diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index 79855cb9e658175f6ca567df6b4c7a7862da7fe5..4b4c9ab7efecd134603296aff702e3a2bacc8770 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -8302,7 +8302,7 @@ 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
- 30
+ 45
true
Internal mag
@@ -8332,6 +8332,26 @@ Particularly useful for testing different low-battery behaviour
Roll 270°, Yaw 135°
Pitch 90°
Pitch 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°
+ Roll 270°, Yaw 270°
+ Pitch 90°, Yaw 180°
+ Pitch 9°, Yaw 180°
+ Pitch 45°
@@ -8383,7 +8403,7 @@ 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
- 30
+ 45
true
Internal mag
@@ -8413,6 +8433,26 @@ for current-based compensation [G/kA]
Roll 270°, Yaw 135°
Pitch 90°
Pitch 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°
+ Roll 270°, Yaw 270°
+ Pitch 90°, Yaw 180°
+ Pitch 9°, Yaw 180°
+ Pitch 45°
@@ -8464,7 +8504,7 @@ 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
- 30
+ 45
true
Internal mag
@@ -8494,6 +8534,26 @@ for current-based compensation [G/kA]
Roll 270°, Yaw 135°
Pitch 90°
Pitch 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°
+ Roll 270°, Yaw 270°
+ Pitch 90°, Yaw 180°
+ Pitch 9°, Yaw 180°
+ Pitch 45°
@@ -8545,7 +8605,7 @@ 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
- 30
+ 45
true
Internal mag
@@ -8575,6 +8635,26 @@ for current-based compensation [G/kA]
Roll 270°, Yaw 135°
Pitch 90°
Pitch 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°
+ Roll 270°, Yaw 270°
+ Pitch 90°, Yaw 180°
+ Pitch 9°, Yaw 180°
+ Pitch 45°