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Simulationen Alles zum Thema Simulation |
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#21 |
Elite
![]() Registriert seit: 23.10.2003
Beiträge: 1.171
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![]() Hallo Nils,
habe deinen Rat befolgt (Aerosim Tristar + Omwings-Panel). Ich bin mit der kombination sehr zufrieden. Mit dem Merge scheint es aber Probleme zu geben. Wenn ich das VC aufrufe ist mein Blickpunkt weit über dem Cockpit. Ich muss mich mittels Active Camera immer nach unten bewegen. Außerdem sind im VC alle Anzeigen schwarz bzw. es werden keine Gauges dargestellt. Als letztes Manko habe ich entdeckt, dass das Hauptfahrwerk ein wenig in den Boden versinkt. Das Bugfahrwerk ist i.O. Gibt es für die Fehler einen Patch ? Vielen Dank. Philipp |
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#22 |
Elite
![]() Registriert seit: 23.10.2003
Beiträge: 1.171
|
![]() Hallo Leute,
konnte das Problem mit den schwarzen bzw. nicht vorhandenen Gauges im VC ganz einfach beheben. Jetzt bleibt nur noch das Problem mit den versunkenen Rädern und dem versetzen Blick im VC. Wäre toll, wenn da jemand eine Idee hätte. Vielen Dank. P.S.: Ist es normal, dass die Tristar so eine wahnsinns Power hat. Wenn man beim Takeoff nicht aufpasst ist man sehr schnell im Overspeed-Bereich, selbst wenn der Flieger richtig schwer ist. Philipp |
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#23 |
Veteran
![]() Registriert seit: 23.02.2001
Alter: 57
Beiträge: 293
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![]() Die Aerosim Kiste hat nicht im geringsten was mit den Flugeigeschaften eines realen TriStar zu tun.
Die -1 TriStar war masslos untermotorisiert; der TriStar -500 im ungefähren gleich einem Airbus A340 Ein komplettes AOM der -500 findet Ihr im übrigen bei AVSIM unter den Dateinamen l10115aom.zip und l10115aom2.zip
____________________________________
Always Happy Landings Holger Ludwig German Lockheed L1011 Information Center Mail : Webmaster@L-1011.de Web : http://www.L1011.de Lockheed L1011 TriStar! Alles andere ist tinnef! |
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#24 | |
Gast
Beiträge: n/a
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![]() Zitat:
auf eigene Gefahr, meine Version der Aircraft.cfg (ab General!): [General] atc_type=LOCKHEED atc_model=L101 atc_heavy=1 atc_id_enable=1 performance=Cruising Speed: 898km/h (484kts) at 35000ft\nMax. Speed: 974km/h (526kts) at 30000ft\nMax. FlightLevel: 42000ft (12802m)\nTake-off field length: 7998ft (2438m)\nLanding field length: 6775ft (2065m)\nRange: 7700km(400 Pass.) / 9047km(Empty)\nPower: 3x Rolls-Royce RB.211-524 at 50.000 lbs thrust\nWingspan: 47.35m\nLength: 54.15m\nWing Area: 321 square meters\nFuselage Diameter: 5.97m [WEIGHT_AND_BALANCE] max_gross_weight=502000.000 empty_weight=244000.000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 max_number_of_stations =50 station_load.0 = "170.0, 82.0, -1.5, 0.0, Pilot" station_load.1 = "170.0, 82.0, 1.5, 0.0, Co-Pilot" station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" station_load.3 = "5440.0, 61.5, 0.0, 0.0, First Class 1-7" station_load.4 = "7990.0, 41.0, 0.0,0.0, Economy 10-19" station_load.5 = "24310.0, -0.0, 0.0,0.0, Economy 21-36" station_load.6 = "8160.0, -42.0, 0.0,0.0, Economy 40-48" station_load.7 = "10000.0, 50.5, 0.0, 0.0, Forward Cargo" station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Cargo" ;Moments of Inertia empty_weight_pitch_MOI=24000000.000 empty_weight_roll_MOI=5500000.000 empty_weight_yaw_MOI=16300000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=0.9120 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=5.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 1 Engine.0= 1.000, -36.000, -8.500 Engine.1= -71.000, 0.000, 3.500 Engine.2= 1.000, 36.000, -8.500 fuel_flow_scalar= 1.000 min_throttle_limit=-0.199951 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=28.000 rated_N2_rpm=14000.000 static_thrust=36800.000 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.000 |
