//Файл конфигурации динамического поведения модели вертолета Ми-8т(МТВ) для пилотажно навигационного тренажёра АО "ТУВААВИА" "ИРКУТСКАВИА" Антипин К.В. [email protected] 2004г//================
//======Адаптировано к данной модели 07.2010 - В. Жигульский гю Киев, Украина
[fltsim.0]
title=Mil Mi-8MT Russian Ministry of Emergency (MChS)
sim=Mi8zh
model=PZU
panel=
sound=
texture=PZU
checklists=
kb_checklists=
kb_reference=
atc_id=RF23
atc_airline=MChS
atc_flight_number=RF23
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=MChS
visual_damage=1
description=Mil Mi-8MTV transport - SAR helicopter, Russia.
atc_heavy=0
\\\================================
[fltsim.1]
title=Mil Mi-8MTV Russian Army
sim=Mi8zh
model=NURS
panel=
sound=
texture=NURS
checklists=
kb_checklists=
kb_reference=
atc_id=RA57
atc_airline=Ru Army
atc_flight_number=RA57
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Russian Army
visual_damage=1
description=Mil Mi-8MT multirole helicopter modern Russian Army.
atc_heavy=0
\\\================================
[fltsim.2]
title=Mil Mi-8MT VVS Afganistan War
sim=Mi8zh
model=EVU
panel=AFG
sound=
texture=AFG
checklists=
kb_checklists=
kb_reference=
atc_id=BS31
atc_airline=VVS
atc_flight_number=BS31
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Soviet AF (VVS) 262 Bagram squadron
visual_damage=1
description= Вечная память!.. We remember. Eternal memory... Mil Mi-8MT military transport helicopter Soviet AF (VVS) of time Afganistan War (1979-1989) - 262 Bagram helicipters squadron, USSR.
atc_heavy=0
\\\================================
[fltsim.3]
title=Mil Mi-8MT Kolavia
sim=Mi8zh
model=NORD
panel=
sound=
texture=NORD
checklists=
kb_checklists=
kb_reference=
atc_id=RA77
atc_airline=Clavia
atc_flight_number=RA77
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Kolavia
visual_damage=1
description=Mil Mi-8MT transport helicopter with External load (oil truss), Kolavia AL, oil worksite in much-much Nord of Russia .
atc_heavy=0
\\================================
[fltsim.4]
title=Mil Mi-8MT UN
sim=Mi8zh
model=UN
panel=
sound=
texture=UN
checklists=
kb_checklists=
kb_reference=
atc_id=URHL
atc_airline=UN
atc_flight_number=URHL
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=UN
visual_damage=1
description=Mil Mi-8MT transport helicopter UN (Kherson helicopters brigade, based in Kherson AB (UKOH), South Ukraine).
atc_heavy=0
\\================================
[fltsim.5]
title=Mil Mi-8MT Aeroflot
sim=Mi8zh
model=GVF
panel=
sound=
texture=GVF
checklists=
kb_checklists=
kb_reference=
atc_id=RA2585
atc_airline=Aeroflot
atc_flight_number=RA2585
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=Aeroflot
visual_damage=1
description=Mil Mi-8MT transport helicopter Aeroflot AL, Russia.
atc_heavy=0
\\================================
[fltsim.6]
title=Mil Mi-8MT Ukraine NAVI
sim=Mi8zh
model=NURS
panel=
sound=
texture=UA
checklists=
kb_checklists=
kb_reference=
atc_id=UA09
atc_airline=Ua NAVI
atc_flight_number=UA09
ui_manufacturer=Mil_ZH
prop_anim_ratio=-1.52
ui_type=Mi-8MT
ui_variation=UA NAVI
visual_damage=1
description=Mil Mi-8MT transport helicopter Ukraine NAVI.
atc_heavy=0
\\\=================================
[General]
atc_type=Mil Mi-8
performance=Mil Mi-8MT, medium multirole helicopter. Version 2010. Autur -VLadimir Zhyhulskiy, former sergeant Soviet AF, Kiev, Ukraine.
