diff --git a/src/modules/mc_att_control_multiplatform/mc_att_control_params.c b/src/modules/mc_att_control_multiplatform/mc_att_control_params.c
index e34732d1f3..983e345269 100644
--- a/src/modules/mc_att_control_multiplatform/mc_att_control_params.c
+++ b/src/modules/mc_att_control_multiplatform/mc_att_control_params.c
@@ -45,6 +45,7 @@
  *
  * Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -55,6 +56,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLL_P);
  *
  * Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -65,6 +67,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLLRATE_P);
  *
  * Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -75,6 +78,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_ROLLRATE_I);
  *
  * Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -96,6 +100,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCH_P);
  *
  * Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -106,6 +111,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCHRATE_P);
  *
  * Pitch rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -116,6 +122,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_PITCHRATE_I);
  *
  * Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -137,6 +144,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAW_P);
  *
  * Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -147,6 +155,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_P);
  *
  * Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -157,6 +166,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_I);
  *
  * Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
  *
+ * @unit
  * @min 0.0
  * @group Multicopter Attitude Control
  */
@@ -167,6 +177,7 @@ PX4_PARAM_DEFINE_FLOAT(MP_YAWRATE_D);
  *
  * Feed forward weight for manual yaw control. 0 will give slow responce and no overshot, 1 - fast responce and big overshot.
  *
+ * @unit
  * @min 0.0
  * @max 1.0
  * @group Multicopter Attitude Control