// AI Helicopter configuration files // by Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2003 // // for Sikorsky UH-60 Blackhawk GMax // by Daniel M. Dunn, dd@bac-f6.com // // tweaked for AS332 Super Puma from Brian Franklin // Nov 2004 // // 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=Puma 33 Sqn sim=stemme_as_helicopter_2 model= panel= sound= texture=RAF-Royal Air Force 33sqn ui_manufacturer=Aerospatiale ui_type=Puma HC1 ui_variation=RAF Royal Air Force 33sqn description=Battlefield support helicopter of the Royal Air Force prop_anim_ratio=1.1 [fltsim.1] title=Puma 230 Sqn sim=stemme_as_helicopter_2 model= panel= sound= texture=RAF-Royal Air Force 230sqn kb_checklists= ui_manufacturer=Aerospatiale ui_type=Puma HC1 ui_variation=RAF Royal Air Force 230sqn description=Battlefield support helicopter of the Royal Air Force prop_anim_ratio=1.1 [fltsim.2] title=COUGAR FAV sim=stemme_as_helicopter_2 model= panel= sound= texture=FAV ui_manufacturer=Aerospatiale ui_type=AS552 COUGAR ui_variation=Grupo Aereo de Operaciones Especiales N°10 description=Ba. Libertador, Maracay. Edo. Aragua - Grupo Aéreo de Operaciones Especiales No. 10.\n\nTexturas Daniel Borrego prop_anim_ratio=1.1 atc_heavy=0 atc_id=FAV0121 atc_airline=FAV atc_flight_number=0121 [fltsim.3] Title=AS332 ORF-Oman Royal Flight Sim=stemme_as_helicopter_2 Model= Panel= Sound= Texture=ORF-Oman Royal Flight Atc_id_color=0xc6eff7ff Atc_id= Ui_manufacturer=Aerospatiale Ui_type=AS332 Super Puma Ui_variation=Oman Royal Flight Atc_flight_number=332 Atc_heavy=0 Atc_airline=OMAN Description=altered for AI helicopters project by Holger Sandmann\s braking strength set to max and 'dummy' engine added prop_anim_ratio=1.1 atc_parking_codes=AS32,M004 atc_parking_types=RAMP [General] atc_type=AEROSPATIALE atc_model=AS32 performance=Cruise Speed 149 kts @ 3750 kg\nMaximum Range 483 nm @ 3750 kg\nService Ceiling >15 000 ft\nHovering Ceiling 10 203 ft, O.G.E.\nMax Gross Weight 4300 kg\nHook Load Limit 1600 kg\nSeating 1-2 pilots + 11 passengers\nUseful Load 1944 kg //---- misc tweaked parameters [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 max_gross_weight=1450 // (pounds) empty_weight=550 ;Moments of Inertia empty_weight_pitch_MOI=2600 empty_weight_roll_MOI=2400 empty_weight_yaw_MOI=5010 empty_weight_coupled_MOI=0.0 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=40 full_flaps_stall_speed=35 cruise_speed=149.0 //cruise_speed=115 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=0.7 // was 1.0 parasite_drag_scalar=0.5 // was 1.0 induced_drag_scalar=0.5 // was 1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 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 //---- parameters from Sikorsky, 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, -8.00, 0.000, -4.35, 3875.173, 0.000, 0.523, 90.000, 0.366, 2.500, 1.173, 3.000, 3.000, 0.000, 0.000, 0.000 point.1= 1.000, 10.917, -7.833, -4.35, 3875.173, 1.000, 0.523, 0.000, 0.538, 2.500, 1.309, 3.000, 3.000, 2.000, 0.000, 0.000 point.2= 1.000, 10.917, 7.833, -4.35, 3875.173, 2.000, 0.523, 0.000, 0.538, 2.500, 1.309, 3.000, 3.000, 3.000, 0.000, 0.000 static_pitch = 0 static_cg_height = 2.294003 gear_system_type=0 [Views] eyepoint = 12, 2, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -6.88, -7.10, -0.00, fx_navred , light.1 = 3, -6.88, 7.10, -0.00, fx_navgre , light.2 = 3, -44.98, 0.00, 13.00, fx_navwhi , light.3 = 1, -42.00, 0.44, 14.34, fx_beacon , light.5 = 4, 2.00, 0.00, 1.50, fx_vclight , light.6=5, 13.70, 0.00, -1.60, fx_navwhih , [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 wake=fx_wake [exits] number_of_exits=8 exit_rate.0=1 exit_rate.1=1 exit_rate.2=1.2 exit_rate.3=1.2 exit_rate.4=1.3 exit_rate.5=1.3 exit_rate.6=1.4 exit_rate.7=1.4 //---- 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=280 // was 201.000000 wing_span=57.000000 wing_root_chord=4.916670 wing_dihedral=3.499146 wing_incidence=3.999268 // was 2.999268 wing_twist=-1.994019 oswald_efficiency_factor=1.564814 // 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=20.000447 //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=25.0 //was 19.497754 spoiler_limit=70.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=0 Engine.0=6.000000,0.000000,0.000000 Engine.1=6.000000,0.000000,0.000000 // 'dummy' for tail rotor fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=100.300000 compression_ratio=6.000000 number_of_cylinders=2 max_rated_rpm=2700.000000 max_rated_hp=45.000000 // was 115 fuel_metering_type=1 cooling_type=1 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 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=0 propeller_diameter=5.433000 propeller_blades=2 propeller_moi=3.350000 beta_max=29.800000 beta_min=17.000000 min_gov_rpm=700.000000 prop_tc=0.004000 gear_reduction_ratio=1.000 fixed_pitch_beta=0.000000 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=0.000000 beta_feather=90.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=1 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] default_bank_mode=0 default_pitch_mode=0 autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 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=1,0 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=15.996982 flap_limit_idle=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=0.500000 system_type=3 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 // //Default FF Code installed by FFUtil 18:32:18 04-23-2004
