diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index 0f8aeba83d9101ec182b8792be6e3513d91feda8..22a883ae27583f0737e1c014ad35548afb65004e 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -1573,7 +1573,7 @@ This parameter is used when the magnetometer fusion method is set automatically
6
modules/ekf2
-
+
Magnetic declination
deg
1
@@ -4040,19 +4040,6 @@ Used to calculate increased terrain random walk nosie due to movement0.5
modules/navigator
-
- Multirotor only. Yaw setpoint mode
- The values are defined in the enum mission_altitude_mode
- 0
- 3
- modules/navigator
-
- Heading as set by waypoint
- Heading towards waypoint
- Heading towards home
- Heading away from home
-
-
Max yaw error in degrees needed for waypoint heading acceptance
0
@@ -4072,6 +4059,19 @@ Used to calculate increased terrain random walk nosie due to movement1
modules/navigator
+
+ Yaw mode
+ Specifies the heading in Auto.
+ 0
+ 2
+ modules/mc_pos_control
+
+ towards waypoint
+ towards home
+ away from home
+ along trajectory
+
+
Acceptance Radius
Default acceptance radius, overridden by acceptance radius of waypoint if set. For fixed wing the L1 turning distance is used for horizontal acceptance.
@@ -7805,7 +7805,7 @@ to takeoff is reached
-
+
Accelerometer 0 enabled
modules/sensors
@@ -7838,7 +7838,7 @@ to takeoff is reached
Accelerometer Z-axis scaling factor
modules/sensors
-
+
Accelerometer 1 enabled
modules/sensors
@@ -7871,7 +7871,7 @@ to takeoff is reached
Accelerometer Z-axis scaling factor
modules/sensors
-
+
Accelerometer 2 enabled
modules/sensors
@@ -7908,148 +7908,123 @@ to takeoff is reached
Primary accel ID
modules/sensors
-
- Airspeed sensor compensation model for the SDP3x
- Model with Pitot CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Model without Pitot (1.5 mm tubes) CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Tube Pressure Drop CAL_AIR_TUBED_MM: Diameter in mm of the pitot and tubes, must have the same diameter. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor and the static + dynamic port length of the pitot.
- modules/sensors
-
- Model with Pitot
- Model without Pitot (1.5 mm tubes)
- Tube Pressure Drop
-
-
-
- Airspeed sensor tube diameter. Only used for the Tube Pressure Drop Compensation
- 0.1
- 100
- millimeter
- modules/sensors
-
-
- Airspeed sensor tube length
- See the CAL_AIR_CMODEL explanation on how this parameter should be set.
- 0.01
- 2.00
- meter
- modules/sensors
-
-
+
Primary baro ID
modules/sensors
-
+
Gyro 0 enabled
modules/sensors
-
+
ID of the Gyro that the calibration is for
modules/sensors
-
+
Gyro X-axis offset
modules/sensors
-
+
Gyro X-axis scaling factor
modules/sensors
-
+
Gyro Y-axis offset
modules/sensors
-
+
Gyro Y-axis scaling factor
modules/sensors
-
+
Gyro Z-axis offset
modules/sensors
-
+
Gyro Z-axis scaling factor
modules/sensors
-
+
Gyro 1 enabled
modules/sensors
-
+
ID of the Gyro that the calibration is for
modules/sensors
-
+
Gyro X-axis offset
modules/sensors
-
+
Gyro X-axis scaling factor
modules/sensors
-
+
Gyro Y-axis offset
modules/sensors
-
+
Gyro Y-axis scaling factor
modules/sensors
-
+
Gyro Z-axis offset
modules/sensors
-
+
Gyro Z-axis scaling factor
modules/sensors
-
+
Gyro 2 enabled
modules/sensors
-
+
ID of the Gyro that the calibration is for
modules/sensors
-
+
Gyro X-axis offset
modules/sensors
-
+
Gyro X-axis scaling factor
modules/sensors
-
+
Gyro Y-axis offset
modules/sensors
-
+
Gyro Y-axis scaling factor
modules/sensors
-
+
Gyro Z-axis offset
modules/sensors
-
+
Gyro Z-axis scaling factor
modules/sensors
-
+
Primary gyro ID
modules/sensors
-