//////////////=============================
//////////////=============================
//////////////=============================
////==================================
[WEIGHT_AND_BALANCE]
max_gross_weight = 26000.000
empty_weight = 15553.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 7.709, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =170.000000, 21.489000, -2.132000, -2.132000, Pilot
station_load.1 =170.000000, 21.489000, 2.135000, -2.132000, Co-Pilot
station_load.2 =170.000000, 20.177000, 0.000000, -2.130000, Engineer
station_load.3 =170.000000, 14.271000, -1.640000, -2.788000, Pass FrontLeft1
station_load.4 =170.000000, 14.271000, -3.280000, -2.788000, Pass FrontLeft2
station_load.5 =170.000000, 11.318000, -1.640000, -2.952000, Pass FRontLeft3
station_load.6 =170.000000, 11.318000, -3.280000, -2.952000, Pass FrontLeft4
station_load.7 =170.000000, 8.202000, -1.640000, -3.280000, Pass MiddleLeft
station_load.8 =170.000000, 8.202000, -3.280000, -3.280000, Pass MiddleLeft
station_load.9 =170.000000, 5.249000, -1.640000, -3.444000, Pass BackLeft1
station_load.10 =170.000000, 5.249000, -3.280000, -3.444000, Pass BackLeft2
station_load.11 =170.000000, 2.600000, -1.640000, -3.608000, Pass BackLeft3
station_load.12 =170.000000, 2.600000, -3.280000, -3.608000, Pass BackLeft4
station_load.13 =170.000000, 14.271000, 1.640000, -2.788000, Pass FrontRight
station_load.14 =170.000000, 14.271000, 3.280000, -2.788000, Pass FrontRight
station_load.15 =170.000000, 11.318000, 1.640000, -2.952000, Pass FRontRight
station_load.16 =170.000000, 11.318000, 3.280000, -2.952000, Pass FrontRight
station_load.17 =170.000000, 8.202000, 1.640000, -3.280000, Pass MiddleRigh
station_load.18 =170.000000, 8.202000, 3.280000, -3.280000, Pass MiddleRigh
station_load.19 =170.000000, 5.249000, 1.640000, -3.444000, Pass BackRight1
station_load.20 =170.000000, 5.249000, 3.280000, -3.444000, Pass BackRight2
station_load.21 =170.000000, 2.600000, 1.640000, -3.608000, Pass BackRight3
station_load.22 =170.000000, 2.600000, 3.280000, -3.608000, Pass BackRight4
;Moments of Inertia
empty_weight_roll_MOI= 50000.000
empty_weight_pitch_MOI= 50000.000
empty_weight_yaw_MOI= 106000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
//=================================================
[flight_tuning]
rudder_effectiveness=0.05
aileron_effectiveness= 1.0
elevator_effectiveness=1.3
//=================================================
[fuel]
fuel_type = 2
number_of_tank_selectors = 1
Center1 = -3.0, 0, -4, 740, 20
LeftAux = -3.0, -3, -4, 240, 20
RightAux= -3.0, 3, -4, 240, 20
electric_pump=0
//=================================================
[GeneralEngineData]
engine_type = 1
Engine.0 = 11.975, -0.984, 2.624
Engine.1 = 11.975, 0.984, 2.624
Engine.2 = 5.000, 0.000, 3.000
fuel_flow_scalar = 5.100
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -60.0
master_ignition_switch = 1
//=================================================
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 4.772
rated_N2_rpm= 15000.000
static_thrust= 2225.000
afterburner_available= 0
reverser_available= 0.000
//=================================================
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 4, 4 , 15.0
avionics = 0, 5 , 15.0
pitot_heat = 4, 2 , 15.0
additional_system = 0, 2 , 15.0
marker_beacon = 4, 2 , 10.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 24.0
starter2 = 0, 20, 24.0
starter3 = 0, 20, 24.0
light_nav = 0, 5 , 10.0
light_beacon = 4, 5 , 15.0
light_landing = 4, 5 , 15.0
light_taxi = 0, 5 , 15.0
light_strobe = 0, 5 , 10.0
light_panel = 0, 5 , 10.0
light_cabin = 4, 5 , 10.0
light_logo = 4, 5 , 10.0
light_recognition = 4, 5 , 10.0
hydraulic_pump = 0, 5 , 15.0
fuel_transfer_pump = 0, 5 , 15.0
max_battery_voltage = 38.0
generator_alternator_voltage = 208.0
max_generator_alternator_amps = 150.0
////================================================
////================================================
////================================================
[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)
static_pitch =3.3
static_cg_height = 6.3
max_number_of_points = 8
//--------0-----1------2-------3-----4---5---6-----7----8------9---10----11-12-13-14--15
point.0 = 1, 17.22, 0.00, -7.70, 2500, 0, 0.55, 45, 0.52, 1.25, 0.5, 0, 0, 2, 00, 300 ; nose wheel left
point.1 = 1, -4.75, -8.90, -6.90, 2500, 1, 0.70, 0, 0.80, 1.25, 0.5, 0, 0, 3, 00, 300 ; aft wheel left
point.2 = 1, -4.75, 8.90, -6.90, 2500, 2, 0.70, 0, 0.80, 1.25, 0.5, 0, 0, 3, 00, 300 ; aft wheel right
point.3 = 2, 6.60, 0.00, -2.47, 2500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 5, 0, 0 ; scrape fuse front
