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Autopilot probleme ! (Read 162 times)
Apr 5th, 2004 at 1:41pm

Woodylepic   Offline
Colonel
Quebec Canada

Posts: 330
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[img]http://www.angelfire.com/ab6/jg3/Levasseurpl8.gif[/img]

Hi have an other glue here !
have solved my propeler trouble but now i have a trouble whit my autopilot whit my new aircraft.cfg my autopilot not work good  :(

the plane go right go left and zizag like a hell finaly the aotopilot disengage and i crash i have try to change the bank aceleration ,  limit etc nothing work i have also put the autopilot on the curtiss jenny same trouble whit the jenny pls help  ??? ??? ???

here the cfg.

[airplane_geometry]
wing_area=200.0                 //Square feet
wing_span=47.89                  //Feet
wing_root_chord=8.5                  //Feet
wing_dihedral=0.0                   //Degrees
wing_incidence=2.0                   //Degrees
wing_twist=0.0                  //Degrees
oswald_efficiency_factor=0.6                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=2.3                   //Degrees, wing leading edge
wing_pos_apex_lon=-5.1                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=3.0                   //Feet, vertical distance from reference point, positive going up

htail_area=51.0                  //Square feet
htail_span=14.1                  //Feet
htail_pos_lon=-22.6                 //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=20.0                   //Degrees, horizontal tail leading edge

vtail_area=18.0                  //Square feet
vtail_span=5.8                   //Feet, tip to body
vtail_sweep=20.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-21.6                 //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=16.3                  //Square feet
aileron_area=25.6                  //Square feet
rudder_area=7.8                   //Square feet
elevator_up_limit=25.0                  //Degrees
elevator_down_limit=25.0                  //Degrees
aileron_up_limit=16.0                  //Degrees
aileron_down_limit=16.0                  //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=0.01                   //Degrees
spoilerons_available=1                     //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

[Reference Speeds]
flaps_up_stall_speed=62.5                  //Knots True (KTAS)
full_flaps_stall_speed=62.5                  //Knots True (KTAS)
cruise_speed=89.09                //Knots True (KTAS)
max_indicated_speed=200                   //Red line (KIAS)


[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.0
default_bank_mode=2     //Default to Heading Hold

« Last Edit: Apr 6th, 2004 at 4:59pm by Woodylepic »  

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