|
| צפה בנושא הקודם :: צפה בנושא הבא |
| מחבר |
הודעה |
echo69
טיסות סדירות
הצטרף בתאריך: Apr 25, 2009
הודעות: 25
|
 נשלח: 19:19 ,27 יולי 2009, ב' כותרת הודעה: נמחק מטוס! |
 |
|
| עשיתי טעות גורלית ניסיתי להתקין צביעה וכמו מפגר מחקתי את הCFG המקורי, והצביעה לא עובדת. אז עכשיו בכלל לא רואים את המטוס. יש לי FSX והמטוס שנמחק הוא Lear 45. אני ישמח אם מישהו יעשה מצווה וישלח לי את התקייה של המטוס באימייל זה לוקח בדיוק שתי דקות תודה רבה רבה לעוזרים!! |
|
| חזור למעלה |
|
 |
|
|
|
Mike_69th
מנהל ראשי
הצטרף בתאריך: 11/04/2005
הודעות: 7521
|
|
| חזור למעלה |
|
|
Mike_69th
מנהל ראשי
הצטרף בתאריך: 11/04/2005
הודעות: 7521
|
| נשלח: 19:41 ,27 יולי 2009, ב' כותרת הודעה: |
|
|
| קוד: | [fltsim.0]
title=Learjet 45
sim=Lear45
model=
panel=
sound=
texture=
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=JA-068X
ui_manufacturer="Bombardier"
ui_type="Learjet 45"
ui_variation="Gold, Black"
ui_typerole="Twin Engine Jet"
ui_createdby="Microsoft Corporation"
description="The Model 45 is Learjet's first all-new aircraft since Bill Lear's first Model 23. Although it looks like a Learjet, it has only half the parts of a Model 35, reflecting a significant design progression. The parameters set down for the 45 called for it to have the performance of the Learjet 35, the handling of the Learjet 31A, and greater cabin space than the competition."
[fltsim.1]
title=Learjet 45 Limited Edition
sim=Lear45
model=
panel=
sound=
texture=1
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=N45LR
ui_manufacturer="Bombardier"
ui_type="Learjet 45"
ui_variation="Anniversary edition"
ui_typerole="Twin Engine Jet"
ui_createdby="Microsoft Corporation"
description="The Model 45 is Learjet's first all-new aircraft since Bill Lear's first Model 23. Although it looks like a Learjet, it has only half the parts of a Model 35, reflecting a significant design progression. The parameters set down for the 45 called for it to have the performance of the Learjet 35, the handling of the Learjet 31A, and greater cabin space than the competition."
[General]
atc_type=BOMBARDIER
atc_model=LJ45
editable=0
performance="Cruise Speed\t\nMach 0.81 464 kts 859 kmh\n\nEngines\t\nAllied Signal TFE731-20 3,500 lb thrust\n\nMaximum Range\t\n2,200 nm 2,532 sm \t 4,074 km\n\nService Ceiling\t\n51,000 ft 15,545 m\n\nFuel Capacity\t\n6,062 lb 2,722 kg\n905 U.S. gal 3,424 L \n\nMaximum Gross Weight\t\n20,450 lb 9,276 kg\n\nMaximum Takeoff Weight - HGW\t\n20,200 lb \t9,163 kg\n\nUseful Load\t\n8,750 lb \t3,969 kg\n\nLength\t\n58.4 ft\t 17.7 m\n\nWingspan\t\n47.8 ft\t 14.6 m\n\nHeight\t\n14.3 ft\t 4.3 m\n\nSeating\t\nUp to 9"
Category = airplane
[CameraDefinition.0]
Title=Tail
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 2.3, -20.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title=Right Wing
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 10.8, 1.4, -2.0
InitialPbh = 6, 0, 290
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title=Left Wing
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -10.8, 1.4, -2.0
InitialPbh = 6, 0, 70
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.001]
Title=Radio Stack
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, -0.25, -0.1
InitialPbh=14.2, 0, 0
[CameraDefinition.002]
Title=Engine Controls
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.30, 0.09, -0.18
InitialPbh=48.5, 0, 9
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -17.0, -1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -17.0, 1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, -22.5, -1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, -22.5, 1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -26.7, -1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -26.7, 1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 0, -30.9, -1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 0, -30.9, 1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 0, -35.1, -1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 0, -35.1, 1.2, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 100, -42.0, 0.0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = 50, -45.0, 0.0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Passenger 1"
