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<xml >
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<object name= "FixedWingPathFollowerSettings" singleinstance= "true" settings= "true" category= "Control" >
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<description > Settings for the @ref FixedWingPathFollowerModule</description>
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<!-- these coefficients control desired movement in airspace -->
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<field name= "HorizontalVelMax" units= "m/s" type= "float" elements= "1" defaultvalue= "20" />
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<!-- Maximum speed the autopilot will try to achieve, usually for long distances -->
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<field name= "HorizontalVelMin" units= "m/s" type= "float" elements= "1" defaultvalue= "10" />
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<!-- V_y, Minimum speed the autopilot will try to fly, for example when loitering -->
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<field name= "VerticalVelMax" units= "m/s" type= "float" elements= "1" defaultvalue= "10" />
<!-- maximum allowed climb or sink rate in guided flight -->
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<field name= "CourseFeedForward" units= "s" type= "float" elements= "1" defaultvalue= "3.0" />
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<!-- how many seconds to plan the flight vector ahead when initiating necessary heading changes - increase for planes with sluggish response -->
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<field name= "HorizontalPosP" units= "(m/s)/m" type= "float" elements= "1" defaultvalue= "0.05" />
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<!-- proportional coefficient for correction vector in path vector field to get back on course - reduce for fast planes to prevent course oscillations -->
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<field name= "VerticalPosP" units= "(m/s)/m" type= "float" elements= "1" defaultvalue= "0.2" />
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<!-- proportional coefficient for desired vertical speed in relation to altitude displacement -->
<!-- these coefficients control actual control outputs -->
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<field name= "CoursePI" units= "deg/deg" type= "float" elements= "3" elementnames= "Kp,Ki,ILimit" defaultvalue= "0.2, 0, 0" />
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<!-- coefficients for desired bank angle in relation to ground bearing error - this controls heading -->
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<field name= "SpeedPI" units= "deg / (m/s)" type= "float" elements= "3" elementnames= "Kp,Ki,ILimit" defaultvalue= "2.5, .25, 10" />
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<!-- coefficients for desired pitch
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in relation to speed error IASerror -->
<field name= "VerticalToPitchCrossFeed" units= "deg / (m/s)" type= "float" elementnames= "Kp,Max" defaultvalue= "5, 10" />
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<!-- coefficients for adjusting desired pitch
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in relation to "vertical speed error -->
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<field name= "AirspeedToPowerCrossFeed" units= "1 / (m/s)" type= "float" elementnames= "Kp,Max" defaultvalue= "0.2, 1" />
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<!-- proportional coefficient for adjusting vertical speed error for power calculation
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in relation to airspeed error IASerror -->
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<field name= "PowerPI" units= "1/(m/s)" type= "float" elements= "3" elementnames= "Kp,Ki,ILimit" defaultvalue= "0.01,0.05,0.5" />
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<!-- proportional coefficient for desired throttle
in relation to vertical speed error (absolute but including crossfeed) -->
<!-- output limits -->
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<field name= "RollLimit" units= "deg" type= "float" elements= "3" elementnames= "Min,Neutral,Max" defaultvalue= "-35,0,35" />
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<!-- maximum allowed bank angles in navigates flight -->
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<field name= "PitchLimit" units= "deg" type= "float" elements= "3" elementnames= "Min,Neutral,Max" defaultvalue= "-10,5,20" />
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<!-- maximum allowed pitch angles and setpoint for neutral pitch -->
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<field name= "ThrottleLimit" units= "" type= "float" elements= "3" elementnames= "Min,Neutral,Max" defaultvalue= "0.1,0.5,0.9" />
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<!-- minimum and maximum allowed throttle and setpoint for cruise speed -->
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<field name= "Safetymargins" units= "" type= "float"
elementnames="Wind, Stallspeed, Lowspeed, Highspeed, Overspeed, Lowpower, Highpower, Pitchcontrol"
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defaultvalue="90, 1.0, 0.5, 1.5, 1.0, 1, 1, 1" />
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<!-- Wind: degrees of crabbing allowed
Speeds: percentage (1.0=100%) of the limit to be over/onder
Power & Control: flag to turn on/off 0.0 =off 1.0 = on -->
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<field name= "UpdatePeriod" units= "ms" type= "int32" elements= "1" defaultvalue= "100" />
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<access gcs= "readwrite" flight= "readwrite" />
<telemetrygcs acked= "true" updatemode= "onchange" period= "0" />
<telemetryflight acked= "true" updatemode= "onchange" period= "0" />
<logging updatemode= "manual" period= "0" />
</object>
</xml>