<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>
<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>
<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>
<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>
<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>
<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>
<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>
<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>
<short_desc>Rotation of magnetometer 0 relative to airframe</short_desc>
<long_desc>An internal magnetometer 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>
<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>
<reboot_required>true</reboot_required>
<values>
<valuecode="-1">Internal mag</value>
<valuecode="-1">Internal</value>
<valuecode="0">No rotation</value>
<valuecode="1">Yaw 45°</value>
<valuecode="2">Yaw 90°</value>
...
...
@@ -8396,12 +8869,12 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 1 relative to airframe</short_desc>
<long_desc>An internal magnetometer 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>
<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>
<reboot_required>true</reboot_required>
<values>
<valuecode="-1">Internal mag</value>
<valuecode="-1">Internal</value>
<valuecode="0">No rotation</value>
<valuecode="1">Yaw 45°</value>
<valuecode="2">Yaw 90°</value>
...
...
@@ -8511,12 +8984,12 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 2 relative to airframe</short_desc>
<long_desc>An internal magnetometer 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>
<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>
<reboot_required>true</reboot_required>
<values>
<valuecode="-1">Internal mag</value>
<valuecode="-1">Internal</value>
<valuecode="0">No rotation</value>
<valuecode="1">Yaw 45°</value>
<valuecode="2">Yaw 90°</value>
...
...
@@ -8626,12 +9099,12 @@ for current-based compensation [G/kA]</short_desc>
<short_desc>Rotation of magnetometer 3 relative to airframe</short_desc>
<long_desc>An internal magnetometer 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>
<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>
<reboot_required>true</reboot_required>
<values>
<valuecode="-1">Internal mag</value>
<valuecode="-1">Internal</value>
<valuecode="0">No rotation</value>
<valuecode="1">Yaw 45°</value>
<valuecode="2">Yaw 90°</value>
...
...
@@ -10579,6 +11052,54 @@ How often the sensor is readout</short_desc>