Динамика для пакета "Семейство Антонов V3" (Ан-24, Ан-26, Ан-30) V5.25 Просмотр ZIP-архива

An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/Aircraft.cfg

// Title:	An-30 dynamics
// Author:	Aless (thanks for the help to Curl, ALZP, UNKL, Agat, Vinni-Puh, Ranger ...) 
// Version: v5.25 (for new Samdim 2012 visual model)
// Date: june 2012
//full fuel, full equip., pass empty, Baggage 3 = 400kg (100%)
//TOW 21590 kg, MAC=24.4% (with fuel)

[fltsim.0]
title=Samdim Design Antonov An-30 Novosibirsk State Enterprise RA-30052
sim=Antonov An-30
model=30
panel=30
sound=
texture=30_N-skAvia RA-30052
kb_reference=An-24RV_flight_instructions
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=Novosibirsk Avia RA-30052
description=The Russian Turboprop\nAn-30 is a twin-engined turboprop designed for aerial cartography and produced in the USSR from 1971. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, rw3det@yandex.ru) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - samdimdesign@gmail.com

[fltsim.1]
title=Samdim Design Antonov An-30 Russia - Air Force BLACK 04 
sim=Antonov An-30
model=30
panel=30
sound=
texture=30_VVS 04 BLACK
kb_reference=An-24RV_flight_instructions
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=VVS BLACK 04 
description=The Russian Turboprop\nAn-30 is a twin-engined turboprop designed for aerial cartography and produced in the USSR from 1971. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, rw3det@yandex.ru) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - samdimdesign@gmail.com

[fltsim.2]
title=Samdim Design Antonov An-30 Russia - Air Force YELLOW 33
sim=Antonov An-30
model=30
panel=30
sound=
texture=30_VVS 33
kb_reference=An-24RV_flight_instructions
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-30
ui_variation=VVS YELLOW 33 
description=The Russian Turboprop\nAn-30 is a twin-engined turboprop designed for aerial cartography and produced in the USSR from 1971. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, rw3det@yandex.ru) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - samdimdesign@gmail.com

[fltsim.3]
title=Samdim Design Antonov An-30D Novosibirsk State Enterprise RA-30063
sim=Antonov An-30
model=30D
panel=30
sound=
texture=30D_NskAvia RA-30063
kb_reference=An-24RV_flight_instructions
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-30D
ui_variation=Novosibirsk Avia RA-30063
description=The Russian Turboprop\nAn-30 is a twin-engined turboprop designed for aerial cartography and produced in the USSR from 1971. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, rw3det@yandex.ru) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - samdimdesign@gmail.com

[fltsim.4]
title=Samdim Design Antonov An-30D Lukiaviatrans RA-30053
sim=Antonov An-30
model=30D
panel=30
sound=
texture=30D_Lukiaviatrans RA-30053
kb_reference=An-24RV_flight_instructions
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-30D
ui_variation=Lukiaviatrans RA-30053
description=The Russian Turboprop\nAn-30 is a twin-engined turboprop designed for aerial cartography and produced in the USSR from 1971. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, rw3det@yandex.ru) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - samdimdesign@gmail.com

// --- do not modify after this line ---

[General]
atc_type=Antonov 
atc_model=AN30
editable=0 
performance="Cruise Speed\n234 kts            430 km\/hr\n\nEngine\n2 x Ivchenko AI-20VT 2820 hp each\n\nPropeller\n4-Bladed Constant Speed (diam. 3.9 m)\n\nMaximum Range\n1,420 nm            1,634 mi          2,630 km\n\nService Ceiling\n20,000 ft\t         6000 m\n\nEmpty Weight\n34370 lb\t          15590 kg\n\nMaximum Gross Weight\n50,706 lb\t   23,000 kg\n\nLength\n79 ft, 7 in          24.26 m\n\nWingspan\n 95 ft, 9.5 in\t           29.2 m\n\nHeight\n27 ft, 3.5 in\t           8.32 m\n\nCrew           7"

[Propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.795 
propeller_blades=4 
propeller_moi=300 
beta_max=49.99 
beta_min=8.0 
min_gov_rpm=13900.00 
prop_tc=0.006 
gear_reduction_ratio=12.1285 
fixed_pitch_beta=15 
low_speed_theory_limit=60.0 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=500.000 //1245
beta_feather=93.320 
power_absorbed_cf=1.000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=8.0 
minimum_reverse_beta=0.0 
rotation=-1 -1

[Turboprop_engine]
power_scalar=1.05
maximum_torque=11349.83  //10614.3602 lbs*ft
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.00 
idle_rpm_friction_scalar=1.0 

[TurbineEngineData]
fuel_flow_gain=0.0045 //0.003
inlet_area=1.000 
rated_N2_rpm=15100 
static_thrust=470 
afterburner_available=0 

[flight_tuning]
cruise_lift_scalar=1.0 
pitch_stability=1.0 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.00 
aileron_effectiveness=1.00 
rudder_effectiveness=1.0 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 
hi_alpha_on_roll=1 //multiplier on the effects on roll at high angles of attack
hi_alpha_on_yaw=1 //multiplier on the effects on yaw at high angles of attack
p_factor_on_yaw=1 //multipliers on the effects induced by rotating propellers 
torque_on_roll=1
prop_effect_on_pitch=1
prop_effect_on_yaw=1
gyro_precession_on_yaw=1
gyro_precession_on_pitch=1 
gyro_precession_on_roll=1

[weight_and_balance]

// ACM V2.5
max_gross_weight = 50706.32  //23000 kg, TOW 46297.08 lbs (21000 kg) without RU-19
empty_weight = 34370.07 //   15590 kg
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.485, 0, 0
empty_weight_pitch_MOI = 400000
empty_weight_roll_MOI = 250000
empty_weight_yaw_MOI = 500000
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.88
CG_aft_limit = -0.7
max_number_of_stations = 1

station_load.0 = 2289,-6.4194,0,0,Weight

[Lights]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -3, -47.8, 3.24, fx_navredm
light.1 = 3, -3, 47.8, 3.24, fx_navgrem
light.2 = 2, -34.59, 0, 8.89, fx_beaconh_an24
light.3 = 2, 13.40, 0, -4.4, fx_beacon_an24
light.4 = 3, -46.1, 0, 3.95, fx_navwhi
light.5 = 4, 23, 2, 2, fx_vclight
light.6 = 4, 23, -2, 2, fx_vclight
light.7 = 5, 14.21,  26.42, -5.3, fx_land_an24_light,
light.8 = 5, 14.21, -26.42, -5.3, fx_land_an24_light,
light.9 = 5, 0.95,  -26.37, 3.38, fx_land_an24,
light.10 = 5, 0.95,  26.37, 3.38, fx_land_an24,
//INS
light.11 = 6, 11.21, 17.1, 0.3, fx_taxi_an24,
light.12 = 6, 11.21, -17.1, 0.3, fx_taxi_an24,
light.13 = 6, 0.95,  -26.37, 3.38, fx_land_an24,
light.14 = 6, 0.95,  26.37, 3.38, fx_land_an24,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.01 //0.88
min_throttle_limit = 0.0
engine.0 = 12.00, -12.956, 3.0
engine.1 = 12.00, 12.956, 3.0

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 0

LeftMain = 0.485, -10, 4.3, 435.9, 0
LeftAux = 0.485, -17.4, 4.3, 499.3, 0
RightMain = 0.485, 10, 4.3, 435.9, 0
RightAux = 0.485, 17.4, 4.3, 499.3, 0


