// AI Vessel configuration files
// by Holger Sandmann, hsandman@sfu.ca
// FS9 Version, January 2005
//
// for JetFoil V3
// by Mitsuya Hamaguchi ("hama"), m28hama@i.bekkoame.ne.jp
//
// !!!Copyright remains with the original authors!!!
[fltsim.0]
title=AI Vessel Jetfoil Hovercontrol CRG
sim=hama_jetfoil
model=j
panel=
sound=
texture=hc
atc_parking_types=
ui_manufacturer=AI Vessel
ui_type=JetFoil
ui_variation=JR Beetle CRG
description=
[General]
atc_type=
atc_model=
editable=0
performance=Cruise Speed\n47 Knots 87 km\n\n
//---- misc tweaked parameters
//0 Class <0=none,1=wheel, 2=scrape, 3=skid>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
// Class 1 points provide the main ground contact
point.0=1, 2.15, -0.50, -5.800, 15600, 0, 0.519, 40.0, 0.3, 2.5, 0.80, 0.0, 0.0, 0, 0.0, 0.0
point.1=1, 2.15, 0.50, -5.800, 15600, 0, 0.519, 40.0, 0.3, 2.5, 0.80, 0.0, 0.0, 1, 0.0, 0.0
point.2=1, -6.40, -5.25, -5.800, 15600, 1, 0.519, 0.0, 0.4, 2.5, 0.80, 0.0, 0.0, 2, 0.0, 0.0
point.3=1, -6.40, 5.25, -5.800, 15600, 2, 0.519, 0.0, 0.4, 2.5, 0.80, 0.0, 0.0, 3, 0.0, 0.0
// Class 4 points determine the trigger points for splash effects
point.4=4, 36.00, -2.50, -5.600, 15600, 0, 0.319, 40.0, 0.85, 2.5, 0.4, 0.0, 0.0, 0, 0.0, 0.0
point.5=4, 36.00, 2.50, -5.600, 15600, 0, 0.319, 40.0, 0.80, 2.5, 0.4, 0.0, 0.0, 1, 0.0, 0.0
point.6=4, -32.00,-15.00, -5.600, 15600, 0, 0.319, 3.0, 0.95, 2.5, 0.4, 0.0, 0.0, 2, 0.0, 0.0
point.7=4, -32.00, 15.00, -5.600, 15600, 0, 0.319, 3.0, 0.95, 2.5, 0.4, 0.0, 0.0, 3, 0.0, 0.0
point.8=4, -31.00, 0.00, -5.600, 15600, 0, 0.319, 3.0, 0.95, 2.5, 0.4, 0.0, 0.0, 3, 0.0, 0.0
//point.0=1, 2.15, -0.50, -5.700, 1600, 0, 1.40, 10.0, 0.3, 2.5, 0.80, 0.0, 0.0, 0, 175.0, 175.0
//point.1=1, 2.15, 0.50, -5.700, 1600, 0, 1.40, 10.0, 0.3, 2.5, 0.80, 0.0, 0.0, 1, 175.0, 175.0
//point.2=1, -6.40, -5.250, -5.700, 1650, 1, 1.50, 0.0, 0.4, 2.5, 0.80, 0.0, 0.0, 2, 175.0, 175.0
//point.3=1, -6.40, 5.250, -5.700, 1650, 2, 1.50, 0.0, 0.4, 2.5, 0.80, 0.0, 0.0, 3, 175.0, 175.0
//point.4=4, 4.00, -2.5, -5.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.4, 0.0, 0.0, 0, 0.0, 0.0
//point.5=4, 4.00, 2.5, -5.600, 1600, 0, 0.00, 0.0, 0.8, 2.5, 0.4, 0.0, 0.0, 1, 0.0, 0.0
//point.6=4, -14.00, -8.00, -5.600, 1600, 0, 0.00, 3.0, 0.95, 2.5, 0.4, 0.0, 0.0, 2, 0.0, 0.0
//point.7=4, -14.00, 8.00, -5.600, 1600, 0, 0.00, 3.0, 0.95, 2.5, 0.4, 0.0, 0.0, 3, 0.0, 0.0
//point.8=2, -12.90, -26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
//point.9=2, -12.90 26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
//point.10=2, -36.23, 0.00, 0.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
//point.11=2, -0.50, 0.00, -2.17, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
//point.12=2, -38.00, 0.00, 9.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
//point.13=5, 30.90, -5.250, -7.300, 1600, 0, 0.00, 0.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
//point.14=5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 0.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0
max_number_of_points=21
static_pitch=0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.765 //feet, altitude of CG when at rest on the ground
//static_pitch=0.000000
//static_cg_height=1.500000
[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=4, 20.00, 0.00 ,12.10, fx_vclighth ,
light.1=1, 9.00, -10.88, 19.65, fx_navred ,
light.2=1, 9.00, 10.88, 19.65, fx_navgre ,
//light.1=1, 19.90, -14.98, 14.05, fx_navred ,
//light.1=1, 19.90, 14.98, 14.05, fx_navgre ,
light.3=1, 9.50, 0.00, 30.80, fx_beacon ,
light.4=1, 5.00, 0.00, -4.00, fx_AI_ship_wake_l
[SMOKESYSTEM]
smoke.0=0, 36.0, 0.0, fx_spray1.fx,
smoke.1=0, -32.0, 15.0, fx_spray1.fx,
smoke.2=0, -32.0, -15.0, fx_spray1.fx,
smoke.3=0, -31.0, 0.0, fx_spray1.fx,
[EFFECTS]
wake=fx_wake
water=fx_sparks
dirt=fx_tchdrt
concrete=fx_spray1
//concrete=fx_spray
touchdown=fx_wtrspray_s, 1
//wake=fx_wake_ss
//water=fx_spray_lie
//dirt=fx_tchdrt
