[fltsim.0] title=Skydiver sim=Skydiver model= panel= sound= texture= kb_checklists=Skydiver_check kb_reference=Skydiver_ref atc_id=N0SKY ui_manufacturer=Tango Golf Aeronautics ui_type="Skydiver" ui_variation= description="This skydiver represents a 180 lb man in free fall using standard techniques for control and stability. At about 5000 ft you should change to the Parafoil. Steer with the stick and use the flaps (legs) and the gear (arms) to control speed." [General] atc_type=Skydiver atc_model=Man editable=0 performance="Max Terminal Speed\t\n133 kts 225 fps\n\nEngine\t\nnone\n\nGlide Ratio\t\n0.25 to 1\n\nEmpty Weight\t\n180 lb 454 kg\n\nLength\t\n6.0 ft \t 8.78 m\n\nWingspan\n2 ft\n\nWing Area\t\n12 sq ft\n\nAspect Ratio\t\n0.3" [WEIGHT_AND_BALANCE] max_gross_weight = 180 // (pounds) empty_weight = 180 // (pounds) reference_datum_position = 1.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.08, 0, 0.2 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "0, 0.0, 0.0, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 800 empty_weight_roll_MOI = 300 empty_weight_yaw_MOI = 900 empty_weight_coupled_MOI = 0.0 [electrical] electric_always_available=1 [flight_tuning] parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.3 aileron_effectiveness = 1.8 rudder_effectiveness = 1.8 pitch_stability = 1.0 roll_stability = 1.5 yaw_stability = 1.5 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 2 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop fuel_flow_scalar = 0 //Fuel flow scalar [pitot_static] vertical_speed_time_constant = 4 //Increasing this value will cause a more instantaneous reaction in the VSI //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, -2.0, -1.5, -2.5, 1574.8, 2, 0.509, 0.0, 0.40, 2.5, 1.00, 2.0, 2.0, 3, 0.0, 0.0 point.1=1, -2.0, 1.5, -2.5, 1574.8, 2, 0.509, 0.0, 0.40, 2.5, 1.00, 2.0, 2.0, 3, 0.0, 0.0 point.2=2, -1.25, -28.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.3=2, -1.25, 28.5, 0.5, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.4=2, -15.42, 0.0, -0.7, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0 point.5=2, 6.25, 0.0, -2.2, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = -4.65 static_cg_height = 2.17 gear_system_type=0 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.67 //Brake scalar [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 lift_scalar=2.00 drag_scalar=1.00 pitch_scalar=1.0 flaps-position.0=0.000000,0.000000 flaps-position.1=35.00,0.000000 flaps-position.2=70.000,0.000000 [SMOKESYSTEM] smoke.0= -2.623, 0.156, -2.157, fx_smoke_w smoke.1= -2.623, 0.156, 2.157, fx_smoke_r [fuel] electric_pump=0 fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint = 1.063, 0.0, 1.435 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 2.7, 0.00, 1.50, fx_vclight, [flaps.0] type = 0 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 0 // seconds flaps-position.0 = 0 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [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 = 160, 360 aileron = 160, 360 rudder = 160, 360 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [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_tchdwn_s [airplane_geometry] wing_area = 12.0 //Square feet wing_span = 2.0 //Feet wing_root_chord = 6.0 //Feet wing_dihedral = 2.0 //Degrees wing_incidence = 3.0 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 0.5 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -0.5 //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 = 4.0 //Square feet htail_span = 2.9 //Feet htail_pos_lon = -12.3 //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 = 0.0 //Degrees, horizontal tail leading edge vtail_area = 4.0 //Square feet vtail_span = 4.0 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon = -12.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 0.9 //Feet, vertical distance from reference point, positive going up elevator_area = 3.0 //Square feet aileron_area = 8.7 //Square feet rudder_area = 4.0 //Square feet elevator_up_limit = 26.0 //Degrees elevator_down_limit = 26.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 30.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 70.0 //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 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 40.0 //Knots True (KTAS) full_flaps_stall_speed = 40.0 //Knots True (KTAS) cruise_speed = 47.0 //Knots True (KTAS) max_indicated_speed = 158 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [forcefeedback] ground_bumps_magnitude1=2500 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=10.0 ground_bumps_slope1=0.300 ground_bumps_magnitude2=350 ; 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