- 28 zář 2009, 16:34
#56512
Trošku jsem si pohrál s cfg Wilca. Je tam přidáno několik load stations, aby to odpovídalo modelu (osm sedadel + piloti), dál jsem upravil data u nádrží, motorů, view point VC...
Vyzkoušel jsem to, Cessna se mi zdá v letu stabilnější a klidnější.
(původní hodnoty jsem nechal za lomítkama)
[General]
atc_type=Cessna
atc_model=
editable=1
performance= \"See Docs\"
[WEIGHT_AND_BALANCE]
max_gross_weight=36400.0 // (pounds)
empty_weight=22100.0 // (pounds)
reference_datum_position=0.00, 0.00, 0.00 //centerline, waterline)
empty_weight_CG_position=1.0, 0.00, 0.0 //
max_number_of_stations=12
//station_load.0=\"170, 19.0, 0, 0.0, Pilot\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.1=\"170, 19.0, 0, 0.0, Co-Pilot\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.2=\"170, 11.5, 0, 0.0, Passenger 1\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.3=\"170, 11.5, 0, 0.0, Passenger 2\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.4=\"170, 6.5, 0, 0.0, Passenger 3 //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.5=\"170, 6.5, 0, 0.0, Passenger 4\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
//station_load.6=\"500, 0.0, 0, 0.0, Baggage\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.0=\"0.0, 19.0, -1.2, 0.0, Pilot\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.1=\"0.0, 19.0, 1.2, 0.0, Co-Pilot\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.2=\"0.0, 11.9, -1.2, 0.0, Passenger 1\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.3=\"0.0, 11.9, 1.2, 0.0, Passenger 2\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.4=\"0.0, 7.8, -1.2, 0.0, Passenger 3 //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.5=\"0.0, 7.8, 1.2, 0.0, Passenger 4\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.6=\"0.0, 4.3, -1.2, 0.0, Passenger 5\" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.7=\"0.0, 4.3, 1.2, 0.0, Passenger 6\"
station_load.8=\"0.0, -0.3, -1.2, 0.0, Passenger 7\"
station_load.9=\"0.0, -0.3, 1.2, 0.0, Passenger 8\"
station_load.10=\"0.0, -10.9, 0.0, 0.0, Baggage\"
;Moments of Inertia
empty_weight_pitch_MOI=346000
empty_weight_roll_MOI=220000
empty_weight_yaw_MOI=168000
empty_weight_coupled_MOI=0.0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 400
electric_always_available = 1
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 0 , 17.0
gear_motor = 0, 0 , 17.0
autopilot = 0, 0 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 0, 0 , 17.0
pitot_heat = 0, 0 , 17.0
additional_system = 0, 0 , 17.0
marker_beacon = 0, 0 , 17.0
gear_warning = 0, 0 , 17.0
fuel_pump = 0, 0 , 17.0
starter1 = 0, 0 , 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 0 , 17.0
light_beacon = 0, 0 , 17.0
light_landing = 0, 0 , 17.0
light_taxi = 0, 0 , 17.0
light_strobe = 0, 0 , 17.0
light_panel = 0, 0 , 17.0
light_cabin = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
standby_vacuum = 0, 0 , 17.0
hydraulic_pump = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition = 0, 0 , 17.0
light_wing = 0, 0 , 17.0
light_logo = 0, 0 , 17.0
directional_gyro = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0
[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=1.7
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=-14.4, -5.3, 3.0 //-10.4, -3.8, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-14.4, 5.3, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.8 //Scalar for fuel flow efficiency
min_throttle_limit=-0.3 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain=0.0030
inlet_area=1.67
rated_N2_rpm=29920
static_thrust=6764 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar=0.8
//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, 22.0, 0.00, -4.07, 1181.1, 0, 0.6349, 77.0, 0.3000, 2.5, 0.5000, 5.0, 5.0, 0, 260.0, 260.0
point.1=1, -6.5, -3.90, -4.84, 1574.8, 1, 0.6349, 0.0, 0.4000, 2.5, 0.6000, 5.0, 5.0, 2, 260.0, 260.0
point.2=1, -6.5, 3.90, -4.84, 1574.8, 2, 0.6349, 0.0, 0.4000, 2.5, 0.6000, 5.2, 5.2, 3, 260.0, 260.0
