The dynamics for the Il-62M Просмотр ZIP-архива

Il62/Aerodynamics/il62/aircraft.cfg

[fltsim.0]
title=Il 62M 
sim=Il62m_2k2
model=
panel=
sound=
texture=
checklists=
kb_reference=
atc_id=
atc_airline=Aeroflot
ui_manufacturer=Ilyushin
ui_variation=Aeroflot
ui_type=Il 62M
description=Notes: FS2002 PRO Ilyushin Il-62M


[GENERAL]
atc_type=Ilyushin
atc_model=Il62M
editable=1
performance=Max Cruise Speed: 890 km\nNormal Cruise Speed: 0.79M
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1


[pitot_static]
vertical_speed_time_constant=10                //Increasing this value will cause a more instantaneous reaction in the VSI

[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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -1.228,   40.524,   3.684, fx_navgreh ,
light.1=3, -1.228,  -40.524,   3.684, fx_navredh ,
light.2=4,  26.40,    0.00,    5.526, fx_vclighth ,
//Nose lights
light.3=5,  25.174,   -1.23,   0.614, fx_landing ,
light.4=5,  25.174,    1.23,   0.614, fx_landing ,
//Main gear lights
//light.5=5,  -2.95,  -13.72,   -4.80, fx_landing ,
//light.6=5,  -2.95,   13.72,   -4.80, fx_landing ,


[Views]
eyepoint=90.12,-3.26,13.54

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=1, 5 , 17.0
avionics_bus=0, 12, 17.0
avionics=1, 2 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
starter2=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

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=190000.000000  //185-5000
empty_weight_roll_MOI=10300000.000000 //7 3
empty_weight_pitch_MOI=13000000.000000 //9 0
empty_weight_yaw_MOI=14000000.000000 //9 4
empty_weight_coupled_MOI=7500.000000 //7500
max_gross_weight=371100.000

[fuel]
LeftMain=0.000, 0.00000,0.0000,6287.000000,0.000000 //6287
LeftAux=0.000,-10.000000,0.000000,6287.000000,0.000000
RightMain=0.0, 0.00000,0.000,6287.000000,0.000000
RightAux=0.0000,10.000000,0.000000,6287.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=2

[airplane_geometry]
wing_area=3007.4000  //wing area m2 x 10.758
wing_span=141.7  //span m x 3.28
wing_root_chord=42.76
wing_dihedral=3.240
wing_incidence=3 
wing_twist=0
oswald_efficiency_factor=0.8
wing_winglets_flag=0
wing_sweep=35.00000
wing_pos_apex_lon=-29.20000
wing_pos_apex_vert=1.630000
htail_area=430.3000  //area m2 x 10.758
htail_span=40.100
htail_pos_lon=-79.27000
htail_pos_vert=30.5000
htail_incidence=0.000
htail_sweep=30.000000
vtail_area=383.0000
vtail_span=35.0 //29.74  
vtail_sweep=32.000000
vtail_pos_lon=-64.8000
vtail_pos_vert=29.74
elevator_area=87.7
aileron_area=87.40000
rudder_area=101.800000
elevator_up_limit=15.0
elevator_down_limit=25.0
aileron_up_limit=27.0
aileron_down_limit=15.0
rudder_limit=27.0
elevator_trim_limit=15.0
spoiler_limit=45
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,72.20,0.000000,-11.5000, 800.0,0.000000,1.44,59.0000,1.1,2.500000,0.90,15.000000,15.000000,0.000000,217.000000,220.000000
point.1=1.000000,-1.6,-12.5,-10.9,1100.0,1.000000,1.164610,0.000000,0.364720,2.500000,0.617757,15.500000,15.500000,2.000000,217.000000,220.000000
point.2=1.000000,-1.6, 12.5,-10.9,1100.0,2.000000,1.164610,0.000000,0.364720,2.500000,0.617757,15.500000,15.500000,3.000000,217.000000,220.000000
point.3=1.000000,-6.9,-12.5,-10.9,1100.0,1.000000,1.164610,0.000000,0.364720,2.500000,0.617757,15.500000,15.500000,2.000000,217.000000,220.000000
point.4=1.000000,-6.9, 12.5,-10.9,1100.0,2.000000,1.164610,0.000000,0.364720,2.500000,0.617757,15.500000,15.500000,3.000000,217.000000,220.000000
static_pitch=0.000000
static_cg_height=10.90

[Flaps.0]
type=1
span-outboard=0.610000
extending-time=21.000000
system_type=0
lift_scalar=0.70
drag_scalar=1.40
pitch_scalar=1.00
flaps-position.0=0.000000,0.000000
flaps-position.1=5.000000,0.000000
flaps-position.2=10.000000,0.000000
flaps-position.3=15.000000,0.000000
flaps-position.4=20.000000,0.000000
flaps-position.5=25.000000,0.000000
flaps-position.6=30.000000,0.000000
flaps-position.7=35.000000,0.000000

damaging-speed=217                                  // KIAS
blowout-speed=220                                  // KIAS

[SMOKESYSTEM]
smoke.0=-44.51,-16.30,4.34, fx_smoke_rx                 
smoke.1=-44.51,-9.77,4.34, fx_smoke_rx 
smoke.0=-44.51, 16.30,4.34, fx_smoke_rx                 
smoke.1=-44.51, 9.77,4.34, fx_smoke_rx 

[GeneralEngineData]
engine_type=1
Engine.0=-28.16000,-15.65, 4.35
Engine.1=-28.160000,-9.4, 4.3500
Engine.2=-28.16000,  9.4, 4.35
Engine.3=-28.1600, 15.65, 4.35

fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_scalar=1.000000
fuel_flow_gain=0.005500
inlet_area=62.0000
rated_N2_rpm=11700.000000
static_thrust=27444.000000 //24444
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=127.000000
full_flaps_stall_speed=118.0000
cruise_speed=432

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=2000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=100.000000
pitch_takeoff_ga=10.000000
//For no wing leveler when AP On
use_no_default_bank=1
//For no pitch holding when AP On
use_no_default_pitch=0
//Nothing autoland, only hand
autoland_available=0

[direction_indicators]
direction_indicator.0=3,0






il62_dynamics.zip

Имя файла Дата Размер
Il62/Aerodynamics/il62/aircraft.cfg 03.12.2002 02:11 7 KB
Il62/Aerodynamics/il62/Il62m_2k2.air 04.12.2002 22:40 8 KB
заметки по пилотированию.doc 24.12.2002 13:26 60 KB
avsim_ru.diz 14.03.2004 00:19 349 B
Итого: 76 KB
The dynamics for the IL-62M.
→ Size: 16 KB
→ Date: 23 years ago (07.02.2003 15:46)
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