diff --git a/libraries/AC_AttitudeControl/AC_AttitudeControl.h b/libraries/AC_AttitudeControl/AC_AttitudeControl.h
index 9cc8a9177f..e4e51a856a 100644
--- a/libraries/AC_AttitudeControl/AC_AttitudeControl.h
+++ b/libraries/AC_AttitudeControl/AC_AttitudeControl.h
@@ -264,7 +264,7 @@ protected:
     virtual float rate_bf_to_motor_yaw(float rate_target_rads);
 
     // Compute a throttle value that is adjusted for the tilt angle of the vehicle
-    virtual float get_boosted_throttle(float throttle_in) = 0;
+    virtual float get_throttle_boosted(float throttle_in) = 0;
 
     // Return angle in radians to be added to roll angle. Used by heli to counteract
     // tail rotor thrust in hover. Overloaded by AC_Attitude_Heli to return angle.
diff --git a/libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.h b/libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.h
index 1212442690..51c6d2fc64 100644
--- a/libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.h
+++ b/libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.h
@@ -125,9 +125,6 @@ private:
     //
     // throttle methods
     //
-
-    // calculate total body frame throttle required to produce the given earth frame throttle
-    float get_boosted_throttle(float throttle_in);
     
     // pass through for roll and pitch
     int16_t _passthrough_roll;
diff --git a/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.cpp b/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.cpp
index 41b44c18a4..6a05558900 100644
--- a/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.cpp
+++ b/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.cpp
@@ -153,7 +153,7 @@ void AC_AttitudeControl_Multi::set_throttle_out(float throttle_in, bool apply_an
     _throttle_in_filt.apply(throttle_in, _dt);
     _motors.set_throttle_filter_cutoff(filter_cutoff);
     if (apply_angle_boost) {
-        _motors.set_throttle(get_boosted_throttle(throttle_in));
+        _motors.set_throttle(get_throttle_boosted(throttle_in));
     }else{
         _motors.set_throttle(throttle_in);
         // Clear angle_boost for logging purposes
@@ -163,7 +163,7 @@ void AC_AttitudeControl_Multi::set_throttle_out(float throttle_in, bool apply_an
 
 // returns a throttle including compensation for roll/pitch angle
 // throttle value should be 0 ~ 1
-float AC_AttitudeControl_Multi::get_boosted_throttle(float throttle_in)
+float AC_AttitudeControl_Multi::get_throttle_boosted(float throttle_in)
 {
     if (!_angle_boost_enabled) {
         _angle_boost = 0;
diff --git a/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.h b/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.h
index cf9fa1409b..a47ab3751f 100644
--- a/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.h
+++ b/libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.h
@@ -59,7 +59,7 @@ public:
     void set_throttle_out(float throttle_in, bool apply_angle_boost, float filt_cutoff) override;
 
     // calculate total body frame throttle required to produce the given earth frame throttle
-    float get_boosted_throttle(float throttle_in);
+    float get_throttle_boosted(float throttle_in);
 
     // user settable parameters
     static const struct AP_Param::GroupInfo var_info[];