Bernhard Platzer
27. February 2003, 19:54
Hallo Markus!!
Jetzt hab ich echt ein Problem. Ich hab mir jetzt schon die aircraft.cfg von 7 versch. Flugzeugen angesehen allerdings noch nirgends den Eintrag "VIEW_FORWARD_ZOOM" gefunden.
Hier ist mal eine meiner aircraft.cfgs:
[fltsim.0]
title=Eurowings ATR 42-300
sim=ATR42-300_2k2v3.8
model=
panel=ew
sound=
texture=ew
kb_checklists=ATR_check
kb_reference=ATR 42-300_ref
atc_airline=Eurowings
atc_flight_number=452
atc_id=D-BCRO
atc_id_enable=1
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR 42-300 (EWPro)
ui_variation=Eurowings
description=FS2002 ATR42-300\nDesign: Christoph Klose\nTextures: Christoph Klose\nFDX: Alexander M. Metzger 2k2V3.8
[fltsim.1]
title=Eurolot ATR 42-300
sim=ATR42-300_2k2v3.8
model=
panel=lo
sound=
texture=lo
kb_checklists=ATR_check
kb_reference=ATR 42-300_ref
atc_airline=EuroLOT
atc_flight_number=1134
atc_id=SP-EED
atc_id_enable=1
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR 42-300 (EWPro)
ui_variation=EuroLOT
description=FS2002 ATR42-300\nDesign: Christoph Klose\nTextures: Christoph Klose\nFDX:Alexander M. Metzger 2k2V3.8
[General]
atc_type=Aerospatiale
atc_model=AT43
editable=0
performance=ATR 42-300\nWing span: 24.57 m \/ 80.6 ft\nLength: 22.67 m \/ 74.4 ft\nHeight: 7.59 m \/ 24.9 ft\nWing area: 54.5 m2 \/ 586 sqft Dry Operating Weight: 11,113 kg \/ 24,500 lb\nMax. Fuel Weight: 4,500 kg \/ 1,500 gal\nMax. Take Off Weight: 16,900 kg \/ 37,258 lb\nZero Fuel Weight FDX: 14,589 kg \/ 32,163 lb\nEngine: PW120 \nPropeller HS 14F, 4 blade\nPassengers: 35 max. 46\nMax. speed Vmo: 250 KIAS\nCruise speed: 265 KTAS at FL170
[WEIGHT_AND_BALANCE]
// You may modify below the Zero Fuel Weight of the aircraft you want to fly.
// !!WARNING!!:
// To maintain operational flight model, the following values of weight need to be checked:
// Empty operational weight: 24500 lbs
// Maximum fuel weight: 9938 lbs
// Maximum take off weight: 37258lbs
empty_weight= 24500.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -2.700, 0.000, 0.000
max_number_of_stations=50 // Payload weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=370, 20.900, 0.000, 0.000
station_load.1=185, 11.100, 0.000, 0.000
station_load.2=185, -21.900, 0.000, 0.000
station_load.3=1587, 14.600, 0.000, 0.000
station_load.4=1191, -25.000, 0.000, 0.000
station_load.5=370, 8.800, 0.000, 0.000
station_load.6=556, 6.300, 0.000, 0.000
station_load.7=185, 3.800, 0.000, 0.000
station_load.8=741, 1.300, 0.000, 0.000
station_load.9=370, -1.300, 0.000, 0.000
station_load.10=370, -3.800, 0.000, 0.000
station_load.11=185, -6.300, 0.000, 0.000
station_load.12=370, -8.800, 0.000, 0.000
station_load.13=370, -11.300, 0.000, 0.000
station_load.14=370, -13.800, 0.000, 0.000
station_load.15=370, -16.300, 0.000, 0.000
station_load.16=185, -18.800, 0.000, 0.000
//The Zero Fuel Weight of this aircraft is 14589 kg equal 32163 pounds
// Moment of Inertia
empty_weight_roll_MOI= 182898.000
empty_weight_pitch_MOI= 167235.000
empty_weight_yaw_MOI= 190976.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 37258.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[Reference Speeds]
flaps_up_stall_speed= 110.000
full_flaps_stall_speed= 83.000
cruise_speed= 265.000
[pitot_static]
vertical_speed_time_constant=2.0 // Increasing this value will cause a faster reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.040
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.500
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 5
Engine.0= 5.200, -13.400, 3.100
Engine.1= 5.200, 13.400, 3.100
fuel_flow_scalar= 0.770
[TurbineEngineData]
fuel_flow_gain= 0.005
inlet_area= 0.800
rated_N2_rpm= 30000.000
static_thrust= 400.000
afterburner_available= 0
[turboprop_engine]
power_scalar= 1.000
maximum_torque= 8992.000
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
[propeller]
thrust_scalar= 1.000
propeller_type= 0
propeller_diameter= 12.900
propeller_blades= 4
propeller_moi= 120.000
beta_max= 45.000
beta_min= 11.500
min_gov_rpm= 21150.000
prop_tc= 0.001
gear_reduction_ratio= 25.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 350.000
beta_feather= 86.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -25.000
[fuel]
// Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain= -4.130, -14.900, 5.100, 753.000, 5.000
RightMain= -4.130, 14.900, 5.100, 753.000, 5.000
fuel_type=2 // Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 586.000
wing_span= 80.600
wing_root_chord= 9.800
wing_dihedral= 1.000
wing_incidence= 3.000
wing_twist= 0.000
oswald_efficiency_factor= 0.31
