// AI Helicopter configuration files // by Rob Nieuwenhoven (rjnieuwe@optusnet.com.au) based on the work //of Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2004 // // for Hovercontrol BellHuey2 // by Jordan Moore, webmaster@hovercontrol.com // // based on Stemme motor glider aircraft.cfg // by Al Kaiser, kaiser@va-works.com or http://www.va-works.com/ // // !!!Copyright remains with the original authors!!! [fltsim.0] title=AIBellHuey2 "AAAvn" sim=stemme_as_helicopter_1 model=1 panel= sound= texture=AAAvn kb_checklists= prop_anim_ratio=1.46 atc_airline=Iroquois atc_parking_types=RAMP atc_parking_codes=UH1 visual_damage=1 description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max [fltsim.1] title=AIBellHuey2 "1st Cav Div" sim=stemme_as_helicopter_1 visual_damage=1 model= panel= sound= texture=US Army kb_checklists=Bell_UH-1H_check kb_reference=Bell_UH-1H_ref prop_anim_ratio=1.46 atc_id_color=0xc6eff7ff atc_id=65-11833 atc_parking_types=MIL_COMBAT,RAMP atc_parking_codes=UH1 description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max [fltsim.2] title=AI BellHuey sim=stemme_as_helicopter_1 model= panel= sound= texture= kb_checklists= prop_anim_ratio=1.46 atc_airline=Iroquois atc_parking_codes=UH1 atc_parking_types=MIL_COMBAT visual_damage=1 description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max [General] atc_type=BELL atc_model=UH1 performance=Cruise Speed\t115 kts\nMaximum Range\t435 nm\nService Ceiling\t20,000 ft\nHovering Ceiling\t19,600\nMax Gross Weight \t3,200 lb\nHook Load Limit \t1, 500 Ib\nSeating\t\tUp to 5\nUseful Load\t1,498 lb\n //---- misc tweaked parameters [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position= 0.000,0.000,-2.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 max_gross_weight=2300 // (pounds) empty_weight=1300 ;Moments of Inertia empty_weight_pitch_MOI=3000 empty_weight_roll_MOI=4000 empty_weight_yaw_MOI=9000 empty_weight_coupled_MOI=-1000 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=15 full_flaps_stall_speed=12 cruise_speed=80 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=1.15 // was 1.15 parasite_drag_scalar=0.8 // was 0.8 induced_drag_scalar=0.8 // was 0.8 elevator_effectiveness=1.5 // was 1.0 aileron_effectiveness=1.0 rudder_effectiveness=2.0 // was 1.5 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=1.9 // was 1.0 [flaps.0] //Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.600 // 0.0 .. 1.0 extending-time=4.000 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=1.3 drag_scalar=0.8 pitch_scalar=1.2 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None //---- parameters from Bell Huey2, tweaked //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] point.0=1.000, 5.830, 4.330, -4.500, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=1.000, -5.500, -4.330, -4.580, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=1.000, -5.500, 4.330, -4.580, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000 point.3=1.000, 5.830, -4.330, -4.500, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 1.000, 0.000, 0.000 //point.0=3.000, 5.830, 4.330, -4.500, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 //point.1=3.000, -5.500, -4.330, -4.580, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 2.000, 0.000, 0.000 //point.2=3.000, -5.500, 4.330, -4.580, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000 //point.3=3.000, 5.830, -4.330, -4.500, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 1.000, 0.000, 0.000 //point.4=2.000, 0.000, -19.670, 10.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //point.5=2.000, 0.000, 19.670, 10.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //point.6=2.000, -27.500, 0.000, 0.670, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //point.7=2.000, 0.000, 9.080, 2.580, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.198 static_cg_height=4.294 [Views] eyepoint=1.8, 1.5, 2.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.60, -3.80, 2.95, fx_navred , light.1=3, 0.60, 3.80, 2.95, fx_navgre , light.2=3, -27.15, 0.00, 1.75, fx_navwhi , light.3=2, -6.57, 0.00, -2.34, fx_strobe , light.4=2, -6.57, 0.00, 4.37, fx_strobe , light.5=2, -6.57, 0.00, -2.34, fx_navred , light.6=2, -6.57, 0.00, 4.37, fx_navred , light.7=4, 6.8, 0.00, 1.6, fx_vclight , light.8=3, 7.15, -2.50, -2.50, fx_navred , light.9=3, 7.15, 2.50, -2.50, fx_navgre , light.10=3, 2.10, 0.00, -2.84, fx_navwhi , [effects] water=fx_spray dirt = fx_tchdrt concrete = fx_tchdrt, 1 touchdown = fx_dustcloud_m, 1 startup=fx_engstrt //touchdown = fx_tchdwn, 1 //landrotorwash = fx_rtr_lnd //waterrotorwash = fx_rtr_wtr contrail=fx_contrail_l [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second //---- parameters from Stemme motor glider, tweaked [fuel] LeftMain=-0.250000,-2.100000,2.500000,6.000000,0.000000 RightMain=-0.250000,2.100000,2.500000,6.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=400 // was 201.0 wing_span=60 // was 57.0 wing_root_chord=4.916670 wing_dihedral=3.499146 wing_incidence=4.999268 // was 2.999268 wing_twist=-1.994019 oswald_efficiency_factor=.448140 // was 1.064814 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=16.000000 htail_span=7.916667 htail_pos_lon=-16.083333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=16.000000 vtail_span=4.560702 vtail_sweep=0.000000 vtail_pos_lon=-14.750000 vtail_pos_vert=4.166667 elevator_area=15.000000 aileron_area=11.740000 rudder_area=6.000000 elevator_up_limit=30.0 // was 25.000447 elevator_down_limit=18.998903 aileron_up_limit=17.996227 aileron_down_limit=13.000035 rudder_limit=20.995472 elevator_trim_limit=10.0 // was 19.497754 spoiler_limit=70 spoilerons_available=1 // was 0 aileron_to_spoileron_gain=0.0005 // was 0 min_ailerons_for_spoilerons=0.005 // was 0 min_flaps_for_spoilerons=0.005 // was 0 [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 fuel_flow_scalar=1.00 min_throttle_limit=0.000000 max_contrail_temperature=-27 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=100.300000 compression_ratio=6.0 number_of_cylinders=6 // was 2 max_rated_rpm=3500 // was 2700 max_rated_hp=200 // was 115 fuel_metering_type=1 cooling_type=0 // was 1 normalized_starter_torque=0.3 turbocharged=0 max_design_mp=0.0 min_design_mp=0.0 critical_altitude=0.0 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 // Propeller thrust scalar propeller_type=2 // was 0 propeller_diameter=8.000 // was 5.433000 propeller_blades=2 propeller_moi=20.50000 // was 3.350000 beta_max=29.800000 beta_min=4.000000 // was 17.000000 min_gov_rpm=50.000000 // was 700.000000 prop_tc=0.4 // was 0.004000 gear_reduction_ratio=1.10 // was 1.0 fixed_pitch_beta=0 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=0 beta_feather=90.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 // was 1 prop_reverse_available=1 // was 0 minimum_on_ground_beta=2.0 // was 0 minimum_reverse_beta=0.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=500.000000 // was 700 autothrottle_available=0 pitch_takeoff_ga=-5.00 // was 8.0 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=25.000000 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=1,0 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