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#25 |
Gast
Beiträge: n/a
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![]() [electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=Ho tBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //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) [contact_points] point.0=1.0, 59.0, 0.0, -16.40, 1181.1, 0.0, 4.521, 70.00, 0.400, 2.500, 0.724, 4.000, 4.000, 1.000, 0.000, 0.000 point.1=1.0, -11.0, -17.0, -17.20, 1574.8, 1.0, 4.521, 0.000, 1.510, 1.100, 0.747, 6.900, 6.900, 2.000, 0.000, 0.000 point.2=1.0, -11.0, 17.0, -17.20, 1574.8, 2.0, 4.521, 0.000, 1.510, 1.100, 0.747, 7.100, 7.100, 3.000, 0.000, 0.000 point.3=2.0, -14.17, -47.33, 0.0, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.0, -14.17, 47.33, 0.0, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.0, -83.33, 0.000, 2.5, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.0, 42.670, 0.000, -3.75, 787.4, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=-0.9 static_cg_height=16.8 gear_system_type=0 [Views] eyepoint=76.5, -1.55, 8.2 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 |
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#26 |
Gast
Beiträge: n/a
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![]() [keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [LIGHTS] light.0=3, -36.20, -78.0, 2.4, fx_navredm , light.1=3, -36.20, 78.0, 2.4, fx_navgrem , light.2=2, -36.70, 0.00, 2.4, fx_strobe_L10_CL2 , light.3=1, 1.96, 0.00, -8.8, fx_as_l10_beaconb , light.4=1, 15.74, 0.00, 11.2, fx_as_l10_beaconh , light.5=3, -45.60, -77.50, 2.10, fx_navwhi , light.6=3, -45.60, 77.50, 2.10, fx_navwhi , light.7=3, -45.60, -78.20, 2.20, fx_navwhi , light.8=3, -45.60, 78.20, 2.20, fx_navwhi , light.9=4, 79.2, 0.0, 2.60, fx_vclightCL2 , [EFFECTS] startup=fx_as_l10_start water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 wake=fx_wake [exits] number_of_exits = 2 exit_rate.0 = 0.2 exit_rate.1 = 0.2 [folding_wings] wing_fold_system_type =2 fold_rates =5.0,5.0 [fuel] Center1=0.000, 0.000, -4.000, 8848.333, 3.000 LeftMain=-7.000, -35.000, 0.000, 4800.333, 3.000 RightMain=-7.000, 35.000, 0.000, 4800.333, 3.000 LeftAux =-7.000, -35.000, 0.000, 4048.0, 3.000 RightAux = -7.000, 35.000, 0.000, 4048.0, 3.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area = 3456.3 wing_span = 155.3 wing_root_chord = 23.0 wing_dihedral = 6.2 wing_incidence = 1.0 wing_twist = -0.5 oswald_efficiency_factor= 0.6 wing_winglets_flag = 0 wing_sweep = 32.0 wing_pos_apex_lon = 38.0 wing_pos_apex_vert = 0.0 htail_area = 973.49 htail_span = 71.58 htail_pos_lon = -100.0 htail_pos_vert = 0.0 htail_incidence = 0.0 htail_sweep = 40.0 vtail_area = 884.6 vtail_span = 27.3 vtail_sweep = 35.0 vtail_pos_lon = -108.3 vtail_pos_vert = 5.8 elevator_area = 97.30 aileron_area = 68.0 rudder_area = 232.0 elevator_up_limit = 30.0 elevator_down_limit = 30.0 aileron_up_limit = 30.0 aileron_down_limit = 15.0 rudder_limit = 25.0 elevator_trim_limit = 20.0 spoiler_limit = 60.0 spoilerons_available = 1 aileron_to_spoileron_gain = 3 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 |
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#27 |
Gast
Beiträge: n/a
