diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index 5cb9e8fcdadfc833270755ff64a71ae8d2250079..bd13ed1e479bfc99681d811e756f967c89bd300c 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -8308,7 +8308,7 @@ Particularly useful for testing different low-battery behaviour
Rotation of magnetometer 0 relative to airframe
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.
-1
- 45
+ 41
true
Internal mag
@@ -8354,10 +8354,6 @@ Particularly useful for testing different low-battery behaviour
Pitch 315°
Roll 90°, Pitch 315°
Roll 270°, Yaw 180°
- Roll 270°, Yaw 270°
- Pitch 90°, Yaw 180°
- Pitch 9°, Yaw 180°
- Pitch 45°
@@ -8427,7 +8423,7 @@ for current-based compensation [G/kA]
Rotation of magnetometer 1 relative to airframe
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.
-1
- 45
+ 41
true
Internal mag
@@ -8473,10 +8469,6 @@ for current-based compensation [G/kA]
Pitch 315°
Roll 90°, Pitch 315°
Roll 270°, Yaw 180°
- Roll 270°, Yaw 270°
- Pitch 90°, Yaw 180°
- Pitch 9°, Yaw 180°
- Pitch 45°
@@ -8546,7 +8538,7 @@ for current-based compensation [G/kA]
Rotation of magnetometer 2 relative to airframe
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.
-1
- 45
+ 41
true
Internal mag
@@ -8592,10 +8584,6 @@ for current-based compensation [G/kA]
Pitch 315°
Roll 90°, Pitch 315°
Roll 270°, Yaw 180°
- Roll 270°, Yaw 270°
- Pitch 90°, Yaw 180°
- Pitch 9°, Yaw 180°
- Pitch 45°
@@ -8665,7 +8653,7 @@ for current-based compensation [G/kA]
Rotation of magnetometer 3 relative to airframe
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.
-1
- 45
+ 41
true
Internal mag
@@ -8711,10 +8699,6 @@ for current-based compensation [G/kA]
Pitch 315°
Roll 90°, Pitch 315°
Roll 270°, Yaw 180°
- Roll 270°, Yaw 270°
- Pitch 90°, Yaw 180°
- Pitch 9°, Yaw 180°
- Pitch 45°
@@ -8997,6 +8981,8 @@ How often the sensor is readout
Board rotation
This parameter defines the rotation of the FMU board relative to the platform.
+ -1
+ 41
true
No rotation
@@ -9025,16 +9011,22 @@ How often the sensor is readout
Roll 270°, Yaw 135°
Pitch 90°
Pitch 270°
- Roll 270°, Yaw 270°
- Roll 180°, Pitch 270°
- Pitch 90°, Yaw 180
- Pitch 90°, Roll 90°
- Yaw 293°, Pitch 68°, Roll 90° (Solo)
- Pitch 90°, Roll 270°
- Pitch 9°, Yaw 180°
- Pitch 45°
- Pitch 315°
- Roll 90°, Yaw 270°
+ Pitch 180°, Yaw 90°
+ Pitch 180°, Yaw 270°
+ Roll 90°, Pitch 90°
+ Roll 180°, Pitch 90°
+ Roll 270°, Pitch 90°
+ Roll 90°, Pitch 180°
+ Roll 270°, Pitch 180°
+ Roll 90°, Pitch 270°
+ Roll 180°, Pitch 270°
+ Roll 270°, Pitch 270°
+ Roll 90°, Pitch 180°, Yaw 90°
+ Roll 90°, Yaw 270°
+ Roll 90°, Pitch 68°, Yaw 293°
+ Pitch 315°
+ Roll 90°, Pitch 315°
+ Roll 270°, Yaw 180°