[contact_points]
static_pitch = -0.5
static_cg_height = 7.1
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 16

point.0 = 1, 22, 0, -7.2, 800, 0, 1.147, 35, 0.26, 2.5, 0.5, 4.0, 4, 0, 0, 0
point.1 = 1, -2.156, -13.1, -7.90, 1400, 1, 1.45, 0, 0.79, 2.5, 0.59, 4.0, 4.3, 2, 0, 0
point.2 = 1, -2.156, 13.1, -7.90, 1400, 2, 1.45, 0, 0.79, 2.5, 0.59, 4.0, 4.3, 2, 0, 0
point.3 = 2, 28.029, 0, -3.953, 9000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.4 = 2.00, -2.26,     0.00, -5.24, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 4, 0, 0
point.5 = 2, -36.506, 0, -0.4302, 6000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2.00, -5.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.7 = 2.00, -5.22,    47.50,  3.43, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.8 = 2.00, -1.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.9 = 2.00, -1.22,    47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.10 = 2.00,  2.70,   -12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.11 = 2.00,  2.70,    12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.12 = 2, -38.523, 0, 19.9995, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.13 = 2, -33.0837, 0, 8.9997, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.14 = 2.00,  4.45,     0.00,  5.50, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 7, 0, 0
point.15 = 2, 24.1051, 0, 3.5603, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0


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


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 807.1
wing_span = 95.80
wing_root_chord = 9.19
wing_dihedral = 0
wing_incidence = 0.0
wing_twist = 0.00
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2.3
wing_pos_apex_vert = 4.3
htail_area = 213.4
htail_span = 32.70
htail_pos_lon = -36.50
htail_pos_vert = 4.3
htail_incidence = -3.00
htail_sweep = 17
vtail_area = 192.4
vtail_span = 16.05
vtail_sweep = 25
vtail_pos_lon = -34
vtail_pos_vert = 4.3
elevator_area = 55.54
aileron_area = 65.87
rudder_area = 53.819
elevator_up_limit = 30.0
elevator_down_limit = 15.0
aileron_up_limit = 24.0
aileron_down_limit = 16.0
rudder_limit = 25.000
elevator_trim_limit = 80  //45
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 27
generator_alternator_voltage = 28
max_generator_alternator_amps = 600
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 15, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 10
light_beacon = 0, 5, 10
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 10
light_panel = 0, 5, 10

[Flaps.0]
type=1
span-outboard=0.600
extending-time=16.000
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=1.0 
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0= 0.000,  0.0
flaps-position.1= 5.000,  0.0
flaps-position.2=10.000,  0.0
flaps-position.3=15.000,  0.0
flaps-position.4=20.000,  0.0
flaps-position.5=25.000,  0.0
flaps-position.6=30.000,  0.0
flaps-position.7=38.000,  0.0

[Flaps.1]
type=1
span-outboard=0.600
extending-time=6.300
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=0.2 
drag_scalar=0.1
pitch_scalar=0.05
flaps-position.0= 0.000, 0.0
flaps-position.1= 5.000, 0.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0.0

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=0.075,0.075

[exits]
number_of_exits = 3
exit_rate.0 = 0.09                             ;Percent per second
exit_rate.1 = 0.2                              ;Percent per second
exit_rate.2 = 0.2

[Reference Speeds]
flaps_up_stall_speed=102.000 
full_flaps_stall_speed=82.800 
cruise_speed=215.000 
max_indicated_speed=292.000000
max_mach=0.650000

[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, 1 
Adf.1=1 
Adf.2=1
Transponder.1=1 
Marker.1=1 

[autopilot]
autopilot_available=0 
flight_director_available=0 
default_vertical_speed=1000.000000 
autothrottle_available=0 
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000 
use_no_default_bank=0	//For no wing leveler when AP On
use_no_default_pitch=0	//For no pitch holding when AP On
autoland_available=0

[brakes]
toe_brakes_scale=0.518815
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=55.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[pitot_static]
vertical_speed_time_constant = 1.0   //0.7

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Views]
eyepoint=22.2, -1.70, 2.1 

