diff --git a/src/modules/mc_att_control/mc_att_control_params.c b/src/modules/mc_att_control/mc_att_control_params.c
index 0427e27908..65d3b9fbc7 100644
--- a/src/modules/mc_att_control/mc_att_control_params.c
+++ b/src/modules/mc_att_control/mc_att_control_params.c
@@ -47,6 +47,7 @@
  * @min 0.15
  * @max 0.25
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLL_TC, 0.2f);
@@ -59,6 +60,7 @@ PARAM_DEFINE_FLOAT(MC_ROLL_TC, 0.2f);
  * @min 0.15
  * @max 0.25
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCH_TC, 0.2f);
@@ -69,7 +71,9 @@ PARAM_DEFINE_FLOAT(MC_PITCH_TC, 0.2f);
  * Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.
  *
  * @min 0.0
+ * @max 8
  * @decimal 2
+ * @increment 0.1
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.5f);
@@ -80,7 +84,9 @@ PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.5f);
  * Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
  * @min 0.0
+ * @max 0.5
  * @decimal 3
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.15f);
@@ -91,6 +97,7 @@ PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.15f);
  * Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset.
  *
  * @min 0.0
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLLRATE_I, 0.05f);
@@ -101,7 +108,9 @@ PARAM_DEFINE_FLOAT(MC_ROLLRATE_I, 0.05f);
  * Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
  *
  * @min 0.0
+ * @max 0.01
  * @decimal 4
+ * @increment 0.0005
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLLRATE_D, 0.003f);
@@ -124,7 +133,9 @@ PARAM_DEFINE_FLOAT(MC_ROLLRATE_FF, 0.0f);
  *
  * @unit 1/s
  * @min 0.0
+ * @max 10
  * @decimal 2
+ * @increment 0.0005
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.5f);
@@ -135,7 +146,9 @@ PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.5f);
  * Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
  * @min 0.0
+ * @max 0.6
  * @decimal 3
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.15f);
@@ -147,6 +160,7 @@ PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.15f);
  *
  * @min 0.0
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCHRATE_I, 0.05f);
@@ -158,6 +172,7 @@ PARAM_DEFINE_FLOAT(MC_PITCHRATE_I, 0.05f);
  *
  * @min 0.0
  * @decimal 4
+ * @increment 0.0005
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCHRATE_D, 0.003f);
@@ -180,7 +195,9 @@ PARAM_DEFINE_FLOAT(MC_PITCHRATE_FF, 0.0f);
  *
  * @unit 1/s
  * @min 0.0
+ * @max 5
  * @decimal 2
+ * @increment 0.1
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAW_P, 2.8f);
@@ -191,7 +208,9 @@ PARAM_DEFINE_FLOAT(MC_YAW_P, 2.8f);
  * Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.
  *
  * @min 0.0
+ * @max 0.6
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.2f);
@@ -203,6 +222,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.2f);
  *
  * @min 0.0
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRATE_I, 0.1f);
@@ -214,6 +234,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_I, 0.1f);
  *
  * @min 0.0
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f);
@@ -225,6 +246,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f);
  *
  * @min 0.0
  * @decimal 4
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRATE_FF, 0.0f);
@@ -237,6 +259,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_FF, 0.0f);
  * @min 0.0
  * @max 1.0
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f);
@@ -250,6 +273,7 @@ PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f);
  * @min 0.0
  * @max 360.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ROLLRATE_MAX, 220.0f);
@@ -263,6 +287,7 @@ PARAM_DEFINE_FLOAT(MC_ROLLRATE_MAX, 220.0f);
  * @min 0.0
  * @max 360.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_PITCHRATE_MAX, 220.0f);
@@ -276,6 +301,7 @@ PARAM_DEFINE_FLOAT(MC_PITCHRATE_MAX, 220.0f);
  * @min 0.0
  * @max 360.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRATE_MAX, 200.0f);
@@ -292,6 +318,7 @@ PARAM_DEFINE_FLOAT(MC_YAWRATE_MAX, 200.0f);
  * @min 0.0
  * @max 120.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_YAWRAUTO_MAX, 45.0f);
@@ -301,8 +328,9 @@ PARAM_DEFINE_FLOAT(MC_YAWRAUTO_MAX, 45.0f);
  *
  * @unit deg/s
  * @min 0.0
- * @max 360.0
+ * @max 1000.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ACRO_R_MAX, 360.0f);
@@ -312,8 +340,9 @@ PARAM_DEFINE_FLOAT(MC_ACRO_R_MAX, 360.0f);
  *
  * @unit deg/s
  * @min 0.0
- * @max 360.0
+ * @max 1000.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ACRO_P_MAX, 360.0f);
@@ -323,7 +352,9 @@ PARAM_DEFINE_FLOAT(MC_ACRO_P_MAX, 360.0f);
  *
  * @unit deg/s
  * @min 0.0
+ * @max 1000.0
  * @decimal 1
+ * @increment 5
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_ACRO_Y_MAX, 360.0f);
@@ -338,6 +369,7 @@ PARAM_DEFINE_FLOAT(MC_ACRO_Y_MAX, 360.0f);
  * @min 0.0
  * @max 1.0
  * @decimal 2
+ * @increment 0.01
  * @group Multicopter Attitude Control
  */
 PARAM_DEFINE_FLOAT(MC_RATT_TH, 1.0f);