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Update PX4 Firmware metadata Mon Dec 28 20:04:12 UTC 2020

QGC4.4
PX4BuildBot 4 years ago
parent
commit
cab35863a8
  1. 39
      src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml

39
src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml

@ -8209,7 +8209,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8209,7 +8209,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of accelerometer 0 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8254,7 +8254,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8254,7 +8254,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_ACC0_XOFF" default="0.0" type="FLOAT" category="System">
@ -8294,7 +8293,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8294,7 +8293,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of accelerometer 1 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8339,7 +8338,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8339,7 +8338,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_ACC1_XOFF" default="0.0" type="FLOAT" category="System">
@ -8379,7 +8377,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8379,7 +8377,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of accelerometer 2 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8424,7 +8422,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8424,7 +8422,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_ACC2_XOFF" default="0.0" type="FLOAT" category="System">
@ -8464,7 +8461,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8464,7 +8461,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of accelerometer 3 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8509,7 +8506,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8509,7 +8506,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_ACC3_XOFF" default="0.0" type="FLOAT" category="System">
@ -8549,7 +8545,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8549,7 +8545,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of gyro 0 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8594,7 +8590,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8594,7 +8590,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_GYRO0_XOFF" default="0.0" type="FLOAT" category="System">
@ -8625,7 +8620,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8625,7 +8620,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of gyro 1 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8670,7 +8665,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8670,7 +8665,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_GYRO1_XOFF" default="0.0" type="FLOAT" category="System">
@ -8701,7 +8695,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8701,7 +8695,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of gyro 2 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8746,7 +8740,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8746,7 +8740,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_GYRO2_XOFF" default="0.0" type="FLOAT" category="System">
@ -8777,7 +8770,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8777,7 +8770,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of gyro 3 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8822,7 +8815,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8822,7 +8815,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_GYRO3_XOFF" default="0.0" type="FLOAT" category="System">
@ -8853,7 +8845,7 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8853,7 +8845,7 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<short_desc>Rotation of magnetometer 0 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -8898,7 +8890,6 @@ Particularly useful for testing different low-battery behaviour</short_desc> @@ -8898,7 +8890,6 @@ Particularly useful for testing different low-battery behaviour</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_MAG0_XCOMP" default="0.0" type="FLOAT" category="System">
@ -8968,7 +8959,7 @@ for current-based compensation [G/kA]</short_desc> @@ -8968,7 +8959,7 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 1 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -9013,7 +9004,6 @@ for current-based compensation [G/kA]</short_desc> @@ -9013,7 +9004,6 @@ for current-based compensation [G/kA]</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_MAG1_XCOMP" default="0.0" type="FLOAT" category="System">
@ -9083,7 +9073,7 @@ for current-based compensation [G/kA]</short_desc> @@ -9083,7 +9073,7 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 2 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -9128,7 +9118,6 @@ for current-based compensation [G/kA]</short_desc> @@ -9128,7 +9118,6 @@ for current-based compensation [G/kA]</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_MAG2_XCOMP" default="0.0" type="FLOAT" category="System">
@ -9198,7 +9187,7 @@ for current-based compensation [G/kA]</short_desc> @@ -9198,7 +9187,7 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 3 relative to airframe</short_desc>
<long_desc>An internal sensor will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="-1">Internal</value>
@ -9243,7 +9232,6 @@ for current-based compensation [G/kA]</short_desc> @@ -9243,7 +9232,6 @@ for current-based compensation [G/kA]</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="CAL_MAG3_XCOMP" default="0.0" type="FLOAT" category="System">
@ -9545,7 +9533,7 @@ How often the sensor is readout</short_desc> @@ -9545,7 +9533,7 @@ How often the sensor is readout</short_desc>
<short_desc>Board rotation</short_desc>
<long_desc>This parameter defines the rotation of the FMU board relative to the platform.</long_desc>
<min>-1</min>
<max>41</max>
<max>40</max>
<reboot_required>true</reboot_required>
<values>
<value code="0">No rotation</value>
@ -9589,7 +9577,6 @@ How often the sensor is readout</short_desc> @@ -9589,7 +9577,6 @@ How often the sensor is readout</short_desc>
<value code="38">Roll 90°, Pitch 68°, Yaw 293°</value>
<value code="39">Pitch 315°</value>
<value code="40">Roll 90°, Pitch 315°</value>
<value code="41">Roll 270°, Yaw 180°</value>
</values>
</parameter>
<parameter name="SENS_BOARD_X_OFF" default="0.0" type="FLOAT">

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