[direction_indicators]
direction_indicator.0=3,0 

[main]
Pilot=1,80
CoPilot=1,80
Navigator=1,80
RadioOperator=1,80
FrontBaggage=1,250
FrontBaggageA=1,250
Dress=1,50
BackBaggage=1,50
Stewardess=1,80
Food=1,40
Rows.4=1,75,1,75
Rows.5=1,75,1,75
Rows.6=1,75,1,75
Rows.7=1,75,1,75
Rows.8=1,75,1,75
Rows.9=1,75,1,75
Rows.10=1,75,1,75
Rows.11=1,75,1,75
Rows.12=1,75,1,75
Rows.13=1,75,1,75
Rows.14=1,75,1,75
Rows.15=1,75,0,75
Rows.16=0,75,0,75
Rows.17=1,75,1,75
Rows.18=1,75,1,75
Rows.19=1,75,1,75
Rows.20=1,75,1,75
Rows.21=1,75,1,75
Rows.22=1,75,1,75
Rows.23=1,75,1,75
Rows.24=1,75,1,75
Rows.25=1,75,1,75
Rows.26=1,75,1,75
Rows.27=1,75,1,75
Rows.28=0,75,1,75
Rows.29=0,75,0,75

45220-Dynamics-v.5.25-Antonov-fam.v3.zip

Имя файла Дата Размер
readme.txt 16.06.2012 22:04 2 KB
An-24_dyn_v5.25_newviz/Aircraft/ 13.06.2012 02:53
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/ 13.06.2012 02:54
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/Aircraft.cfg 13.06.2012 03:23 22 KB
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/Antonov An-24RV.air 13.06.2012 01:56 14 KB
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/panel.B/ 13.06.2012 02:54
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/panel.B/Panel.cfg 11.05.2012 04:13 19 KB
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/panel.RV/ 13.06.2012 02:54
An-24_dyn_v5.25_newviz/Aircraft/SamdimDesign An24 v3/panel.RV/Panel.cfg 11.05.2012 03:59 22 KB
An-26_dyn_v5.25_newviz/Aircraft/ 13.06.2012 02:55
An-26_dyn_v5.25_newviz/Aircraft/SamdimDesign An26 v3/ 13.06.2012 02:56
An-26_dyn_v5.25_newviz/Aircraft/SamdimDesign An26 v3/Aircraft.cfg 16.06.2012 22:01 21 KB
An-26_dyn_v5.25_newviz/Aircraft/SamdimDesign An26 v3/Antonov An-26.air 13.06.2012 02:43 14 KB
An-26_dyn_v5.25_newviz/Aircraft/SamdimDesign An26 v3/panel.26/ 13.06.2012 02:56
An-26_dyn_v5.25_newviz/Aircraft/SamdimDesign An26 v3/panel.26/Panel.cfg 11.05.2012 03:58 22 KB
An-30_dyn_v5.25_newviz/Aircraft/ 13.06.2012 02:57
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/ 16.06.2012 21:06
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/Aircraft.cfg 13.06.2012 03:22 16 KB
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/Antonov An-30.air 13.06.2012 02:43 14 KB
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/Flight_Instruction_An-30_RU.pdf 05.04.2010 19:41 29 MB
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/panel.30/ 13.06.2012 02:57
An-30_dyn_v5.25_newviz/Aircraft/SamdimDesign An30 v3/panel.30/Panel.cfg 11.05.2012 03:57 23 KB
Gauges/An26_XML.cab 10.05.2012 14:43 263 KB
licence_agreement.txt 16.06.2012 20:38 2 KB
avsim_su.diz 17.06.2012 10:37 406 B
Итого: 29 MB
Откорректированная динамика (версия 5.25) для пакета "Семейство Антонов V3".
Исправления коснулись управления по тангажу. Также исправлена вместимость топливных баков для Ан-26 и Ан-30 (тоже что и для Ан-26 на данный момент). Заменен топливный индикатор (на тот что и должен быть). "Клевок" отдален в сторону бОльших скоростей. Теперь, чтобы его осуществить надо очень постараться нарушить правила использования самолета.
Замечание: триммер имеет бОльшие пределы, чем крайние положения индикатора триммера.
→ Размер: 28 MB
→ Дата: 9 лет назад (17.06.2012 00:50)
→ Автор: Александр Терентьев AKA Aless, Михаил Карнизов АКА mikedet
→ Прислал: Aless (прислал 4 файла )
→ Разрешил модератор: SLAVJAN
→ Лицензия: Лицензия поставляется в архиве
→ Скачан: 2271 раз