//////////////////////////////////////////////////////////////////////// //FLIGHT DYNAMICS CONFIGURATION FILE: EnigmaSim BAe ATP // //FOR FS2004. FDE COPYRIGHT ENIGMA SIMULATIONS, MAR2010 // //MARTYN BECKER 04APR10 v1.0 thebecken@hotmail.com // // // //REALISTIC DYNAMICS - ACCURATE DIMENSIONS, LOAD WEIGHTS, // //FUEL, SPEED, ENGINE POWER AND RANGE // //////////////////////////////////////////////////////////////////////// //filename: aircraft_ATP.cfg [fltsim.0] title=Enigma Simulations British Aerospace ATP United Express NOC sim=Enigma_BAe_ATP model=C panel= sound= texture=Unitednoc kb_checklists= kb_reference= atc_id_color=0xffffffffff atc_id=N853AW atc_parking_type=RAMP atc_parking_codes= ui_manufacturer=British Aerospace ui_type=ATP ui_variation=United Express NOC description=The Enigma Simulations British Aerospace BAe ATP! www.enigmasim.com [General] performance=ATP: Power-Two 1978kW (2653shp) Pratt & Whitney Canada PW126A turboprops driving six blade constant speed BAe/Hamilton Standard propellers.\n(Flaps 29 version)\nMTOW: 50,500 lbs\n\nNormal Cruise: 260kts\nCruise alt. FL190-230. Max alt. FL250\nRange with 64 passengers and reserves 1480km (800nm)\nFuel capacity 1,681 US gallons. atc_type=britishaerospace atc_model=atp Category=airplane //AERODYNAMICS [airplane_geometry] wing_area=842.840 wing_span=100.500 wing_root_chord=8.83 wing_dihedral=2.50 wing_incidence=1.50 wing_twist=0.00 oswald_efficiency_factor=0.65 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=5.0 wing_pos_apex_vert=0.0 htail_area=243.00 htail_span=40.50 htail_pos_lon=-40.000 htail_pos_vert=9.000 htail_incidence=-0.28 htail_sweep=2.000 vtail_area=148.000 vtail_span=14.000 vtail_sweep=5.000 vtail_pos_lon=-46.000 vtail_pos_vert=9.000 elevator_area=35.000 aileron_area=35.000 rudder_area=60.530 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=15.481 aileron_down_limit=8.897 rudder_limit=23.491 elevator_trim_limit=16 spoiler_limit=59.989 spoilerons_available=1 aileron_to_spoileron_gain=5.500 min_ailerons_for_spoilerons=5.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [Flaps.0] type=1 span-outboard=0.600 extending-time=17.500 system_type=0 damaging-speed=200.000 blowout-speed=220.000 lift_scalar=1.60 drag_scalar=1.20 pitch_scalar=-0.400 flaps-position.0=0.000, 0.000 flaps-position.1=7.000, 0.000 flaps-position.2=15.000, 0.000 flaps-position.3=20.000, 0.000 flaps-position.4=29.000, 0.000 [flight_tuning] cruise_lift_scalar=1.200 pitch_stability=10.000 roll_stability=1.500 yaw_stability=1.000 parasite_drag_scalar=1.00 induced_drag_scalar=1.00 elevator_effectiveness=1.3 aileron_effectiveness=1.00 rudder_effectiveness=1.00 elevator_trim_effectiveness=5.00 aileron_trim_effectiveness=1.00 rudder_trim_effectiveness=1.00 [Reference Speeds] flaps_up_stall_speed=102.000 full_flaps_stall_speed=81.600 cruise_speed=304.798 max_indicated_speed=270.00 max_mach=0.65 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 ;station_load.0=10240.000000,0.000000,0.000000,0.000000 //total pax loading ;station_load.x ="wt lbs, long, lat, vert, station name" station_load.0="360.0, 40.0, 0.0, 4.0, Flight deck" station_load.1="320.0, 35.0, 0.0, 4.0, Cabin crew" station_load.2="3015.0, 25.0, 0.0, 4.0, Economy 1" station_load.3="3015.0, 0.0, 0.0, 4.0, Economy 2" station_load.4="3015.0, -25.0, 0.0, 4.0, Economy 3" station_load.5="400.0, 25.0, 0.0, -4.0, Forward cargo" station_load.6="400.0, -20.0, 0.0, -4.0, Rear cargo" empty_weight= 31290.00 empty_weight_roll_MOI= 240400.00 empty_weight_pitch_MOI= 1581185.00 empty_weight_yaw_MOI= 406097.00 empty_weight_coupled_MOI= 0.00 max_gross_weight= 50550.00 CG_forward_limit= 0.000 CG_aft_limit= 1.000 //INSTRUMENTS/SYSTEMS [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 autothrottle_available=0 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=96 pitch_takeoff_ga=8 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1 [brakes] toe_brakes_scale=0.80 parking_brake=1 differential_braking_scale=1 [direction_indicators] direction_indicator.0=3,0 [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) //Amended to extend battery life at startup flap_motor= 0, 1 , 1 gear_motor = 0, 1 , 1 light_wing = 0, 1 , 1 light_logo = 0, 1 , 1 autopilot = 0, 5 , 1 avionics_bus = 0, 5, 1 