[fltsim.0]
title=SCm400_Advanced - Standaard
sim=SCm400_aR
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=SCm400v4_ref
description=Model and 3D VRpanel cockpit by AC Kerkhove.\nDynamicks and 2D panel by Gene Naftulyev.\nTHANKS:\nTo Skycar International SA for there suport.\nTo all my testers and those that give me some hints and tips.\nDetails:\nThe Volantor M400, by utilizing its VTOL capability, has the flexible access of the Helicopter. In addition it has the 350 Mph max. cruise speed, 900 mile range and 30,000 foot ceiling of a high performance aircraft. The M400 Volantor can\nalso climb at more than a vertical mile per minute.\nIn the Simulator the skycar is almost VTOL\nthis is due to the limitations off FS2002\nSee the ref tab in the kneebord\nfor flying instructions and more information\nAlso see the Real Skycar.\nwww.skycar.co.za\nwww.moller.com\nMost of the dynamics are based on\n the real vehicle.\nSome parameters had to be changed due to the unique\nnature of the propultion systems and the inflexibility of the Sim.
ui_manufacturer=Skycar International
ui_type=M400_advanced
ui_variation=Standaard
atc_heavy=0
atc_id=PHSKY
atc_airline=Skycar International
atc_flight_number=01
[fltsim.1]
title=SCm400_Advanced - Police
sim=SCm400_aR
model=1
panel=
sound=
texture=1
kb_checklists=
kb_reference=SCm400v4_ref
description=Model and 3D VRpanel cockpit by AC Kerkhove.\nDynamicks and 2D panel by Gene Naftulyev.\nTHANKS:\nTo Skycar International SA for there suport.\nTo all my testers and those that give me some hints and tips.\nDetails:\nThe Volantor M400, by utilizing its VTOL capability, has the flexible access of the Helicopter. In addition it has the 350 Mph max. cruise speed, 900 mile range and 30,000 foot ceiling of a high performance aircraft. The M400 Volantor can\nalso climb at more than a vertical mile per minute.\nIn the Simulator the skycar is almost VTOL\nthis is due to the limitations off FS2002\nSee the ref tab in the kneebord\nfor flying instructions and more information\nAlso see the Real Skycar.\nwww.skycar.co.za\nwww.moller.com\nMost of the dynamics are based on\n the real vehicle.\nSome parameters had to be changed due to the unique\nnature of the propultion systems and the inflexibility of the Sim.
ui_manufacturer=Skycar International
ui_type=M400_advanced
ui_variation=Police
atc_heavy=0
atc_id=SWP01
atc_airline=Skycar International
atc_flight_number=01
[fltsim.2]
title=SCm400_Advanced - Cheetah
sim=SCm400_aR
model=1
panel=
sound=
texture=2
kb_checklists=
kb_reference=SCm400v4_ref
description=Model and 3D VRpanel cockpit by AC Kerkhove.\nDynamicks and 2D panel by Gene Naftulyev.\nTHANKS:\nTo Skycar International SA for there suport.\nTo all my testers and those that give me some hints and tips.\nDetails:\nThe Volantor M400, by utilizing its VTOL capability, has the flexible access of the Helicopter. In addition it has the 350 Mph max. cruise speed, 900 mile range and 30,000 foot ceiling of a high performance aircraft. The M400 Volantor can\nalso climb at more than a vertical mile per minute.\nIn the Simulator the skycar is almost VTOL\nthis is due to the limitations off FS2002\nSee the ref tab in the kneebord\nfor flying instructions and more information\nAlso see the Real Skycar.\nwww.skycar.co.za\nwww.moller.com\nMost of the dynamics are based on\n the real vehicle.\nSome parameters had to be changed due to the unique\nnature of the propultion systems and the inflexibility of the Sim.