//concrete=fx_sparks
//touchdown=fx_tchdwn_s, 1
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.68 //Brake scalar
[WEIGHT_AND_BALANCE]
max_gross_weight=2500 // (pounds)
empty_weight=2500 // (pounds)
reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-3.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=25400.0
empty_weight_roll_MOI=27137.0
empty_weight_yaw_MOI=20060.0
//CG_forward_limit=0.000000
//CG_aft_limit=1.000000
empty_weight_coupled_MOI=100.000000
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=90.3 //Cubic inches per cylinder
compression_ratio=8.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm=35 //Max rated RPM
//max_rated_rpm=3500 //Max rated RPM
max_rated_hp=10 //Max rated HP
//max_rated_hp=60 //Max rated HP
fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=1 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=50 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=12500 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.4 //Scalar on idle RPM friction
[airplane_geometry]
wing_area=2.39000000
wing_span=8.6083333
//wing_area=239.000000
//wing_span=86.083333
wing_root_chord=4.916670
wing_tip_chord=4.916670
wing_dihedral=-0.735840
wing_incidence=-19.499634
wing_twist=0.999268
oswald_efficiency_factor=0.0308470
//oswald_efficiency_factor=0.708470
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=6.0
wing_pos_apex_vert=35.000000
htail_area=9.000000
htail_span=11.666667
htail_pos_lon=-18.266667
htail_pos_vert=0.000000
htail_incidence=19.246460
htail_sweep=0.000000
vtail_area=900.000000
vtail_pos_lon=-176.183333
vtail_pos_vert=0.000000
elevator_area=16.610000
aileron_area=1.300000
rudder_area=300.650000
elevator_up_limit=28.000447
elevator_down_limit=20.998903
aileron_up_limit=19.996227
aileron_down_limit=15.000035
rudder_limit=3.995472
elevator_trim_limit=19.497754
spoiler_limit=45.000000
vtail_span=4.837355
vtail_sweep=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
//---- original parameters from Jetfoil
[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=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-12.4, -5.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-12.4, 5.0, 0.0 //(feet) longitudinal, lateral, ve
fuel_flow_scalar=0.88 //Fuel flow scalar
min_throttle_limit=0.0 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=5.0 //Propeller moment of inertia
beta_max=0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0 //Miminum governed RPM
prop_tc=0 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
[hydraulic_system]
normal_pressure=0.0 //PSI
[Views]
eyepoint=22.3, 1.3, 12.2 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
;/ Radio Type = availiable, 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
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=100, 180
aileron=200, 1000
rudder=200, 1000
[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=1,0
[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[fuel]
LeftMain=-3.9, -2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-3.9, 2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.2,0.2 ;Percent per second
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.5 // 0.0 .. 1.0
extending-time=7 // seconds
flaps-position.0=0 // degrees
flaps-position.1=12.7 // degrees
flaps-position.2=25.3 // degrees
flaps-position.3=38 // degrees
damaging-speed=120 // KIAS
blowout-speed=150 // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[Reference Speeds]
flaps_up_stall_speed=53.0 //Knots True (KTAS)
full_flaps_stall_speed=48.0 //Knots True (KTAS)
cruise_speed=115.0 //Knots True (KTAS)
max_indicated_speed=163 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.0
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=9.00
nav_integrator_control=0.25
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=0.0
default_pitch_mode=0
default_bank_mode=0
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=1
