// AI Helicopter configuration files // by Holger Sandmann (hsandman@sfu.ca) // and Doug Callihan // // Version 1, May 2003 // // for Aerospatiale/Eurocopter AS365N3 Dauphin GMax // by Antti Pankkonen, apankkon@cc.hut.fi // // 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 AS65 HCG sim=stemme_as_helicopter_2 model= panel= sound= texture=HCG atc_id=CH35 atc_model=AS 365 Atc_airline=COAST GUARD ui_manufacturer=Eurocopter ui_type=AS 365 N3 Dauphin ui_variation=Hellenic Coast Guard prop_anim_ratio=1.41 description=The AS 365 is a medium-weight multipurpose twin-engine helicopter. In addition to technological innovations (main and rear rotor blades made of composite materials, tail rotor built in the fin...), the reliability and availability of this helicopter are highly valued worldwide. The AS 365 N3 is equipped with two Turbomeca Arriel 2C engines which offer remarkable performance. This engine is equipped with an Full Authority Digital Electronic Control (FADEC). atc_parking_codes=AS65,M004 atc_parking_types=RAMP [General] atc_type=Aerospatiale atc_model=AS365 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,-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=30 full_flaps_stall_speed=27 cruise_speed=115 max_indicated_speed=180.000000 [flight_tuning] cruise_lift_scalar=1.25 // 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 AS365 Dauphin, 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, -21.2, 0.0, -0.4, 3500.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.0=1, 9.25, 0.0, -2.56, 3378.0, 0.0, 0.984, 90.0, 0.96, 1.25, 1.260614, 1.0, 1.0, 0 point.1=1, -3.0, -3.33, -3.38, 3378.0, 1.0, 1.148, 0.0, 0.86, 1.35, 1.416001, 1.5, 1.5, 2 point.2=1, -3.0, 3.33, -3.38, 3378.0, 2.0, 1.148, 0.0, 0.86, 1.35, 1.416001, 1.5, 1.5, 3 //point.1=1, 9.25, 0.0, -2.56, 3378.0, 0.0, 0.984, 90.0, 0.96, 1.25, 0.226892, 1.0, 1.0, 0 //point.2=1, -3.0, -3.33, -3.38, 3378.0, 1.0, 1.148, 0.0, 0.86, 1.35, 0.329804, 1.5, 1.5, 2 //point.3=1, -3.0, 3.33, -3.38, 3378.0, 2.0, 1.148, 0.0, 0.86, 1.35, 0.329804, 1.5, 1.5, 3 //point.4=2, 11.0, 0.0, 1.0, 1000.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4 //point.5=2, -22.0, 0.0, 1.5, 1000.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 //point.6=2, 0.0, -19.0, 7.3, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5 //point.7=2, 0.0, 19.0, 7.3, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6 static_pitch=-5.000000 static_cg_height=2.294003 gear_system_type=3 [Views] eyepoint=-0.72,1.4,3.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -16.6, -5.30, 0.90, fx_navred , light.1=3, -16.6, 5.30, 0.90, fx_navgre , light.2=3, -25.4, 0.00, 0.90, fx_navwhi , light.3=1, -24.2, -0.20, 9.30, fx_beacon , light.4=4, 1.00, -1.00, 1.50, fx_vclight , light.5=4, -4.50, 0.00, 1.30, fx_vclight , light.6=4, 1.00, 1.00, 1.50, fx_vclight , [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 //---- 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=8.3 Engine.1=8.3 // 'dummy' for tail rotor fuel_flow_scalar=1.00 min_throttle_limit=0.000000 [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=100.0 // 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 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=15.996982 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
