Difference between revisions of "Adaptive"
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(Created page with "Implementation of stabilization adaptive === A === {{Box Code|conf/airframes/myplane.xml| <source lang="xml"> <section name="HORIZONTAL CONTROL" prefix="H_CTL_"> <def...") |
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Implementation of stabilization adaptive | Implementation of stabilization adaptive | ||
{{Box Code|conf/airframes/myplane.xml| | {{Box Code|conf/airframes/myplane.xml| |
Revision as of 06:03, 3 July 2015
Implementation of stabilization adaptive
File: conf/airframes/myplane.xml |
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.8"/>
<define name="COURSE_DGAIN" value="0.3"/>
<define name="ROLL_MAX_SETPOINT" value="50" unit="deg"/>
<define name="ROLL_ATTITUDE_GAIN" value="7400."/>
<define name="ROLL_RATE_GAIN" value="200."/>
<define name="ROLL_IGAIN" value="100."/>
<define name="ROLL_KFFA" value="1."/>
<define name="ROLL_KFFD" value="1."/>
<define name="PITCH_MAX_SETPOINT" value="30" unit="deg"/>
<define name="PITCH_MIN_SETPOINT" value="-30" unit="deg"/>
<define name="PITCH_PGAIN" value="8000."/>
<define name="PITCH_DGAIN" value="0."/>
<define name="PITCH_IGAIN" value="100."/>
<define name="PITCH_KFFA" value="1."/>
<define name="PITCH_KFFD" value="1."/>
<define name="PITCH_OF_ROLL" value="0.03"/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="YAW_LOOP" value="TRUE"/>
<define name="YAW_TRIM_NY" value="TRUE"/>
<define name="YAW_DGAIN" value="5000."/>
<define name="YAW_NY_IGAIN" value="5000."/>
<define name="CL_LOOP" value="TRUE"/>
<define name="CL_LOOP_USE_AIRSPEED_SETPOINT" value="TRUE"/>
<define name="CL_LOOP_INCREASE_FLAPS_WITH_LOADFACTOR" value="TRUE"/>
<define name="CL_FLAPS_STALL" value="0.5"/>
<define name="CL_FLAPS_NOMINAL" value="0."/>
<define name="CL_FLAPS_RACE" value="-0.5"/>
<define name="CL_DEADBAND" value="1."/>
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