// AI Helicopter configuration files // by Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2003 // // for Bell 205 UH-1H "Iroquois" GMax // by Vladimir Zhyhulskiy, zh@selena.kherson.ua // //changed for UH1 Deane Baunton // // 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=MHAI UH1H HAF_SAR sim=stemme_as_helicopter_1 model= texture=HAF_SAR prop_anim_ratio=-1.76 atc_airline=AIR FORCE atc_flight_number=7089 atc_id=7089 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Air Force SAR description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=MHAI UH1H HAA_olive_1 sim=stemme_as_helicopter_1 model= texture=HAA_olive_1 prop_anim_ratio=-1.76 atc_airline=ARMY atc_flight_number=7149 atc_id=7149 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Army (olive) description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [fltsim.2] title=MHAI UH1H HAA_olive_2 sim=stemme_as_helicopter_1 model= texture=HAA_olive_2 prop_anim_ratio=-1.76 atc_airline=ARMY atc_flight_number=7149 atc_id=7149 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Army (olive 2) description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_font=Verdana,-11,1,600,0 [fltsim.3] title=MHAI UH1H HAA_camo sim=stemme_as_helicopter_1 model= texture=HAA_camo prop_anim_ratio=-1.76 atc_airline=ARMY atc_flight_number=7149 atc_id=7149 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Army (camo) description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_font=Verdana,-11,1,600,0 [fltsim.4] title=MHAI B212 HAF_VIP sim=stemme_as_helicopter_1 model= texture=HAF_VIP prop_anim_ratio=-1.76 atc_airline=Hellenic Air Force atc_flight_number=190 atc_id=31190 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Air Force VIP description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_font=Verdana,-11,1,600,0 [fltsim.5] title=MHAI B212 HN sim=stemme_as_helicopter_1 model= texture=HN prop_anim_ratio=-1.76 atc_airline=NAVY atc_flight_number=190 atc_id=31190 atc_heavy=0 ui_manufacturer=Bell ui_type=UH1H ui_variation=Hellenic Navy description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max atc_parking_codes=UH1,M004 atc_parking_types=MIL_COMBAT atc_id_font=Verdana,-11,1,600,0 [General] atc_type=BELL atc_model=UH1 performance=rotor width 14.63 meters footprint length 17.62 meters \n fuselage length 12.77 meters height 4.41 meters \n mpty weight 2,365 kilograms max loaded weight 4,310 kilograms maximum speed 205 KPH \n service ceiling 3,840 meters //---- misc tweaked parameters editable=0 [weight_and_balance] // ACM V2.5 max_gross_weight = 2300 empty_weight = 1300 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, -2 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 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 = 3, 9.95, -3.9, 5.25, fx_navred , light.1 = 3, 9.95, 3.9, 5.25, fx_navgre , light.2 = 1, 1.38, 0.00, 7.60, fx_beacon , light.3 = 3, -18.52, 0.00, 6.37, fx_navwhi , light.4 = 3, 13.90, 3.50, 0.6, fx_navgre , light.5 = 3, 13.90, -3.50, 0.6, fx_navred , light.6 = 4, 17.0, 1.80, 3.2, fx_vclight , light.7 = 4, 17.0, -1.80, 3.2, fx_vclight , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.00 min_throttle_limit = 0.000000 engine.0 = 6.000000,0.000000,0.000000 [effects] water = fx_spray //dirt = fx_tchdrt //concrete = fx_tchdrt, 1 //touchdown = fx_dustcloud_m, 1 startup = fx_engstrt windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 1 LeftMain = -0.25, -2.1, 2.5, 6, 0 RightMain = -0.25, 2.1, 2.5, 6, 0 [contact_points] static_pitch = 3 static_cg_height = 2.2 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 8 point.0 = 1, 6, 8.33, -2.4, 5600, 0, 0.519, 90, 0.5, 0.75, 0.85, 0, 0, 3, 0, 0 point.1 = 1, -8.5, -8.33, -1.95, 5600, 1, 0.519, 90, 0.5, 0.75, 0.85, 0, 0, 2, 0, 0 point.2 = 1, -8.5, 8.33, -1.95, 5600, 2, 0.519, 90, 0.5, 0.75, 0.85, 0, 0, 3, 0, 0 point.3 = 1, 6, -8.33, -2.4, 5600, 0, 0.519, 90, 0.5, 0.75, 0.85, 0, 0, 2, 0, 0 [keyboard_response] elevator = 100.000000, 180.000000 aileron = 200.000000, 1000.000000 rudder = 200.000000, 1000.000000 [airplane_geometry] //ACM_AREAW1// 0,0,0,1.4986,1.0160,1.0160,0,1.4236,2.0320,2.0320 //ACM_AREAW2// 0,1.3487,3.0480,3.0480,0,1.2738,4.0640,4.0640,0,1.1988 //ACM_AREAW3// 5.0799,5.0799,0,1.1239,6.0960,6.0960,0,1.0490,7.1119,7.1119 //ACM_AREAW4// 0,0.9740,8.1280,8.1280,0,0.8991,9.1440,9.1440,0,0.8242 //ACM_AREAH1// 0,0,0,0.8043,0.1340,0.1340,0,0.7641,0.2681,0.2681 //ACM_AREAH2// 0,0.7239,0.4021,0.4021,0,0.6836,0.5362,0.5362,0,0.6434 //ACM_AREAH3// 0.6702,0.6702,0,0.6032,0.8043,0.8043,0,0.5630,0.9383,0.9383 //ACM_AREAH4// 0,0.5228,1.0724,1.0724,0,0.4826,1.2065,1.2065,0,0.4423 //ACM_AREAV1// 0,0,0,1.3901,0.1544,0.1544,0,1.2788,0.3089,0.3089 //ACM_AREAV2// 0,1.1676,0.4633,0.4633,0,1.0564,0.6178,0.6178,0,0.9452 //ACM_AREAV3// 0.7722,0.7722,0,0.8340,0.9267,0.9267,0,0.7228,1.0811,1.0811 //ACM_AREAV4// 0,0.6116,1.2356,1.2356,0,0.5004,1.3901,1.3901,0,0.3892 //ACM_CAREAW1// 4.5720,4.5720,0.7493,1.0490,5.0799,5.0799,0.7493,1.0340,5.5879,5.5879 //ACM_CAREAW2// 0.7493,1.0190,6.0960,6.0960,0.7493,1.0040,6.6040,6.6040,0.7493,0.9890 //ACM_CAREAW3// 7.1119,7.1119,0.7493,0.9740,7.6199,7.6199,0.7493,0.9591,8.1280,8.1280 //ACM_CAREAW4// 0.7493,0.9441,8.6359,8.6359,0.7493,0.9291,9.1440,9.1440,0.7493,0.9141 //ACM_CAREAH1// 0,0,0.4021,0.8043,0.1340,0.1340,0.4021,0.7842,0.2681,0.2681 //ACM_CAREAH2// 0.4021,0.7641,0.4021,0.4021,0.4021,0.7440,0.5362,0.5362,0.4021,0.7239 //ACM_CAREAH3// 0.6702,0.6702,0.4021,0.7037,0.8043,0.8043,0.4021,0.6836,0.9383,0.9383 //ACM_CAREAH4// 0.4021,0.6635,1.0724,1.0724,0.4021,0.6434,1.2065,1.2065,0.4021,0.6233 //ACM_CAREAV1// 0,0,0.3475,1.0425,0.1544,0.1544,0.3475,0.9869,0.3089,0.3089 //ACM_CAREAV2// 0.3475,0.9313,0.4633,0.4633,0.3475,0.8757,0.6178,0.6178,0.3475,0.8201 //ACM_CAREAV3// 0.7722,0.7722,0.3475,0.7645,0.9267,0.9267,0.3475,0.7089,1.0811,1.0811 //ACM_CAREAV4// 0.3475,0.6533,1.2356,1.2356,0.3475,0.5977,1.3901,1.3901,0.3475,0.5421 wing_area = 400 wing_span = 60 wing_root_chord = 4.916670 wing_dihedral = 3.499146 wing_incidence = 4.999268 wing_twist = -1.994019 oswald_efficiency_factor = .448140 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 elevator_down_limit = 18.998903 aileron_up_limit = 17.996227 aileron_down_limit = 13.000035 rudder_limit = 20.995472 elevator_trim_limit = 10.0 spoiler_limit = 70 aileron_to_spoileron_gain = 0.0005 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0.005 min_flaps_for_spoilerons = 0.005 spoilerons_available = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 0 [Reference Speeds] flaps_up_stall_speed=30 full_flaps_stall_speed=27 cruise_speed=100 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 [Views] eyepoint=1.8, 1.5, 2.2 [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 [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 // 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 [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
