IL18DINFS9 Просмотр ZIP-архива

Aircraft.cfg

[FLTSIM.0]
TITLE=Ilyushin Il-18D_V1_0
SIM=Il18d_2k2
MODEL=
PANEL=
SOUND=
TEXTURE=
KB_CHECKLISTS=
KB_REFERENCE=
atc_id=53122
atc_airline=Aeroflot
atc_flight_number=76654
ui_manufacturer=Ilyushin
ui_type=Il-18D_V1_0
ui_variation=Aeroflot
EDITABLE=1
description=FS2002 PRO Ilyushin Il-18D\n\n\n
atc_heavy=0


[TURBOPROP_ENGINE]
POWER_SCALAR=1.000
maximum_torque=13100.000
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=14.76
propeller_blades=4
propeller_moi=75.000
beta_max=50.000
beta_min=8.000
min_gov_rpm=700.000
prop_tc=0.004
gear_reduction_ratio=12.100
fixed_pitch_beta=0.000
low_speed_theory_limit=180.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.000
beta_feather=93.320
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available =1
minimum_on_ground_beta=-0.0001
minimum_reverse_beta=-20.000

[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=27000		; 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]
MTW=142200
MLW=142200
empty_weight=88900.000

max_number_of_stations=50

empty_weight_cg_position=0.000, 0.000, 0.000
reference_datum_position=0.000, 0.000, 0.000
empty_weight_roll_MOI=7659435.000
empty_weight_pitch_MOI=2836600.000
empty_weight_yaw_MOI=731380.000
empty_weight_coupled_MOI=0.000
max_gross_weight=142200.000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.0=0.000000,0.000000,0.000000,0.000000

[electrical]

max_battery_voltage=24.0
generator_alternator_voltate=28.0
max_generator_alternator_amps=200.0

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, 15, 17.0
additional_system=0, 2 , 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
starter2=0, 20, 17.0
light_nav=0, 5 , 10.0
light_beacon=0, 5 , 10.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 10.0
light_panel=0, 5 , 10.0

[General]
performance=Four-Engine Long-range Turboprop Airliner\nFour-Engine Turboprop
atc_type=
atc_model=

[fuel]
LeftMain=0.000, -20.600, 0.0, 1981.5.000, 0.000
LeftAux=0.000, -30.000, 0.000, 1981.500, 0.000
RightMain=0.000, 20.600, 0.0, 1981.500, 0.000
RightAux=0.000, 30.000, 0.000, 1981.5, 0.000
fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=0

[airplane_geometry]
wing_area=1502.2
wing_span=122.73
wing_root_chord=17.166
wing_dihedral=4.500
wing_incidence=2.000
wing_twist=0.000
oswald_efficiency_factor=0.7000
wing_winglets_flag=0
wing_sweep=5.000
wing_pos_apex_lon=-0.85
wing_pos_apex_vert=4.291
htail_area=220.000
htail_span=35.19
htail_pos_lon=-60.939
htail_pos_vert=3.862
htail_incidence=0.000
htail_sweep=11.500
vtail_area=490.000
vtail_span=19.740
vtail_sweep=24.000
vtail_pos_lon=-52.356
vtail_pos_vert=22.315
elevator_area=75.000
aileron_area=58.000
rudder_area=370.000
elevator_up_limit=20.000
elevator_down_limit=20.000
aileron_up_limit=18.002
aileron_down_limit=18.002
rudder_limit=30.000
elevator_trim_limit=25.000
spoiler_limit=50.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[contact_points]

point.0=1.000, 45.489, 0.000, -8.440, 1181.102, 0.000, 0.618, 55.000, 0.212, 2.500, 1.000, 15.000, 15.000, 0.000, 216.000, 232.000
point.1=1.000, -2.29, -15.445, -9.440, 1574.803, 1.000, 0.618, 0.000, 1.0, 2.500, 0.9, 15.000, 15.000, 2.000, 216.000, 232.000
point.2=1.000, -2.29, 15.445, -9.440, 1574.803, 2.000, 0.618, 0.000, 1.0, 2.500, 0.9, 15.00, 15.00, 3.000, 216.000, 232.000
static_pitch=0.000
static_cg_height=9.44
point.3=2.000, -35.190, 0.000, -3.433, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
gear_system_type=0

[GeneralEngineData]
engine_type=5
Engine.0=12.874, -30.469, 3.862
Engine.1=18.024, -15.449, 1.716
Engine.2=12.874,  30.469, 3.862
Engine.3=18.024,  15.449, 1.716

fuel_flow_scalar=0.5700
min_throttle_limit=0.000000

[TurbineEngineData]
fuel_flow_scalar=1.000000
fuel_flow_gain=0.001
inlet_area=4.000
rated_N2_rpm=22800.000
static_thrust=2100.000
afterburner_available=0
[Reference Speeds]
flaps_up_stall_speed=100.000
full_flaps_stall_speed=83.800
cruise_speed=310.000
max_indicated_speed=330.000000
max_mach=0.650000
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=42.056,-1.716, 4.291


[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=100
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=9.000000
//For no wing leveler when AP On
use_no_default_bank=1
//For no pitch holding when AP On
use_no_default_pitch=1
//Nothing autoland, only hand
autoland_available=0
[direction_indicators]
direction_indicator.0=2,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[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

[pitot_static]
vertical_speed_time_constant=10                //Increasing this value will cause a more instantaneous reaction in the VSI
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[Flaps.0]
type=1
span-outboard=0.570
extending-time=17.000
system_type=1
damaging-speed=200.000
blowout-speed=210.000
lift_scalar=1.900
drag_scalar=3.20
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=10.000,0.000
flaps-position.3=15.000,0.000
flaps-position.4=30.000, 0.000

[brakes]
toe_brakes_scale=0.488296
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

Il18dinfs9.zip

Имя файла Дата Размер
Il18d_2k2.air 08.03.2002 23:20 15 KB
Aircraft.cfg 02.11.2003 21:42 8 KB
Flightinstructions.doc 23.05.2003 16:00 70 KB
readme.txt 03.11.2003 10:29 503 B
avsim_ru.diz 14.03.2004 00:19 419 B
Итого: 93 KB
Modified dynamics Peter Yashin under FS9, using data from Ptitsa. See the readme.
→ Size: 25 KB
→ Date: 22 years ago (07.11.2003 07:13)
→ Author: CURL
→ License: Freeware - Free version, Unlimited Distribution
→ Downloaded: 743 time(s)