station_name.3 = "Passenger 2"
station_name.4 = "Passenger 3"
station_name.5 = "Passenger 4"
station_name.6 = "Passenger 5"
station_name.7 = "Passenger 6"
station_name.8 = "Passenger 7"
station_name.9 = "Passenger 8"
station_name.10 = "Baggage1"
station_name.11 = "Baggage2"
;Moments of Inertia
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 70000
empty_weight_coupled_MOI = 0.0
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 400.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 3500 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.5 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 0 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 1.0
//0 Class
//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
[contact_points]
point.0=1, -10.00, 0.00, -4.35, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -37.25, -4.75, -4.87, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -37.25, 4.75, -4.87, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -37.83, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -37.83, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.84
static_cg_height = 4.36
gear_system_type=1 //Hydraulic
emergency_extension_type=2 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //Brake scalar
auto_brakes = 0
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -16.385, -1.3, 3.15
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -39.00, -23.6, -0.25, fx_shockwave_navred ,
light.1 = 3, -39.00, 23.6, -0.25, fx_shockwave_navgre ,
light.2 = 3, -63.93, 0.00, 9.20, fx_shockwave_navwhi_l ,
light.3 = 1, -37.00, 0.00, -2.59, fx_shockwave_beaconb_nl ,
light.4 = 2, -36.97, 0.00, -2.62, fx_shockwave_strobe_lowl ,
light.5 = 1, -63.05, 0.00, 9.75, fx_shockwave_beaconh ,
light.6 = 5, -16.00, 0.00, -24, fx_shockwave_landing_light_light,
light.7 = 4, -14.00, 0.00, 1.90, fx_shockwave_vclight,
light.8 = 5, -28.7, -1.3, -1.71, fx_Shockwave_landing_light_short // Shockwave light
light.9 = 5, -28.7, 1.3, -1.71, fx_Shockwave_landing_light_short // Shockwave light
light.10 = 5, -34.0, -4.45, -2.3, fx_Shockwave_landing_light_narrow // Shockwave light
light.11 = 5, -34.0, 4.45, -2.3, fx_Shockwave_landing_light_narrow // Shockwave light
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[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.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[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=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2
[altimeters]
altimeter.0 = 1
altimeter.1 = 1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
Center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -36.3, 10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 312.0 //Square feet
wing_span = 45.8 //Feet
wing_root_chord = 9.9 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 13.4 //Degrees, wing leading edge
wing_pos_apex_lon = -31.5 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -59.1 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 2.0 //Degrees
htail_sweep = 25.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 2.0 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 1
positive_g_limit_flaps_up = 3.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -2.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -2.0 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 464.0 //Knots True (KTAS)
max_mach = 0.81
max_indicated_speed = 330 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
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=27,14
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[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
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots |
מיכאל לוייב, צוות ניהול ראשי
69 הפטישים הוירטואלית הותיקה |
|
| חזור למעלה |
|
|
FreeFlight
טיסות סדירות
הצטרף בתאריך: Sep 24, 2008
הודעות: 2504
|
| נשלח: 20:25 ,27 יולי 2009, ב' כותרת הודעה: |
|
|
אמממממממממממממממ.... 
מישהו אולי יכול לתת לי בבקשה גם את הCFG של המוני בראבו הדיפולטי? עשיתי פעם את אותה טעות.