+
Mag 0 enabled
modules/sensors
-
+
ID of Magnetometer the calibration is for
modules/sensors
-
+
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
@@ -8086,40 +8061,40 @@ to takeoff is reached
Pitch 270°
-
+
Magnetometer X-axis offset
modules/sensors
-
+
Magnetometer X-axis scaling factor
modules/sensors
-
+
Magnetometer Y-axis offset
modules/sensors
-
+
Magnetometer Y-axis scaling factor
modules/sensors
-
+
Magnetometer Z-axis offset
modules/sensors
-
+
Magnetometer Z-axis scaling factor
modules/sensors
-
+
Mag 1 enabled
modules/sensors
-
+
ID of Magnetometer the calibration is for
modules/sensors
-
+
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
@@ -8156,40 +8131,40 @@ to takeoff is reached
Pitch 270°
-
+
Magnetometer X-axis offset
modules/sensors
-
+
Magnetometer X-axis scaling factor
modules/sensors
-
+
Magnetometer Y-axis offset
modules/sensors
-
+
Magnetometer Y-axis scaling factor
modules/sensors
-
+
Magnetometer Z-axis offset
modules/sensors
-
+
Magnetometer Z-axis scaling factor
modules/sensors
-
+
Mag 2 enabled
modules/sensors
-
+
ID of Magnetometer the calibration is for
modules/sensors
-
+
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
@@ -8226,40 +8201,40 @@ to takeoff is reached
Pitch 270°
-
+
Magnetometer X-axis offset
modules/sensors
-
+
Magnetometer X-axis scaling factor
modules/sensors
-
+
Magnetometer Y-axis offset
modules/sensors
-
+
Magnetometer Y-axis scaling factor
modules/sensors
-
+
Magnetometer Z-axis offset
modules/sensors
-
+
Magnetometer Z-axis scaling factor
modules/sensors
-
+
Mag 3 enabled
modules/sensors
-
+
ID of Magnetometer the calibration is for
modules/sensors
-
+
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
@@ -8296,31 +8271,31 @@ to takeoff is reached
Pitch 270°
-
+
Magnetometer X-axis offset
modules/sensors
-
+
Magnetometer X-axis scaling factor
modules/sensors
-
+
Magnetometer Y-axis offset
modules/sensors
-
+
Magnetometer Y-axis scaling factor
modules/sensors
-
+
Magnetometer Z-axis offset
modules/sensors
-
+
Magnetometer Z-axis scaling factor
modules/sensors
-
+
Primary mag ID
modules/sensors
@@ -8329,7 +8304,7 @@ to takeoff is reached
Pick the appropriate scaling from the datasheet. this number defines the (linear) conversion from voltage to Pascal (pa). For the MPXV7002DP this is 1000. NOTE: If the sensor always registers zero, try switching the static and dynamic tubes.
modules/sensors
-
+
Differential pressure sensor offset
The offset (zero-reading) in Pascal
modules/sensors
@@ -8366,6 +8341,31 @@ is less than 50% of this value
+
+ Airspeed sensor compensation model for the SDP3x
+ Model with Pitot CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Model without Pitot (1.5 mm tubes) CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Tube Pressure Drop CAL_AIR_TUBED_MM: Diameter in mm of the pitot and tubes, must have the same diameter. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor and the static + dynamic port length of the pitot.
+ modules/sensors
+
+ Model with Pitot
+ Model without Pitot (1.5 mm tubes)
+ Tube Pressure Drop
+
+
+
+ Airspeed sensor tube diameter. Only used for the Tube Pressure Drop Compensation
+ 0.1
+ 100
+ millimeter
+ modules/sensors
+
+
+ Airspeed sensor tube length
+ See the CAL_AIR_CMODEL explanation on how this parameter should be set.
+ 0.01
+ 2.00
+ meter
+ modules/sensors
+
Bitfield selecting mag sides for calibration
DETECT_ORIENTATION_TAIL_DOWN = 1 DETECT_ORIENTATION_NOSE_DOWN = 2 DETECT_ORIENTATION_LEFT = 4 DETECT_ORIENTATION_RIGHT = 8 DETECT_ORIENTATION_UPSIDE_DOWN = 16 DETECT_ORIENTATION_RIGHTSIDE_UP = 32