2 <object name="FixedWingPathFollowerSettings" singleinstance="true" settings="true" category="Control">
3 <description>Settings for the @ref FixedWingPathFollowerModule</description>
5 <!-- these coefficients control desired movement in airspace -->
6 <field name="HorizontalVelMax" units="m/s" type="float" elements="1" defaultvalue="20"/>
7 <!-- Maximum speed the autopilot will try to achieve, usually for long distances -->
8 <field name="HorizontalVelMin" units="m/s" type="float" elements="1" defaultvalue="10"/>
9 <!-- V_y, Minimum speed the autopilot will try to fly, for example when loitering -->
10 <field name="VerticalVelMax" units="m/s" type="float" elements="1" defaultvalue="10"/>
11 <!-- maximum allowed climb or sink rate in guided flight-->
13 <field name="CourseFeedForward" units="s" type="float" elements="1" defaultvalue="3.0"/>
14 <!-- how many seconds to plan the flight vector ahead when initiating necessary heading changes - increase for planes with sluggish response -->
15 <field name="ReverseCourseOverlap" units="deg" type="float" elements="1" defaultvalue="20.0"/>
16 <!-- how big the overlapping area behind the plane is, where, if the desired course lies behind, the current bank angle will determine if the plane goes left or right -->
18 <field name="HorizontalPosP" units="(m/s)/m" type="float" elements="1" defaultvalue="0.2"/>
19 <!-- proportional coefficient for correction vector in path vector field to get back on course - reduce for fast planes to prevent course oscillations -->
20 <field name="VerticalPosP" units="(m/s)/m" type="float" elements="1" defaultvalue="0.4"/>
21 <!-- proportional coefficient for desired vertical speed in relation to altitude displacement-->
23 <!-- these coefficients control actual control outputs -->
24 <field name="CoursePI" units="deg/deg" type="float" elements="3" elementnames="Kp,Ki,ILimit" defaultvalue="0.2, 0, 0"/>
25 <!-- coefficients for desired bank angle in relation to ground bearing error - this controls heading -->
27 <field name="SpeedPI" units="deg / (m/s)" type="float" elements="3" elementnames="Kp,Ki,ILimit" defaultvalue="2.5, .25, 10"/>
28 <!-- coefficients for desired pitch
29 in relation to speed error IASerror -->
30 <field name="VerticalToPitchCrossFeed" units="deg / (m/s)" type="float" elementnames="Kp,Max" defaultvalue="5, 10"/>
31 <!-- coefficients for adjusting desired pitch
32 in relation to "vertical speed error -->
33 <field name="AirspeedToPowerCrossFeed" units="1 / (m/s)" type="float" elementnames="Kp,Max" defaultvalue="0.2, 1"/>
34 <!-- proportional coefficient for adjusting vertical speed error for power calculation
35 in relation to airspeed error IASerror -->
36 <field name="PowerPI" units="1/(m/s)" type="float" elements="3" elementnames="Kp,Ki,ILimit" defaultvalue="0.01,0.05,0.5"/>
37 <!-- proportional coefficient for desired thrust
38 in relation to vertical speed error (absolute but including crossfeed) -->
40 <!-- output limits -->
41 <field name="RollLimit" units="deg" type="float" elements="3" elementnames="Min,Neutral,Max" defaultvalue="-45,0,45" />
42 <!-- maximum allowed bank angles in navigates flight -->
43 <field name="PitchLimit" units="deg" type="float" elements="3" elementnames="Min,Neutral,Max" defaultvalue="-10,5,20" />
44 <!-- maximum allowed pitch angles and setpoint for neutral pitch -->
45 <field name="ThrustLimit" units="" type="float" elements="3" elementnames="Min,Neutral,Max" defaultvalue="0.1,0.5,0.9" />
46 <!-- minimum and maximum allowed thrust and setpoint for cruise speed -->
47 <field name="Safetymargins" units="" type="float"
48 elementnames="Wind, Stallspeed, Lowspeed, Highspeed, Overspeed, Lowpower, Highpower, Pitchcontrol"
49 defaultvalue="90, 1.0, 0.5, 1.5, 1.0, 1, 0, 1" />
50 <!-- Wind: degrees of crabbing allowed
51 Speeds: percentage (1.0=100%) of the limit to be over/onder
52 Power & Control: flag to turn on/off 0.0 =off 1.0 = on -->
53 <field name="UpdatePeriod" units="ms" type="int32" elements="1" defaultvalue="100"/>
55 <access gcs="readwrite" flight="readwrite"/>
56 <telemetrygcs acked="true" updatemode="onchange" period="0"/>
57 <telemetryflight acked="true" updatemode="onchange" period="0"/>
58 <logging updatemode="manual" period="0"/>