[fltsim.0]
title=SkycarM400Pro
sim=SCm400Pro
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=SkycarM400pro_ref
description=Model_Dynamicks_3D VRpanel cockpit by AC Kerkhove.\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.\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_Production_Type
ui_variation=Standaard_RED
atc_heavy=0
atc_id=SCV5
atc_airline=Skycar International
atc_flight_number=01
[fltsim.1]
title=SkycarM400Cheetha
sim=SCm400Pro
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=SkycarM400pro_ref
description=Model_Dynamicks_3D VRpanel cockpit by AC Kerkhove.\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.\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_Production_Type
ui_variation=Cheetha WNF
atc_heavy=0
atc_id=SCWNF
atc_airline=Skycar WNF
atc_flight_number=01
[fltsim.2]
title=SkycarM400_Police
sim=SCm400Pro
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=SkycarM400pro_ref
description=Model_Dynamicks_3D VRpanel cockpit by AC Kerkhove.\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.\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_Production_Type
ui_variation=Police
atc_heavy=0
atc_id=SCV5
atc_airline=Police
atc_flight_number=01
[fltsim.3]
title=SkycarM400Alternatief
sim=SCm400Pro
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=SkycarM400pro_ref
description=Model_Dynamicks_3D VRpanel cockpit by AC Kerkhove.\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.\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_Production_Type
ui_variation=Alternatief
atc_heavy=0
atc_id=SCV5
atc_airline=Skycar International
atc_flight_number=01
[General]
performance=Length:21.49 ft\nSpan:18.47 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. 330MPh\nDesigner: Dr. P Moller
atc_type=Sky Car
atc_model=M400
[turboprop_engine]
power_scalar=50
[propeller]
thrust_scalar=0.20 // was 0.9
propeller_type=1
propeller_diameter=4 // was 0
propeller_blades=8 // was 2
propeller_moi=5.706520
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=180.000000 // was 80.000000
prop_sync_available=1 // was 0
prop_deice_available=1
prop_feathering_available=0
prop_auto_feathering_available=1
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[ground_reaction]
//main_gear_static_compression = 5.2 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression = 5.2 // (feet), The distance the center gear strut is compressed when at rest on the ground
//main_gear_damping_ratio = 0.7 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio = 1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[weight_and_balance]
max_gross_weight = 2400
empty_weight = 1000 0
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 6000
empty_weight_roll_MOI = 4000
empty_weight_yaw_MOI = 10000
empty_weight_coupled_MOI = 1200
max_number_of_stations = 1
station_load.0 = 0.000000,0.000000,0.000000,0.000000
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 6.85, 1.80, -0.90, fx_vclighth
light.1 = 4, 6.85, -1.80, -0.90, fx_vclighth
light.2 = 4, -2.50, 0.00, 2.00, fx_vclighth
light.3 = 4, 0.60, 0.00, 1.20, fx_vclighth
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 3
fuel_flow_scalar = 1.000
engine.0 = -0.01, 0, 6.40,
engine.1 = -25.67, -0.66, 4.05,
min_throttle_limit=0.000000
[SMOKESYSTEM]
smoke.0=-6.984908, -3.946850, -0.738189, fx_smoke_w
smoke.1=-6.984908, 3.946850, -0.738189, fx_smoke_w
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
Center1 = 0, 0, 0, 91, 0
electric_pump=0
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//Wheels
point.0 =1, 8.22, -0.01, -4.00, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.1 =1, -3.19, 2.46, -4.00, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.2 =1, -3.19, -2.46, -4.00, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
//Scrape
point.3 = 2, 10.496, 0.000,-1.290, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.4 = 2, -4.220, 9.328, 0.566, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.5 = 2, -4.220,-9.346, 0.566, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
point.6 = 2,-11.379, 0.000,-0.556, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0
//
point.7 = 5, 0.0, 0.0, 0.0, 0, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 1.0, 1.2, 0, 0.0, 0.0
static_pitch = 0.0000 //degrees (pitch when loaded on ground)
static_cg_height=3.644 //feet, altitude of CG when at rest on the ground
max_number_of_points = 5
gear_system_type=0
[TailHook] tailhook_length=0 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.0
[keyboard_response]
elevator = 100.000, 180.000
aileron = 200.000, 1000.000
rudder = 200.000, 1000.000
[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
wing_winglets_flag = 0
spoilerons_available =0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 1
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[Views]
eyepoint= 0.899427 -0.884650 0.957950 //(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=1,0
Nav.1=1,1,1
Nav.2=1,1,0
Adf.1=1,0
Transponder.1=1
Marker.1=1
[Reference Speeds]
flaps_up_stall_speed=54.000
full_flaps_stall_speed=43.200
cruise_speed=0.000
max_indicated_speed=1000.000000
//[exits]
//number_of_exits=2
//exit_rate.0=0.8
//exit_rate.1=0.8
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.001
autothrottle_available=1
pitch_takeoff_ga=0.000000
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
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=0.000000[direction_indicators]
direction_indicator.0=3,0yaw_damper_gain=0.000000
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.4 // was 1.0
induced_drag_scalar = 0.4 // was 1.0
rudder_effectiveness = 1.2 // was 1.0
pitch_stability = 1.0
roll_stability = 2.0 // was 1.0
yaw_stability = 1.0
elevator_effectiveness = 1.2
aileron_effectiveness = 1.5
[MainRotor]
number_of_blades=0.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.000000
inflow_vel_reference=0.000000
[SecondaryRotor]
number_of_blades=0.000000
weight_per_blade=0.000000
weight_to_moi_factor=0.000000
inflow_vel_reference=0.000000
[Helicopter]
reference_length=0.000000
reference_frontal_area=0.000000
reference_side_area=0.000000
side_aero_center=0.000000
right_trim_scalar=1.000000
correlator_available=1.000000
governed_pct_rpm_ref=1.000000
rotor_brake_scalar=1.000000
torque_scalar=1.000000
cyclic_roll_control_scalar=1.000000
cyclic_pitch_control_scalar=1.000000
pedal_control_scalar=1.000000
collective_on_rotor_torque_scalar=1.000000
[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=0.000000
roll_damp_cf=0.000000
yaw_damp_cf=0.000000
yaw_stability_cf=0.000000
[pitot_static]
vertical_speed_time_constant = 1 //try a value larger than 1