ui_manufacturer=Skycar International
ui_type=M400_advanced
ui_variation=Cheetah
atc_heavy=0
atc_id=PHSKY
atc_airline=Cheetah Airlines
atc_flight_number=01
[fltsim.3]
title=SCm400_Advanced - Africa
sim=SCm400_aR
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=SCm400v4_ref
description=Model and 3D VRpanel cockpit by AC Kerkhove.\nDynamicks and 2D panel by Gene Naftulyev.\nTHANKS:\nTo Skycar International SA for there suport.\nTo all my testers and those that give me some hints and tips.\nDetails:\nThe Volantor M400, by utilizing its VTOL capability, has the flexible access of the Helicopter. In addition it has the 350 Mph max. cruise speed, 900 mile range and 30,000 foot ceiling of a high performance aircraft. The M400 Volantor can\nalso climb at more than a vertical mile per minute.\nIn the Simulator the skycar is almost VTOL\nthis is due to the limitations off FS2002\nSee the ref tab in the kneebord\nfor flying instructions and more information\nAlso see the Real Skycar.\nwww.skycar.co.za\nwww.moller.com\nMost of the dynamics are based on\n the real vehicle.\nSome parameters had to be changed due to the unique\nnature of the propultion systems and the inflexibility of the Sim.
ui_manufacturer=Skycar International
ui_type=M400_advanced
ui_variation=Africa
atc_heavy=0
atc_id=SASKY
atc_airline=South Africa
atc_flight_number=01
//========================================================================================================================================
// Most of the dynamics are based on the real vehicle. Some parameters had to be changed due to the unique nature of the propultion sustems and the inflexibility of FS.
//=========================================================================================================================================
[General]
performance=Length:19.5 ft\nSpan:8.5 ft\nWeight:2400 lbs\nPower:8 x 150 hp\nRange:800 miles\nDate: 2005\nFuel consumption 25 mpg\npayload 750 lbs\nceiling 30.000 ft\nVTOL aircar\nMaxium rate of climb 5800 fpm\nCruise speed 300 mph\nTop speed at 20K ft. 380MPh\nDesigner: Dr. P Moller
atc_type=Sky Car
atc_model=M400
[WEIGHT_AND_BALANCE]
empty_weight=1400 // (pounds)
max_gross_weight = 2400
reference_datum_position = 0, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position= -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=210, -7.0, 0.0, 1.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=0, -9.0, 1.0, 1.5 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=0, -9.0, -1.0, 1.5 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=0, -11.0, 0.0, 1.5 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=116, -13.0, 0.0, 1.5 //Lugage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 25000
empty_weight_roll_MOI = 10000
empty_weight_yaw_MOI = 25000
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.15
induced_drag_scalar = 1.0
elevator_effectiveness = 1.5
aileron_effectiveness = 1.5
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
fuel_flow_scalar=1.250000
min_throttle_limit= -1.0
Engine.0=-16.000000,0.000000,1.000000
Engine.1=-10.000000,0.000000,1.000000
[TurbineEngineData]
fuel_flow_gain=0.100000
inlet_area=2.500000
rated_N2_rpm=29920.000000
static_thrust=1200.000000
afterburner_available=0
reverser_available=0.000000
[jet_engine]
thrust_scalar = 1.0
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Reference Speeds]
flaps_up_stall_speed=75.000000
// full_flaps_stall_speed=0.00000
cruise_speed=283
max_indicated_speed=331
max_mach=.79
full_flaps_stall_speed=60.000000
[exits]
number_of_exits=1
exit_rate.0=0.2 ;Percent per second
[ELECTRICAL]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 30.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 12
gear_motor = 0, 5 , 12
autopilot = 1, 5 , 12
avionics_bus = 0, 10 ,17
avionics = 1, 5 , 12
pitot_heat = 0, 2 , 12
additional_system = 0, 20 ,12
marker_beacon = 0, 2 , 12
gear_warning = 0, 2 , 12
fuel_pump = 0, 5 , 12
starter1 = 0, 20, 12
starter2 = 0, 20, 17
light_nav = 0, 5 , 12
light_beacon = 0, 5 , 12
light_landing = 0, 15, 12
light_taxi = 0, 5 , 12
light_strobe = 0, 5 , 12
light_panel = 3, 5 , 12
hydraulic_pump = 0, 2 , 12
light_recognition = 0, 5 , 12
light_wing = 0, 5 , 12
light_logo = 0, 5 , 12
[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[fuel]
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
LeftMain=-15.000000,-4.000000,0.000000,25.000000,0.000000
LeftAux=-24.000000,-4.000000,-2.000000,4.50000,0.000000