אתם צריכים לכתוב יותר בדייקנות בהורדות באתר אם הם מתאימים לFS9 או FSX.  |
|
| חזור למעלה |
|
|
echo69
טיסות סדירות
הצטרף בתאריך: Apr 25, 2009
הודעות: 25
|
| נשלח: 20:31 ,27 יולי 2009, ב' כותרת הודעה: |
|
|
| ווווווואייי גבר תודה רבה רבה ממש הצלת אותי |
|
| חזור למעלה |
|
|
echo69
טיסות סדירות
הצטרף בתאריך: Apr 25, 2009
הודעות: 25
|
| נשלח: 20:32 ,27 יולי 2009, ב' כותרת הודעה: |
|
|
קבל Freeflight
[fltsim.0]
title=Mooney Bravo
sim=Mooney_Bravo
model=
panel=
sound=
texture=
kb_checklists=Mooney_Bravo_Check
kb_reference=Mooney_Bravo_ref
atc_id=N123MS
ui_manufacturer="Mooney"
ui_type="Bravo"
ui_variation="White, Black"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="Mooneys are built to go fast. A focus on speed seems natural for a company that at one time offered a plane powered by a Porsche engine. Although the partnership with the Germans didn't last, Mooney's commitment to speed certainly has. In keeping with this idea, Mooney has experimented with a number of "big engine" models. The Bravo is Mooney's fastest\s with 270 hp all the way to 25,000 ft, the Bravo can attain speeds up to 220 KTAS, making it the fastest single-engine airplane currently produced."
[fltsim.1]
title=Mooney Bravo Retro
sim=Mooney_Bravo
model=
panel=
sound=
texture=1
kb_checklists=Mooney_Bravo_Check
kb_reference=Mooney_Bravo_ref
atc_id=N195KT
ui_manufacturer="Mooney"
ui_type="Bravo"
ui_variation="White, Blue"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="Mooneys are built to go fast. A focus on speed seems natural for a company that at one time offered a plane powered by a Porsche engine. Although the partnership with the Germans didn't last, Mooney's commitment to speed certainly has. In keeping with this idea, Mooney has experimented with a number of "big engine" models. The Bravo is Mooney's fastest\s with 270 hp all the way to 25,000 ft, the Bravo can attain speeds up to 220 KTAS, making it the fastest single-engine airplane currently produced."
[fltsim.2]
title=Mooney Bravo With G1000
sim=Mooney_Bravo
model=G1000
panel=G1000
sound=
texture=G1000
kb_checklists=Mooney_Bravo_Check
kb_reference=Mooney_Bravo_ref
atc_id=N1000B
ui_manufacturer="Mooney"
ui_type="Bravo G1000"
ui_variation="Glass Cockpit"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="Mooneys are built to go fast. A focus on speed seems natural for a company that at one time offered a plane powered by a Porsche engine. Although the partnership with the Germans didn't last, Mooney's commitment to speed certainly has. In keeping with this idea, Mooney has experimented with a number of "big engine" models. The Bravo is Mooney's fastest\s with 270 hp all the way to 25,000 ft, the Bravo can attain speeds up to 220 KTAS, making it the fastest single-engine airplane currently produced."
[General]
atc_type=Mooney
atc_model=M20T
editable=0
performance="Maximum Speed\t\n220 kts 253 mph\t407 kmh\n\nCruise Speed\t\n195 kts 224 mph \t361 kmh\n\nEngine\t\nTextron Lycoming TIO-540-AF1B 270 hp\n\nPropeller\t\nThree-bladed McCauley constant speed\n\nMaximum Range\t\n1,050 nm 1,204 sm \t1,945 km\n\nService Ceiling\t\n25,000 ft 7,620 m\n\nFuel Capacity\t\n89 U.S. gal 337 L \n\nEmpty Weight\t\n2,189 lb \t 993 kg\n\nMaximum Gross Weight\t\n3,368 lb \t 1,528 kg\n\nUseful Load\t\n1,179 lb \t 535 kg\n\nLength\t\n26.75 ft\t 8.15 m\n\nWingspan\t\n36 ft\t 11 m\n\nHeight\t\n8.33 ft\t 2.5 m\n\nSeating\t\nUp to 4"
Category = airplane
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 9.0, 0.3, 0.0
InitialPbh = 5, 0, 275
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -9.0, 0.3, 0.0
InitialPbh = 5, 0, 85
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = 0, 2.0, -6.5
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz=0.45, -0.02, 0.0
InitialPbh=0, 0, 0
[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz=0, -0.21, 0
InitialPbh=9, 0, 16
[WEIGHT_AND_BALANCE]
max_gross_weight = 3368 // (pounds)
empty_weight = 2189 // (pounds)
reference_datum_position = 3.9, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.7, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -3.1, -1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -3.1, 1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 100, -6.1, -1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 100, -6.1, 1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 33, -8.5, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Front Passenger"
