diff --git a/ROMFS/px4fmu_common/init.d/10016_3dr_iris b/ROMFS/px4fmu_common/init.d/10016_3dr_iris
index a2536e5418..ffaa935055 100644
--- a/ROMFS/px4fmu_common/init.d/10016_3dr_iris
+++ b/ROMFS/px4fmu_common/init.d/10016_3dr_iris
@@ -13,11 +13,11 @@ if [ $AUTOCNF == yes ]
 then
 	# TODO tune roll/pitch separately
 	param set MC_ROLL_P 7.0
-	param set MC_ROLLRATE_P 0.13
+	param set MC_ROLLRATE_P 0.15
 	param set MC_ROLLRATE_I 0.05
 	param set MC_ROLLRATE_D 0.004
 	param set MC_PITCH_P 7.0
-	param set MC_PITCHRATE_P 0.13
+	param set MC_PITCHRATE_P 0.15
 	param set MC_PITCHRATE_I 0.05
 	param set MC_PITCHRATE_D 0.004
 	param set MC_YAW_P 2.5
diff --git a/ROMFS/px4fmu_common/init.d/4010_dji_f330 b/ROMFS/px4fmu_common/init.d/4010_dji_f330
index 4303320ffe..aea5292a24 100644
--- a/ROMFS/px4fmu_common/init.d/4010_dji_f330
+++ b/ROMFS/px4fmu_common/init.d/4010_dji_f330
@@ -16,11 +16,11 @@ sh /etc/init.d/4001_quad_x
 if [ $AUTOCNF == yes ]
 then
 	param set MC_ROLL_P 7.0
-	param set MC_ROLLRATE_P 0.13
+	param set MC_ROLLRATE_P 0.15
 	param set MC_ROLLRATE_I 0.05
 	param set MC_ROLLRATE_D 0.003
 	param set MC_PITCH_P 7.0
-	param set MC_PITCHRATE_P 0.13
+	param set MC_PITCHRATE_P 0.15
 	param set MC_PITCHRATE_I 0.05
 	param set MC_PITCHRATE_D 0.003
 	param set MC_YAW_P 2.8
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 9af68a4e1e..30a50480e0 100644
--- a/src/modules/mc_att_control/mc_att_control_params.c
+++ b/src/modules/mc_att_control/mc_att_control_params.c
@@ -36,8 +36,8 @@
  * Parameters for multicopter attitude controller.
  *
  * @author Tobias Naegeli <naegelit@student.ethz.ch>
- * @author Lorenz Meier <lm@inf.ethz.ch>
- * @author Anton Babushkin <anton.babushkin@me.com>
+ * @author Lorenz Meier <lorenz@px4.io>
+ * @author Anton Babushkin <anton@px4.io>
  */
 
 #include <systemlib/param/param.h>
@@ -60,7 +60,7 @@ PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.5f);
  * @min 0.0
  * @group Multicopter Attitude Control
  */
-PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.12f);
+PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.15f);
 
 /**
  * Roll rate I gain
@@ -111,7 +111,7 @@ PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.5f);
  * @min 0.0
  * @group Multicopter Attitude Control
  */
-PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.12f);
+PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.15f);
 
 /**
  * Pitch rate I gain