diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index af5b048..2f04c53 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -4885,17 +4885,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX
1.0
1
-
+
Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again
- 0.005
- 0.1
+ defined as correction acceleration in m/s^2 per m/s^2 velocity derivative
+ 0.1
+ 2.0
3
-
+
Integral gain for horizontal velocity error
- Non-zero value allows to eliminate steady state errors in the presence of disturbances like wind.
+ defined as correction acceleration in m/s^2 per m velocity integral Non-zero value allows to eliminate steady state errors in the presence of disturbances like wind.
0.0
- 3.0
+ 60.0
3
@@ -4907,10 +4908,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX
2
1
-
+
Proportional gain for horizontal velocity error
- 0.06
- 0.15
+ defined as correction acceleration in m/s^2 per m/s velocity error
+ 1.2
+ 3.0
2
@@ -4933,17 +4935,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX
1.5
2
-
+
Differential gain for vertical velocity error
+ defined as correction acceleration in m/s^2 per m/s^2 velocity derivative
0.0
- 0.1
+ 2.0
3
-
+
Integral gain for vertical velocity error
- Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff.
- 0.01
- 0.1
+ defined as correction acceleration in m/s^2 per m velocity integral Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff.
+ 0.2
+ 2.0
3
@@ -4961,10 +4964,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX
m/s
1
-
+
Proportional gain for vertical velocity error
- 0.1
- 0.4
+ defined as correction acceleration in m/s^2 per m/s velocity error
+ 2.0
+ 8.0
2