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![]() [Reference Speeds]
flaps_up_stall_speed=150.000 full_flaps_stall_speed=120.000 cruise_speed=482.000 max_indicated_speed=355.000000 max_mach=0.860010 [autopilot] use_no_default_bank=1 use_no_default_pitch=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; autoland_available=1 default_pitch_mode=0 default_bank_mode=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 [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 [brakes] toe_brakes_scale=0.8 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.300 extending-time=10.000 system_type=1 damaging-speed=260.000 blowout-speed=300.000 lift_scalar=0.550 drag_scalar=0.550 pitch_scalar=0.550 flaps-position.0=0.000, 0.000 flaps-position.1=4.000, 0.000 flaps-position.2=10.000, 0.000 flaps-position.3=14.000, 0.000 flaps-position.4=18.000, 0.000 flaps-position.5=22.000, 0.000 flaps-position.6=27.000, 0.000 flaps-position.7=33.000, 0.000 flaps-position.8=45.000, 0.000 [Flaps.1] type=1 span-outboard=0.900 extending-time=10.000 system_type=1 damaging-speed=260.000 blowout-speed=300.000 lift_scalar=0.350 drag_scalar=0.350 pitch_scalar=0.350 flaps-position.0=0.000, 0.000 flaps-position.1=4.000, 0.000 flaps-position.2=10.000, 0.000 flaps-position.3=14.000, 0.000 flaps-position.4=18.000, 0.000 flaps-position.5=22.000, 0.000 flaps-position.6=27.000, 0.000 flaps-position.7=33.000, 0.000 flaps-position.8=45.000, 0.000 [Flaps.2] type=2 span-outboard=0.300 extending-time=4.000 system_type=1 damaging-speed=260.000 blowout-speed=300.000 lift_scalar=0.050 drag_scalar=0.050 pitch_scalar=0.050 flaps-position.0=0.000, 0.000 flaps-position.1=0.500, 0.000 flaps-position.2=0.500, 0.000 flaps-position.3=0.500, 0.000 flaps-position.4=0.500, 0.000 flaps-position.5=1.000, 0.000 flaps-position.6=1.000, 0.000 flaps-position.7=1.000, 0.000 flaps-position.8=1.000, 0.000 [Flaps.3] type=2 span-outboard=0.900 extending-time=4.000 system_type=1 damaging-speed=260.000 blowout-speed=300.000 lift_scalar=0.050 drag_scalar=0.050 pitch_scalar=0.050 flaps-position.0=0.000, 0.000 flaps-position.1=0.500, 0.000 flaps-position.2=0.500, 0.000 flaps-position.3=0.500, 0.000 flaps-position.4=0.500, 0.000 flaps-position.5=1.000, 0.000 flaps-position.6=1.000, 0.000 flaps-position.7=1.000, 0.000 flaps-position.8=1.000, 0.000 [pitot_static] navigation_hold_time_constant = 10 vertical_speed_time_constant = 100 |
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#28 | |
Veteran
![]() Registriert seit: 16.11.2001
Alter: 51
Beiträge: 409
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![]() Zitat:
Gruss Kov |
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#29 |
Elite
![]() Registriert seit: 23.10.2003
Beiträge: 1.171
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![]() Hallo Leute,
@Nils: Vielen herzlichen Dank für deine Aircraft.cfg. Werd ich gleich mal ausprobieren. @Holger: Super Tipp mit dem AOM. Vielen Dank. @Kov: Wenn die Flueigenschaften der Tristar von Vistaliners besser sind kann man diese ggf. durch die der Aerosim Tristar ersetzen. Was muss ich dazu tun ? Vielen Dank. Philipp |
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#30 |
Elite
![]() Registriert seit: 23.10.2003
Beiträge: 1.171
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![]() Hallo,
@Nils: Dank deiner Aircraft.cfg sieht jetzt alles perfekt aus. Das einzige Problem das geblieben ist, dass ich auf dem Dach sitze, wenn ich das VC öffne. Ich glaube da muss man in der Panel.cfg irgendwie den Blick ändern. Wie das geht weiss ich leider nicht. Vielen Dank. Philipp |
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