diff --git a/src/modules/vtol_att_control/standard.cpp b/src/modules/vtol_att_control/standard.cpp
index 8bcf9a0c5f61..b2ad22eced33 100644
--- a/src/modules/vtol_att_control/standard.cpp
+++ b/src/modules/vtol_att_control/standard.cpp
@@ -67,6 +67,9 @@ Standard::Standard(VtolAttitudeControl *attc) :
 	_params_handles_standard.pitch_setpoint_offset = param_find("FW_PSP_OFF");
 	_params_handles_standard.reverse_output = param_find("VT_B_REV_OUT");
 	_params_handles_standard.reverse_delay = param_find("VT_B_REV_DEL");
+
+	_params_handles_standard.mc_to_fw_gain_roll = param_find("VT_MC_AILE_GAIN");
+	_params_handles_standard.mc_to_fw_gain_pitch = param_find("VT_MC_ELEV_GAIN");
 }
 
 void
@@ -103,6 +106,12 @@ Standard::parameters_update()
 	param_get(_params_handles_standard.reverse_delay, &v);
 	_params_standard.reverse_delay = math::constrain(v, 0.0f, 10.0f);
 
+	param_get(_params_handles_standard.mc_to_fw_gain_roll, &v);
+	_params_standard.mc_to_fw_gain_roll = math::constrain(v, 0.0f, 10.0f);
+
+	param_get(_params_handles_standard.mc_to_fw_gain_pitch, &v);
+	_params_standard.mc_to_fw_gain_pitch = math::constrain(v, 0.0f, 10.0f);
+
 }
 
 void Standard::update_vtol_state()
@@ -442,11 +451,11 @@ void Standard::fill_actuator_outputs()
 		} else {
 			// roll
 			_actuators_out_1->control[actuator_controls_s::INDEX_ROLL] =
-				_actuators_fw_in->control[actuator_controls_s::INDEX_ROLL];
+				_actuators_fw_in->control[actuator_controls_s::INDEX_ROLL] * _params_standard.mc_to_fw_gain_roll;
 
 			// pitch
 			_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] =
-				_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH];
+				_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH] * _params_standard.mc_to_fw_gain_pitch;
 
 			_actuators_out_1->control[actuator_controls_s::INDEX_YAW] = 0.0f;
 			_actuators_out_1->control[actuator_controls_s::INDEX_AIRBRAKES] = 0.0f;
diff --git a/src/modules/vtol_att_control/standard.h b/src/modules/vtol_att_control/standard.h
index da623cfc30b5..3bf456de2990 100644
--- a/src/modules/vtol_att_control/standard.h
+++ b/src/modules/vtol_att_control/standard.h
@@ -74,6 +74,8 @@ class Standard : public VtolType
 		float pitch_setpoint_offset;
 		float reverse_output;
 		float reverse_delay;
+		float mc_to_fw_gain_roll;
+		float mc_to_fw_gain_pitch;
 	} _params_standard;
 
 	struct {
@@ -84,6 +86,8 @@ class Standard : public VtolType
 		param_t pitch_setpoint_offset;
 		param_t reverse_output;
 		param_t reverse_delay;
+		param_t mc_to_fw_gain_roll;
+		param_t mc_to_fw_gain_pitch;
 	} _params_handles_standard;
 
 	enum class vtol_mode {
diff --git a/src/modules/vtol_att_control/standard_params.c b/src/modules/vtol_att_control/standard_params.c
index 1427e5a07112..69d52eb8477e 100644
--- a/src/modules/vtol_att_control/standard_params.c
+++ b/src/modules/vtol_att_control/standard_params.c
@@ -112,3 +112,25 @@ PARAM_DEFINE_FLOAT(VT_B_REV_DEL, 0.0f);
  * @group VTOL Attitude Control
  */
 PARAM_DEFINE_FLOAT(VT_PSHER_RMP_DT, 3.0f);
+
+/**
+ * Roll scale on fixed-wing actuators in hover.
+ *
+ * Determines how much the roll controlling surfaces (e.g. ailerons or elevons) are used to assist the multicopter motors in hover.
+ *
+ * @min 0
+ * @max 3
+ * @group VTOL Attitude Control
+ */
+PARAM_DEFINE_FLOAT(VT_MC_AILE_GAIN, 1.0f);
+
+/**
+ * Pitch scale on fixed-wing actuators in hover.
+ *
+ * Determines how much the pitch controlling surfaces (e.g. elevator or elevons) are used to assist the multicopter motors in hover.
+ *
+ * @min 0
+ * @max 3
+ * @group VTOL Attitude Control
+ */
+PARAM_DEFINE_FLOAT(VT_MC_ELEV_GAIN, 1.0f);