// AI Helicopter configuration file by Mike MacIntyre using a technique by Ron Nieuwenhoven // // Based on the original work of Holger Sandmann (hsandman@sfu.ca) and Doug Callihan // // Version 1, May 2003 // // For Boeing Vertol Chinook v1.0 GMax // by Tom Woods and Mark Adams // // Developed from the open scource G-max files by Rory Kelly // // 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 CH47 HAA_green sim=NEM_CH47D_AI_Only model= panel= sound= texture=HAA_green prop_anim_ratio=-1.76 atc_id=ES892 ui_manufacturer=Boeing ui_type=CH-47 ui_variation=Hellenic Army (Green Colors) description=The Chinook by Tom Woods and Mark Adams. atc_airline=ARMY atc_parking_codes=CH47,M004 atc_parking_types=RAMP [fltsim.1] title=MHAI CH47 HAA_camo sim=NEM_CH47D_AI_Only model= panel= sound= texture=HAA_camo prop_anim_ratio=-1.76 atc_id=ES882 ui_manufacturer=Boeing ui_type=CH-47 ui_variation=Hellenic Army (Camo Colors) description=The Chinook by Tom Woods and Mark Adams. atc_airline=ARMY atc_parking_codes=CH47,M004 atc_parking_types=RAMP [General] atc_type=SIKORSKY atc_model=CH47 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, 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=235 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, -9.650, -5.250, -7.200, 3000, 1.0, 1.13, 0.001, 0.40, 2.50, 0.60, 0.0, 0.0, 2.0, 0.0, 0.0 point.1=1, -9.650, 5.250, -7.200, 3000, 2.0, 1.13, 0.001, 0.40, 2.50, 0.60, 0.0, 0.0, 3.0, 0.0, 0.0 point.2=1, 12.650, 5.250, -6.200, 3000, 0.0, 1.13, 30.00, 0.40, 2.50, 0.80, 0.0, 0.0, 0.0, 0.0, 0.0 point.3=1, 12.650, -5.250, -6.200, 3000, 0.0, 1.13, 30.00, 0.40, 2.50, 0.80, 0.0, 0.0, 1.0, 0.0, 0.0 static_pitch=-2.0 gear_system_type=1 static_cg_height=6.7 [Views] eyepoint = 12, 2, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, 12.847, -6.158, -1.777, fx_navred light.1=3, 12.847, 6.000, -1.777, fx_navgre light.2=3, -18.841, 0.077, 4.499, fx_navwhi light.3=1, 8.6, 0.0, -3.8, fx_beacon light.4=1, -17.2, 0.0, 9.5, fx_beacon light.5=4, 27.5, -1.7, 2.5, fx_vclight light.6=4, 27.5, 1.7, 2.5, fx_vclight light.7=2, 8.6, 0.0, -3.8, fx_strobe , light.8=2, -17.2, 0.0, 9.5, fx_strobe , [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 [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=90.000000 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=250 //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=1 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] 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
