diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index 8eaafd2..a78627e 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -5100,10 +5100,10 @@
s
2
-
+
Maximum downwards acceleration in climb rate controlled modes
- 2.0
- 15.0
+ 2
+ 15
m/s^2
1
1
@@ -5126,10 +5126,10 @@
2
1
-
+
Maximum upwards acceleration in climb rate controlled modes
- 2.0
- 15.0
+ 2
+ 15
m/s^2
1
1
@@ -5245,8 +5245,8 @@
Minimum collective thrust in Stabilized mode
The value is mapped to the lowest throttle stick position in Stabilized mode. Too low collective thrust leads to loss of roll/pitch/yaw torque control authority. Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE).
- 0.0
- 1.0
+ 0
+ 1
norm
2
0.01
@@ -5270,8 +5270,8 @@
Manual yaw rate input filter time constant
Not used in Stabilized mode Setting this parameter to 0 disables the filter
- 0.0
- 5.0
+ 0
+ 5
s
2
0.01
@@ -5323,7 +5323,7 @@
Horizontal thrust margin
Margin that is kept for horizontal control when higher priority vertical thrust is saturated. To avoid completely starving horizontal control with high vertical error.
- 0.0
+ 0
0.5
norm
2
@@ -5367,7 +5367,7 @@
Numerical velocity derivative low pass cutoff frequency
- 0.0
+ 0
10
Hz
1