station_name.2 = "Rear Passenger"
station_name.3 = "Rear Passenger"
station_name.4 = "Baggage"
;Moments of Inertia
empty_weight_pitch_MOI = 2706
empty_weight_roll_MOI = 2131
empty_weight_yaw_MOI = 3932
empty_weight_coupled_MOI = 0.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.1, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2575 //Max rated RPM
max_rated_hp= 270 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 38 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 18000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3 //Propeller Diameter, (feet)
propeller_blades= 4 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
[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 = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 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
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
//0 Class
//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
[contact_points]
point.0=1, 1.18, 0.0, -4.20, 1181.1, 0, 0.523, 33.66, 0.296, 2.5, 0.794, 3.5, 3.5, 0, 165.0, 165.0
point.1=1, -5.48, -4.5, -3.93, 1574.8, 1, 0.523, 0.00, 0.286, 2.5, 0.808, 4.7, 4.7, 2, 165.0, 165.0
point.2=1, -5.48, 4.5, -3.93, 1574.8, 2, 0.523, 0.00, 0.286, 2.5, 0.808, 5.2, 5.2, 3, 165.0, 165.0
point.3=2, -3.90, -18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.90 18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -20.23, 0.0, 0.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -1.48, 0.0, -2.17, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -20.23, 0.0, 6.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2, -4.90, 0.0, -1.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 2.9
static_cg_height = 3.7
gear_system_type=0 //Electric
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = -4.52, -.884, 1.4
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -2.65, -18.25, -0.18, fx_navred ,
light.1 = 3, -2.65, 18.25, -0.18, fx_navgre ,
light.2 = 7, -2.75, -18.25, -0.18, fx_recog ,
light.3 = 7, -2.75, 18.25, -0.18, fx_recog ,
light.4 = 1, -17.30, 0.00, -1.25, fx_beacon ,
light.5 = 4, -2.90, 0.00, -0.25, fx_vclight,
light.6 = 2, -5.40, -18.35, -0.13, fx_strobe ,
light.7 = 2, -5.40, 18.35, -0.13, fx_strobe ,
//light.8 = 3, -21.30, 0.00, 0.00, fx_navwhi ,
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 8 // degrees, KIAS
flaps-position.2 = 33 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[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=1,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=4.9 //PSI
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -4.1, -7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -4.1, 7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 175.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 5.1 //Feet
wing_dihedral = 5.5 //Degrees
wing_incidence = 2.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.6 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 34.0 //Square feet
htail_span = 11.8 //Feet
htail_pos_lon = -18.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 1.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 10.0 //Square feet
vtail_span = 3.6 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 90.0 //Degrees
spoiler_extension_time = 0.25 //Seconds
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 66.0 //Knots True (KTAS)
full_flaps_stall_speed = 52.8 //Knots True (KTAS)
cruise_speed = 180.0 //Knots True (KTAS)
max_indicated_speed = 195 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[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
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots |
|
| חזור למעלה |
|
|
FreeFlight
טיסות סדירות
הצטרף בתאריך: Sep 24, 2008
הודעות: 2504
|
| נשלח: 21:10 ,27 יולי 2009, ב' כותרת הודעה: |
|
|
תבורך  |
|
| חזור למעלה |
|
|
|
|
|
|
אתה לא יכול לשלוח הודעות בפורום זה
אתה לא יכול להגיב להודעות בפורום זה
אתה לא יכול לערוך את הודעותיך בפורום זה
אתה לא יכול למחוק את הודעותיך בפורום זה
אתה לא יכול להצביע למשאלים בפורום זה
|
|
חוקי הפורום
חיפוש
קבוצות משתמשים
התחבר
עמוד ראשי
-> פלייט סימולטור -> נמחק מטוס!
