division. Production has been transferred to Wichita in the USA (the first US built 800 flew on November 5 1996, the last UK built 800 on April 29 1997). Current production is of the 850XP (Extended Performance) which was certificated in 1995 and has improved engines for better climb and cruise performance. A new interior is being introduced in 1999.
[fltsim.1]
title=Hawker Raytheon Paint1
sim=Hawker
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=9265
ui_manufacturer=British Aerospace
ui_type="Hawker Raytheon"
ui_variation="De franjas"
description=The HS-125-700 and Hawker 800 are two more recent versions of the world's longest running corporate jet production program.The 125-700 and Hawker 800 are direct developments of the DH-125 (later the HS-125), which first flew in August 1962. This aircraft was developed into a number of variants through to the HS-125-600, all of which are powered by the RollsRoyce Viper turbojet and are described separately under Hawker Siddeley.The 125-800 became the Hawker 800 from mid 1993 when Raytheon purchased BAe's Corporate Jets division. Production has been transferred to Wichita in the USA (the first US built 800 flew on November 5 1996, the last UK built 800 on April 29 1997). Current production is of the 850XP (Extended Performance) which was certificated in 1995 and has improved engines for better climb and cruise performance. A new interior is being introduced in 1999.
[fltsim.2]
title=Hawker Raytheon Paint2
sim=Hawker
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=9265
ui_manufacturer=British Aerospace
ui_type="Hawker Raytheon"
ui_variation="Marron"
description=The HS-125-700 and Hawker 800 are two more recent versions of the world's longest running corporate jet production program.The 125-700 and Hawker 800 are direct developments of the DH-125 (later the HS-125), which first flew in August 1962. This aircraft was developed into a number of variants through to the HS-125-600, all of which are powered by the RollsRoyce Viper turbojet and are described separately under Hawker Siddeley.The 125-800 became the Hawker 800 from mid 1993 when Raytheon purchased BAe's Corporate Jets division. Production has been transferred to Wichita in the USA (the first US built 800 flew on November 5 1996, the last UK built 800 on April 29 1997). Current production is of the 850XP (Extended Performance) which was certificated in 1995 and has improved engines for better climb and cruise performance. A new interior is being introduced in 1999.
[fltsim.3]
title=Hawker Raytheon Paint3
sim=Hawker
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=9265
ui_manufacturer=British Aerospace
ui_type="Hawker Raytheon"
ui_variation="Gris"
description=The HS-125-700 and Hawker 800 are two more recent versions of the world's longest running corporate jet production program.The 125-700 and Hawker 800 are direct developments of the DH-125 (later the HS-125), which first flew in August 1962. This aircraft was developed into a number of variants through to the HS-125-600, all of which are powered by the RollsRoyce Viper turbojet and are described separately under Hawker Siddeley.The 125-800 became the Hawker 800 from mid 1993 when Raytheon purchased BAe's Corporate Jets division. Production has been transferred to Wichita in the USA (the first US built 800 flew on November 5 1996, the last UK built 800 on April 29 1997). Current production is of the 850XP (Extended Performance) which was certificated in 1995 and has improved engines for better climb and cruise performance. A new interior is being introduced in 1999.
"
[General]
atc_type=Hawker
atc_model=850xp
editable=0
performance="Cruise Speed\t\nMach 0.80 500 kts 800 kmh\n\nEngines\t\nAllied Signal TFE731-20 3,500 lb thrust\n\nMaximum Range\t\n2,200 nm 2,532 sm \t 4,074 km\n\nService Ceiling\t\n51,000 ft 15,545 m\n\nFuel Capacity\t\n6,062 lb 2,722 kg\n905 U.S. gal 3,424 L \n\nMaximum Gross Weight\t\n20,450 lb 9,276 kg\n\nMaximum Takeoff Weight - HGW\t\n20,200 lb \t9,163 kg\n\nUseful Load\t\n8,750 lb \t3,969 kg\n\nLength\t\n58.4 ft\t 17.7 m\n\nWingspan\t\n47.8 ft\t 14.6 m\n\nHeight\t\n14.3 ft\t 4.3 m\n\nSeating\t\nUp to 9"
Category=airplane
[CameraDefinition.0]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -2.2, -1.2, -7
InitialPbh = 0, 0, 13
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 3, -35.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 25.8, 1.6, 0.0
InitialPbh = 6, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -25.8, 1.6, 0.0
InitialPbh = 6, 0, 80
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.1, 0.0, 0.0
InitialPbh=2, 0, 0
[CameraDefinition.002]
Title = "Center Console"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.54, 0.3, -0.05
InitialPbh=75, 0, 0
[CameraDefinition.003]
Title = "Engine Controls"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.54, 0.0, 0.28
InitialPbh=65.0, 0, 0
[CameraDefinition.004]
Title = "Overhead Panel"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.55, -0.58, -0.3
InitialPbh=-49.7, 0, 0
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -17.0, -1.2, 0.0, Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -17.0, 1.2, 0.0, Co-Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, -22.5, -1.2, 0.0, Passenger 1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, -22.5, 1.2, 0.0, Passenger 2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "170, -26.7, -1.2, 0.0, Passenger 3" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "170, -26.7, 1.2, 0.0, Passenger 4" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "0, -30.9, -1.2, 0.0, Passenger 5" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "0, -30.9, 1.2, 0.0, Passenger 6" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0, -35.1, -1.2, 0.0, Passenger 7" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0, -35.1, 1.2, 0.0, Passenger 8" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "100, -42.0, 0.0, 0.0, Baggage1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "50, -45.0, 0.0, 0.0, Baggage2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 70000
empty_weight_coupled_MOI = 0.0
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 3500 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
//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
[contact_points]
point.0=1, -10.00, 0.00, -4.35, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -37.25, -4.75, -4.87, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -37.25, 4.75, -4.87, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -37.83, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -37.83, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.84
static_cg_height = 4.36
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //Brake scalar
[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 = -16.385, -1.435, 3.012
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -63.05, 0.00, 13.05, fx_beaconh ,
light.1 = 1, -42.00, 0.00, -2.40, fx_beaconb ,
light.2 = 2, -22.97, 0.40, -1.35, fx_strobe ,
light.3 = 3, -43.00, -23.78, 0.10, fx_navredm ,
light.4 = 3, -43.00, 23.77, 0.10, fx_navgrem ,
light.5 = 3, -60.18, 0.00, 7.50, fx_navwhi ,
light.6 = 4, -29.00, -0.10, 3.00, fx_vclight,
light.7 = 4, -28.50, 0.10, 3.00, fx_vclight,
light.8 = 4, -23.30, -0.10, 3.25, fx_vclight,
light.9 = 4, -23.30, 0.10, 3.25, fx_vclighth,
light.10= 4, -16.00, 0.00, 3.25, fx_vclighth,
light.11= 4, -15.00, 0.00, 1.25, fx_vclighth,
light.12= 5, -21.7, 0.00, -1.45, fx_landing,
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 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 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -36.3, 10.0, -1.5, 268.5, 0.0 //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
[airplane_geometry]
wing_area = 312.0 //Square feet
wing_span = 45.8 //Feet
wing_root_chord = 9.9 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 13.4 //Degrees, wing leading edge
wing_pos_apex_lon = -31.5 //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 = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -59.1 //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 = 2.0 //Degrees
htail_sweep = 25.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 464.0 //Knots True (KTAS)
max_mach = 0.81
max_indicated_speed = 330 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
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=25.0
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
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
