Hallo,
mal ne Frage. Ich möchte das Takeoff-Verhalten bei meinen PSS A340er verbessern. Ich habe festgestellt das er trotz richtiger Trimmung nicht zu den errechneten Vr Daten abhebt, sondern zu spät. an welchen Wert(en) in der Aircraftcfg muss ich da schrauben?(probieren)
Flusifix habe ich auch schon "drüberlaufen" lassen...
Hier mal die Datei von nem A340er
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 80.0, 0.0, 4.5, PSS_VC
[exits]
number_of_exits=2
exit_rate.0 = 0.4
exit_rate.1= 0.4
[Views]
eyepoint = 84.0, -1.8, 5.5
[General]
atc_type = AIRBUS
atc_model = A343
performance =
[pitot_static]
vertical_speed_time_constant=99
[GROUND_REACTION]
MAX_STEERING_ANGLE = 72
[GeneralEngineData]
engine_type=1
Engine.0= -7 , -63, -1.5
Engine.1= 15.8, -30, -5.5
Engine.2= -7 , 63, -1.5
Engine.3= 15.8, 30, -5.5
fuel_flow_scalar = 0.8245
min_throttle_limit = -0.25
[jet_engine]
thrust_scalar = 1.13
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[direction_indicators]
direction_indicator.0=3,0
[Radios]
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
[Flaps.0]
type = 1
span-outboard = 1.0
extending-time = 20
system_type = 1
flaps-position.0 = 0
flaps-position.1 = 8
flaps-position.2 = 14
flaps-position.3 = 18
flaps-position.4 = 22
flaps-position.5 = 32
damaging-speed = 240
blowout-speed = 260
lift_scalar = 0.001
drag_scalar = 0.001
pitch_scalar= 0.001
[Flaps.1]
type = 1
span-outboard = 1.0
extending-time = 20
system_type = 1
flaps-position.0 = 0
flaps-position.1 = 2
flaps-position.2 = 8
flaps-position.3 = 14
flaps-position.4 = 25
flaps-position.5 = 32
damaging-speed = 240
blowout-speed = 260
lift_scalar = 0.7
drag_scalar = 1.0
pitch_scalar= 1.0
[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
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
max_number_of_stations=50
pss_num_class = THREE_CLASS // Load Editor Cfg Value
station_load.0 = 450, 0.0, 0.0, 0.0 //Weight Crew (lbs) LEAVE
station_load.1 = 3000, 0.0, 0.0, 0.0 //Weight Galleys (lbs) LEAVE
station_load.2 = 25544, 0.0, 0.0, 0.0 //Weight Baggage (lbs)
station_load.3 = 0, 0.0, 0.0, 0.0 //Weight Cargo (lbs)
station_load.4 = 1050, 0.0, 0.0, 0.0 //Weight First Class (lbs)
station_load.5 = 5700, 0.0, 0.0, 0.0 //Weight Business Class (lbs)
station_load.6 = 36150, 0.0, 0.0, 0.0 //Weight Economy Class (lbs)
empty_weight = 285000
empty_weight_roll_MOI = 3900000
empty_weight_pitch_MOI = 13000000
empty_weight_yaw_MOI = 11500000
empty_weight_coupled_MOI= 0.000000
empty_weight_CG_position= 0.000000,0.000000,0.000000
max_gross_weight=599400.0
***************************************************
[fuel]
Center1 = 5.0, 0.0, -4.0, 12500, 1043
LeftMain = -5.0, -20.0, 0.0, 12150, 949
RightMain = -5.0, 20.0, 0.0, 12150, 949
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1
[airplane_geometry]
wing_area = 3892
wing_span = 163
wing_root_chord = 23.85
wing_dihedral = 6.0
wing_incidence = 0.0
wing_twist = 0.0
oswald_efficiency_factor = 0.625
wing_winglets_flag = 1
wing_sweep = 30
wing_pos_apex_lon = 30
wing_pos_apex_vert = 0
htail_area = 933
htail_span = 70
htail_pos_lon = -82.0
htail_pos_vert = 0.0
htail_incidence = 0.0
htail_sweep = 0.0
vtail_area = 650.0
vtail_span = 28.0
vtail_sweep = 33.0
vtail_pos_lon = -82.0
vtail_pos_vert = 8.0
elevator_area = 95.0
aileron_area = 39.0
rudder_area = 155.0
elevator_up_limit = 30
elevator_down_limit = 18
aileron_up_limit = 25
aileron_down_limit = 25
rudder_limit = 45.0
elevator_trim_limit = 20
spoiler_limit = 35
spoilerons_available = 1
aileron_to_spoileron_gain = 0.5
min_ailerons_for_spoilerons = 10.0
min_flaps_for_spoilerons = 0.0
//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, 65.5, 0.00, -14.6, 1574.803, 0.0, 1.312, 75.0, 1.0, 1.50, 0.257, 10.0, 10.0, 0.00, 0.0, 0.0
point.1=1.0, -12.21, -18.3, -15.2, 1574.803, 1.0, 1.512, 0.0, 1.0, 1.50, 0.688, 17.0, 17.0, 2.00, 0.0, 0.0
point.2=1.0, -12.21, 18.3, -15.2, 1574.803, 2.0, 1.512, 0.0, 1.0, 1.50, 0.688, 15.0, 15.0, 3.00, 0.0, 0.0
point.3=2.0, -14.16, -47.3, 0.00, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 5.00, 0.0, 0.0
point.4=2.0, -14.16, 47.3, 0.00, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 6.00, 0.0, 0.0
point.5=2.0, -54.00, 0.0, 2.83, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 9.00, 0.0, 0.0
point.6=2.0, 42.66, 0.0, -3.75, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 4.00, 0.0, 0.0
point.7=5.0, 0.0, 0.0, 0.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0
static_pitch=0.5
static_cg_height=13.014977
gear_system_type=0
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=28.72
rated_N2_rpm=29920
static_thrust=31200.0
afterburner_available=0
reverser_available=1
max_contrail_temperature = -30
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 800
autothrottle_available = 1
autothrottle_arming_required = 0
autothrottle_takeoff_ga = 8
autothrottle_max_rpm = 105
pitch_takeoff_ga = 10
max_pitch = 10.0
max_pitch_acceleration = 1.0
max_pitch_velocity_lo_alt = 2.0
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000.0
max_pitch_velocity_hi_alt_breakpoint = 28000.0
max_bank = 25.0
max_bank_acceleration = 1.8
max_bank_velocity = 3.0
max_throttle_rate = 0.1
nav_proportional_control = 9.0
nav_integrator_control = 0.25
nav_derivative_control = 0.0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0.0
gs_proportional_control = 9.5
gs_integrator_control = 0.26
gs_derivative_control = 0.0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0.0
yaw_damper_gain = 1.0
[Reference Speeds]
flaps_up_stall_speed = 155
full_flaps_stall_speed = 115
cruise_speed = 460
max_indicated_speed = 350.0
max_mach = 0.84
[brakes]
toe_brakes_scale=0.5
parking_brake=1
[gear_warning_system]
gear_warning_available = 0
pct_throttle_limit = 0.1
flap_limit_power = 25.5
flap_limit_idle = 5.0
[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 0, 0
normal_pressure = 3000
[stall_warning]
type = 1
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1, 0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar =0.8
induced_drag_scalar =0.8
elevator_effectiveness =2.0
aileron_effectiveness =2.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness =1.6
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