point.4= 2, -8.50, 0.00, -2.28, 2500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 6, 0, 0 ; scrape fuse aft
point.5 = 2, -31.40, 0.00, 4.43, 2500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 9, 0, 0 ; scrape boom
point.6 = 5, 0.00, 0.00, 0.00, 0, 0, 0.00, 0., 0.0, 0.0, 0.0, 1, 1, 0, 0, 0 ; Water rudder
gear_system_type=0
////================================================
////================================================
////================================================
////================================================
////================================================
[Views]
eyepoint=1.61, -2.1, 2.2
////================================================
////================================================
////================================================
////==================EFFECT&ANIMATIONS================
////================================================
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.3
[folding_wings]
wing_fold_system_type = 1
fold_rates = 0.4, 0.4
[exits]
number_of_exits=2
exit_rate.0=0.3
exit_rate.1=0.7
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete =ZH_zero
touchdown=ZH_zero
[SMOKESYSTEM]
smoke.0=0.00, -15.30, 0.00, ZH_ikpp.fx /// 1 click-5 second!
smoke.1=-0.00,7.00,10.00, ZH_nurs /// 1 click-1 missile!
smoke.2=0.00,7.00,-10.00, ZH_nurs /// 1 click-1 missile!
smoke.3=0.00, 20.00, 0.0, ZH_PKT /// 1 click-5 second!
[anemometers]
anemometer.0 = -10.0, 0.0, 2.7 //Position from Datum
////================================================
////================================================
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.4 //Brake scalar
//=================================================
[hydraulic_system]
normal_pressure=797.700
engine_map=1,0,0,0
electric_pumps=1
//=================================================
[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
//=================================================
[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.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
rudder = 200, 1000
//=================================================
[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=2,0
//=================================================
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
//=================================================
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
//=================================================
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -21.20, 0.00, 5.30, fx_beacon ; Beacon top
light.1 = 4, 5.00, 0.00, 1.30, fx_vclight ; Pilots
light.2 = 4, 4.00, -1.00, 1.7, fx_vclight ; Pilots
light.3 = 4, 4.00, 1.00, 1.7, fx_vclight ; Pilots
Light.4= 10, -10.00, 0.00, 2.50, ZH_M8cabin
//=================================================
[Reference Speeds]
cruise_speed = 85.0 //Knots True (KTAS)
max_indicated_speed = 115.0 //Red line (KIAS)
//=================================================
[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=1.500000
roll_damp_cf=1.000000
yaw_damp_cf=0.600000
yaw_stability_cf=2.500000
//=================================================
//=================================================
[helicopter]
right_trim_scalar=-5.0
cyclic_roll_control_scalar =1.0
cyclic_pitch_control_scalar =1.0
low_realism_stability_scale = 1.35, 1.3, 5.0 //Pitch , Bank, Yaw
//=================================================
//=================================================
[MainRotor]
Position = 7.873, 0, 6.561
Radius = 34.931
max_disc_angle = 4.0
Number_of_blades = 5
weight_per_blade = 264.0
Weight_to_moi_factor = 42.0
inflow_wel_reference =43.0
inflow_vel_reference=0.000000
//=================================================
[SecondaryRotor]
TailRotor = 1
Position = -34.776, 2.378, 4.101
Radius = 6.397
//=================================================
[autopilot]
autopilot_available= 1
flight_director_available= 0
attitude_indicator= 0
direction_indicator=0
default_pitch_mode=1
max_pitch=20.0
max_pitch_acceleration=5.0
default_vertical_speed=0.01
default_bank_mode=2
max_bank=30
max_bank_acceleration=1.5
autothrottle_available=0
pitch_takeoff_ga= 8.000
max_pitch_velocity_lo_alt= 5.000
max_pitch_velocity_hi_alt= 5.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank_velocity= 5.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 5.000
//=================================================
[yaw_string]
yaw_string_available=1
[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
//=================================================
ФГУП "ТУВА АВИА" 3-Я АЭ г.Кызыл РОССИЯ 2004г.
Антипин К.В
//=================================================
Адаптировано к данной модели 07.2010-
В. Жигульский гю Киев, Украина