avionics = 1, 5 , 1 pitot_heat= 0, 2 , 1 additional_system = 2, 1, 1 marker_beacon = 1, 1 , 1 gear_warning = 0, 1 , 1 fuel_pump = 0, 1 , 1 starter1 = 0, 1, 1 light_nav = 0, 1 , 1 light_beacon = 0, 1 , 1 light_landing = 0, 1 , 1 light_taxi = 0, 1 , 1 light_strobe = 0, 1 , 1 light_panel = 0, 1 , 1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 2, -2.0, -50.0, 3.4, fx_strobeh light.1 = 2, -2.0, 50.0, 3.4, fx_strobeh light.2 = 1, 3.25, 0, -2.7, fx_beaconb light.3 = 1, -42.0, 0, 17.9, fx_beacon //ENGINES [fuel] LeftMain= 0.000, -17.500, 5.000, 840.000, 3.000 RightMain= 0.000, 17.500, 5.000, 840.000, 3.000 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 11.73, -14.23, 1.85 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 11.73, 14.23, 1.85 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.625 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 13.75 //Propeller Diameter, (feet) propeller_blades = 6 //Number of propeller blades propeller_moi = 600.00 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 17 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 35000 //Miminum governed RPM prop_tc = 0.008 //Prop time-constant gear_reduction_ratio = 7.6 //Propeller gear reduction ratio fixed_pitch_beta = 45 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 500 //Minimum RPM for prop feathering beta_feather = 79.3 //Feathering pitch angle (degrees) power_absorbed_cf = 0.09 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -24.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.001 //Gain on fuel flow inlet_area = 0.5 //Square Feet, engine nacelle inlet area rated_N2_rpm = 20000 //RPM, second stage compressor rated value static_thrust = 2200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.0 //Scalar on Turboprop power maximum_torque = 10870 //Maximum torque available (ft-lbs) max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 //MISCELLANEOUS SIMULATOR [attitude_indicators] attitude_indicator.0=1 [contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) // 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15 point.0=1, 29.384, -0.000, -7.600, 1181.00, 0, 0.835, 56, 0.296, 3.570, 1.900, 4.80, 4.80, 0, 205.00, 215.00 //nose gear point.1=1, -2.872, -14.234, -7.250, 1574.00, 1, 1.331, 0, 0.617, 1.890, 0.900, 5.50, 6.80, 2, 205.00, 215.00 //gear port point.2=1, -2.872, 14.234, -7.250, 1574.00, 2, 1.331, 0, 0.617, 1.890, 0.900, 5.80, 7.00, 2, 205.00, 215.00 //gear starboard point.3=2.0, 0.0,-50.0, 2.5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 //port wingtip point.4=2.0, 0.0, 50.0, 2.5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 //starb wingtip point.5=2.0, -37.0, 0.0, -0.6, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 //tail point.6=2.0, 37.0, 0.0,-2.0, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 //nose point.7=2.0, 3.0, -15.0,-3.5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 //port engine point.8=2.0, 3.0, 15.0,-3.5, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 //starb engine max_number_of_points=10 static_pitch=0.0 static_cg_height=6.9 gear_system_type=1 //Hydraulic [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [ground_reaction] main_gear_static_compression=0.8 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=2.00 //1.0 // Main gear strut damping, 0 = undamped oscillations, 1 = critically damped center_gear_damping_ratio=1.5 // Center gear strut damping, 0 = undamped oscillations, 1 = critically damped [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [pitot_static] vertical_speed_time_constant=99 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [stall_warning] type=1 stick_shaker=1 [turn_indicators] turn_indicator.0=1,0 [Views] eyepoint=39.9, -1.31, 4.7 //VISUAL EFFECTS [effects] wake=fx_wake water=fx_spray dirt=fx_tchdr5 concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=5 exit_rate.0=0.4 ;Percent/second exit_rate.1=0.2 ;Percent/second exit_rate.2=0.4 ;Percent/second exit_rate.3=0.4 ;Percent/second exit_rate.4=0.4 ;Percent/second [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 [smokesystem] //Wing tip vortices ;smoke.0=0, -25.167, -34.567, VortexEnigmaFlap ;smoke.1=0, -25.167, 34.567, VortexEnigmaFlap [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=2