wing_winglets_flag= 0
wing_sweep= 6.000
wing_pos_apex_lon= 0.800
wing_pos_apex_vert= 5.200
htail_area= 128.000
htail_span= 24.800
htail_pos_lon= -41.300
htail_pos_vert= 16.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 163.000
vtail_span= 14.500
vtail_sweep= 40.000
vtail_pos_lon= -27.400
vtail_pos_vert= 5.200
elevator_area= 51.200
aileron_area= 61.400
rudder_area= 55.200
elevator_up_limit= 30.000
elevator_down_limit= 20.000
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 90.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Flaps.0]
type= 1
span-outboard= 0.700
extending-time= 15.000
system_type= 1
damaging-speed= 170.000
blowout-speed= 190.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 45.000, 0.000
[Views]
eyepoint=20.85, -1.95, 2.90 // (feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
// type, longitudinal, lateral, vertical distance (feet) from reference datum, filename
// Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -4.10, -39.85, 5.10, fx_navred
light.1=3, -4.10, 39.85, 5.10, fx_navgre
light.2=2, -4.15, -39.90, 5.10, fx_strobe
light.3=2, -4.15, 39.90, 5.10, fx_strobe
light.4=2, -46.00, 0.18, 3.30, fx_strobe
light.5=3, -46.00, -0.18, 3.30, fx_navwhi
light.6=1, -44.80, 0.00, 18.14, fx_beaconh
light.7=1, -3.53, 0.00, -5.33, fx_beaconb
light.8=4, -7.91, 0.00, 2.64, fx_vclight
light.9=5, 1.93, 3.48, -3.70, fx_landing
light.10=5, 1.93, -3.68, -3.70, fx_landing
;light.11=3, -41.50, -6.80, 15.00, fx_navwhis // Logo Lights
;light.12=3, -41.50, 6.80, 15.00, fx_navwhis
light.13=5, 14.50, -4.70, 0.17, fx_navwhis // Wing Inspection Lights
light.14=5, 14.50, 4.73, 0.17, fx_navwhis
[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, 21.400, 0.000, -6.300, 1800.0, 0.000, 1.000, 60.000, 0.300, 1.500, 0.600, 8.000, 10.000, 0, 160, 180
point.1=1, -7.500, -6.400, -6.700, 2400.0, 1.000, 1.410, 0.000, 0.300, 1.500, 0.600, 10.000, 12.000, 2, 160, 180
point.2=1, -7.500, 6.400, -6.700, 2400.0, 2.000, 1.410, 0.000, 0.300, 1.500, 0.600, 10.500, 12.500, 3, 160, 180
point.3=2, 27.900, 0.000, -1.200, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0, 0
point.4=2, -8.800, -40.800, 5.200, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0
point.5=2, -8.800, 40.800, 5.200, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0
point.6=2, -46.500, 0.000, 3.300, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0, 0
point.7=2, -5.200, -40.800, 5.200, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0
point.8=2, -5.200, 40.800, 5.200, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0
point.9=2, -47.000, -11.900, 16.500, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0
point.10=2, -47.000, 11.900, 16.500, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0
point.11=2, 6.700, -13.400, 2.600, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0
point.12=2, 6.700, 13.400, 2.600, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0
point.13=2, -24.800, 0.000, -4.100, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0, 0
max_number_of_points=14
static_pitch= -0.790
static_cg_height= 6.400
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=500
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=0 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=100
pitch_takeoff_ga=10.0
autoland_available=1
[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
[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
[electrical]
// BusType, MaxAmpLoad, MinVoltage
// BusTypes: 0=MainBus, 1=AvionicsBus, 2=BatteryBus, 3=HotBatteryBus, 4-7=Generator/AlternatorBus(1-4)
avionics_bus=0, 0, 1
avionics=1, 0, 1
starter1=0, 0, 1
starter2=0, 0, 1
fuel_transfer_pump=0, 0, 1
flap_motor=0, 0, 1
gear_motor=0, 0, 1
autopilot=0, 0, 1
pitot_heat=0, 0, 1
additional_system=0, 0, 1
marker_beacon=1, 0, 1
fuel_pump = 0, 0, 1=0, 0, 1
gear_warning=0, 0, 1
light_nav=0, 0, 1
light_beacon=0, 0, 1
light_landing=0, 0, 1
light_taxi=0, 0, 1
light_strobe=0, 0, 1
light_panel=0, 0, 1
auto_brake=0, 0, 1
standby_vacuum=0, 0, 1
hydraulic_pump=0, 0, 1
light_recognition=0, 0, 1
light_wing=0, 0, 1
light_logo=0, 0, 1
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=40.0
[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, 200
aileron=150, 200
rudder=150, 200
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=9000 ; 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
Ich finde echt nirgendwo diesen Eintrag. Wenn ich ihn dazufügen würde, wo müsste ich den dann hinschreiben?
Gruss,
Bernhard:confused: :confused:
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