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LibrePilot/ground/src/shared/uavobjectdefinition/stabilizationsettings.xml

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OP-32 GCS/Objects Initial release of ManualControl (ServoIn) and Actuator (ServoOut) related objects. Still work in progress. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@633 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-05-17 04:03:15 +02:00
<xml>
OP-128 Flight Documentation: Added description to all the UAVObject (now mandatory) and changed the parser to populate this information into the autogenerated files. Also added a function to test if an object is read only for flight. Since there are a lot of autogenerated changes the important ones are: flight/OpenPilot/UAVObjects/inc/uavobjecttemplate.h - added description and define to make the ObjectReadOnly query flight/OpenPilot/UAVObjects/uavobjecttemplate.c flight/OpenPilot/UAVObjects/uavobjectmanager.c - added the UAVObjReadOnly query ground/src/libs/uavobjgenerator/uavobjectparser.cpp - added parsing of description field git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1425 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-27 02:15:42 +02:00
<object name="StabilizationSettings" singleinstance="true" settings="true">
<description>PID settings used by the Stabilization module to combine the @ref AttitudeActual and @ref AttitudeDesired to compute @ref ActuatorDesired</description>
Flight: Got a much nicer arming/disarming system going. Made it a separate flag in the end to allow testing the stabilization code with motors not running. Also changes maxRoll/maxPitch/maxYaw to uint8 to keep object size smaller - no reason for float precision for this. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1660 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-16 17:41:11 +02:00
<field name="RollMax" units="degrees" type="uint8" elements="1" defaultvalue="35"/>
<field name="PitchMax" units="degrees" type="uint8" elements="1" defaultvalue="35"/>
<field name="YawMax" units="degrees" type="uint8" elements="1" defaultvalue="35"/>
AHRS: Yaw stabilization now supports rate stabilization or heading hold. Also need to cleanly support rate stabilization on all the other axis. Les suggested this be in manual mode which will require changing the logic somewhat (essentially for vtol it will always be running through the Stabilization module) in an aircraft dependent manner. An alternative would be a stabilization flag indicating to do full attitude hold, attitude + yaw stabilization, or all axis gyro stabilization. This would be my preference. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1659 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-16 17:41:08 +02:00
<field name="YawMode" units="degrees" type="enum" elements="1" options="rate,heading" defaultvalue="rate"/>
Flight: Got a much nicer arming/disarming system going. Made it a separate flag in the end to allow testing the stabilization code with motors not running. Also changes maxRoll/maxPitch/maxYaw to uint8 to keep object size smaller - no reason for float precision for this. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1660 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-16 17:41:11 +02:00
<field name="ThrottleMax" units="frac" type="float" elements="1" defaultvalue="1.0"/>
<field name="ThrottleMin" units="frac" type="float" elements="1" defaultvalue="-1.0"/>
Flight/Stabilization: Make the derivative account for the sampling time (dAngle/dt) for the PID loop since integral does and also make the integral bounds uavobject settings. It was originally bounded by constant/Ki but I'm not sure why as you change the gain of the error integral you also want to decrease the maximum error it can cause. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1590 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-12 04:54:41 +02:00
<field name="RollIntegralLimit" units="" type="float" elements="1" defaultvalue="0.5"/>
<field name="PitchIntegralLimit" units="" type="float" elements="1" defaultvalue="0.5"/>
<field name="YawIntegralLimit" units="" type="float" elements="1" defaultvalue="0.5"/>
OP-128 Flight Documentation: Added description to all the UAVObject (now mandatory) and changed the parser to populate this information into the autogenerated files. Also added a function to test if an object is read only for flight. Since there are a lot of autogenerated changes the important ones are: flight/OpenPilot/UAVObjects/inc/uavobjecttemplate.h - added description and define to make the ObjectReadOnly query flight/OpenPilot/UAVObjects/uavobjecttemplate.c flight/OpenPilot/UAVObjects/uavobjectmanager.c - added the UAVObjReadOnly query ground/src/libs/uavobjgenerator/uavobjectparser.cpp - added parsing of description field git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1425 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-27 02:15:42 +02:00
<field name="PitchKp" units="" type="float" elements="1" defaultvalue="0.04"/>
<field name="PitchKi" units="" type="float" elements="1" defaultvalue="0.000004"/>
<field name="PitchKd" units="" type="float" elements="1" defaultvalue="0.01"/>
<field name="RollKp" units="" type="float" elements="1" defaultvalue="0.02"/>
<field name="RollKi" units="" type="float" elements="1" defaultvalue="0.000004"/>
<field name="RollKd" units="" type="float" elements="1" defaultvalue="0.01"/>
<field name="YawKp" units="" type="float" elements="1" defaultvalue="0.04"/>
<field name="YawKi" units="" type="float" elements="1" defaultvalue="0.000004"/>
<field name="YawKd" units="" type="float" elements="1" defaultvalue="0.01"/>
<access gcs="readwrite" flight="readwrite"/>
<telemetrygcs acked="true" updatemode="onchange" period="0"/>
<telemetryflight acked="true" updatemode="onchange" period="0"/>
<logging updatemode="never" period="0"/>
OP-32 GCS/Objects Initial release of ManualControl (ServoIn) and Actuator (ServoOut) related objects. Still work in progress. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@633 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-05-17 04:03:15 +02:00
</object>
</xml>
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