RightMain=-15.000000,4.000000,0.000000,25.000000,0.000000
RightAux=-24.000000,4.000000,-2.000000,4.50000,0.000000
[airplane_geometry]
wing_area = 300.0 //Square feet
wing_span = 15 //Feet
wing_root_chord = 20 //Feet
wing_dihedral = 0 //Degrees
wing_incidence = 0 //Degrees
wing_twist = 0 //Degrees
oswald_efficiency_factor= 8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 0 //Degrees, wing leading edge
wing_pos_apex_lon = -12 //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 = 55.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -18.1 //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 = 55.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -18.0 //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 = 10.0 //Square feet
aileron_area = 5.5 //Square feet
rudder_area = 3.3 //Square feet
elevator_up_limit = 27.0 //Degrees
elevator_down_limit = 17.5 //Degrees
aileron_up_limit = 9.0 //Degrees
aileron_down_limit = 9.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 13.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
[contact_points]
//0 Class 0=Unused 1=Wheel 2=Scrape Point
//1 Longitudinal Position (feet) + = forward - = aft
//2 Lateral Position (feet) + = right - = left
//3 Vertical Position (feet) + = Up - = down
//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) (Landing gear) in org file first 3 positions 0.500000
//12 Retraction Time (seconds) (landing gear) in org file first 3 positions 0.500000
//13 Sound Type
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//wheel points
point.0=1, 3.00, 0, -4.0, 1500, 0, 0.596, 60, 0.196, 2, 0.9516, 4.8, 4.8, 0, 184.0, 184.0
point.1=1, -16.67, -3, -4.8, 1500, 1, 0.596, 0.0, 0.642, 1.5, 0.8152, 4.5, 5.2, 2, 184.0, 184.0
point.2=1, -16.67, 3, -4.8, 1500, 2, 0.596, 0.0, 0.642, 1.5, 0.8152, 4.8, 4.9, 3, 184.0, 184.0
//Scrape points
point.3=2, -3.33, -16.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.33, 16.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -18.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 18.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
//Floating
point.7=4, -4.00, -5.250, -2.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
point.8=4, -4.00, 5.250, -2.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.9=4, -26.35, -5.250, -0.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.10=4, -26.35, 5.250, -0.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
static_pitch = -.84 //degrees (pitch when loaded on ground)
static_cg_height= 3.714 //feet, altitude of CG when at rest on the ground
gear_system_type= 1
[Flaps.0]
type=1
span-outboard=0.800000
extending-time=4.000000
system_type=0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar = 0.42
drag_scalar = .45
pitch_scalar= 0.93
flaps-position.0=0
flaps-position.1=5
flaps-position.2=10
flaps-position.3=23
flaps-position.4=31
flaps-position.5=39
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.5 = 22 // degrees
damaging-speed = 0 // KIAS
blowout-speed = 0 // KIAS
lift_scalar = 0.42
drag_scalar = 0.45
pitch_scalar= 0.93
system_type = 0 //Hydraulic
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,150.000000
rudder=150.000000,250.000000
[Views]
eyepoint= 0.14, 0.00, 0.85 //(feet) longitudinal, lateral, vertical distance from reference datum
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=3500.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=0
use_no_default_bank=1
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.200000
nav_proportional_control=11.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=.5
[direction_indicators]
direction_indicator.0=3,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_tchdrt
touchdown=fx_tchdwn_s, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -8.17, 6.25, 3.10, fx_navgre
light.1 = 3, -8.27, -6.25, 3.10, fx_navred
light.2 = 2, -8.17, -6.25, 3.10, fx_strobe
light.3 = 2, -8.27, 6.25, 3.10, fx_strobe
light.4 = 1, -9.85, 0.00, 3.55, fx_beacon
light.5 = 4, 6.85, 1.80, -0.90, fx_vclighth
light.6 = 4, 6.85, -1.80, -0.90, fx_vclighth
light.7 = 4, -2.50, 0.00, 2.00, fx_vclighth
light.8 = 4, 0.60, 0.00, 1.20, fx_vclighth
[SMOKESYSTEM]
smoke.0=-8.17, 6.25, 3.10, fx_smoke_r
smoke.1=-8.27, -6.25,3.10, fx_smoke_y
//smoke.2=-8.50, 0.00, 27.00, fx_smoke_p
//smoke.3=-8.50, 0.00, -9.00, fx_smoke_g
//smoke.4=-8.50, 0.00, 9.00, fx_smoke_o
//smoke.5=-8.50, 0.00, -18.00, fx_smoke_l
//smoke.6=-8.50, 0.00, 18.00, fx_smoke_b
[brakes]
toe_brakes_scale=1
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