point.3=2, -15.8, -31.4, 0.70, 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, -15.8, 31.4, 0.70, 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, -25.6, 0.00, 3.20, 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, 29.0, 0.00, -0.08, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch=-2
static_cg_height=4.72
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=0 //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=0.5 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=1 //electric pumps enabled
engine_map=1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=19.2, -1.21, 3.44 //19.2, -.825, 3.45 //RH //Longitudinal, Lateral, Vertical (feet)
//[RYViews]
;eyepoint=19.9, -1.2, 3.45 //RY
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cockpit
light.0=3, -17.90, -32.3, 1.0, fx_navredm ,
light.1=2, -18.50, -32.5, 1.0, fx_strobe ,
light.2=3, -17.90, 32.3, 1.0, fx_navgrem ,
light.3=2, -18.50, 32.5, 1.0, fx_strobe ,
light.4=3, -41.4, 0.00, 14.0, fx_navwhi ,
light.5=1, -33.1, 0.00, 15.50, fx_beacon ,
light.6=1, 2.8, 0.00, -2.9, fx_beacon ,
[SMOKESYSTEM]
smoke.1=-13.3, -22.6, -22.6, fx_contrail_s.fx
smoke.2=-13.3, -22.60, 22.6, fx_contrail_s.fx
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=1.0 // 0.0 .. 1.0
extending-time=20 // seconds
flaps-position.0=0 // degrees
flaps-position.1=0 // degrees
flaps-position.2=0 // degrees
flaps-position.3=5 // degrees
flaps-position.4=15 // degrees
flaps-position.5=35 // degrees
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
system_type=0
[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard=1.0 // 0.0 .. 1.0
extending-time=2 // seconds
flaps-position.0=0 // degrees
flaps-position.1=3 // degrees
flaps-position.2=3 // degrees
damaging-speed=250 // KIAS
blowout-speed=300
system_type=0
[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, 1
Adf.1=1,0
Adf.2=1,0
Transponder.1=1
Marker.1=1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1= 5.5, 0.0, -0.8, 895.0, 0.0 //-1.5, 0.0, 0.0, 895.0, 0.0
LeftMain= -3.0, 6.5, -0.8, 522.0, 0.0 //-1.5, 6.5, 0.0, 522.0, 0.0
RightMain= -3.0,-6.5, -0.8, 522.0, 0.0
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=1
[airplane_geometry]
wing_area=390.0 //Square feet
wing_span=63.9 //Feet
wing_root_chord=14.2 //Feet
wing_dihedral=3.3 //Degrees
wing_incidence=0.0 //Degrees
wing_twist=-1.0 //Degrees
oswald_efficiency_factor=0.84 //Measure of lift effeciency of wing 0.816
wing_winglets_flag=0 //Are winglets available?
wing_sweep=28.0 //Degrees, wing leading edge
wing_pos_apex_lon=11 //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=60.0 //Square feet
htail_span=20.6 //Feet
htail_pos_lon=-27.00 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=11.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=5.0 //Degrees
htail_sweep=32 //Degrees, horizontal tail leading edge
vtail_area=40 //Square feet
vtail_span=7.0 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-45 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=4.0 //Feet, vertical distance from reference point, positive going up
elevator_area=19.0 //Square feet
aileron_area=12.0 //Square feet
rudder_area=17.0 //Square feet
elevator_up_limit=22 //Degrees
elevator_down_limit=21 //Degrees
aileron_up_limit=22 //Degrees
aileron_down_limit=20 //Degrees
rudder_limit=77 //Degrees
elevator_trim_limit=18 //Degrees
spoiler_limit=66 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=2 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=112.0 //Knots True (KTAS)
full_flaps_stall_speed=102.0 //Knots True (KTAS)
cruise_speed=494.0 //MAX Knots True (KTAS)
max_mach=0.922
max_indicated_speed=350 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2200.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=97.5
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8;
max_pitch=12.0
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=0.07
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=0
[airspeed_indicators] //IAS adjustmet parameters
airspeed_indicator.0 = 0.9826, 0.0 //Appropriate values for Jet AC