AC_AttitudeControl: Vector3f multiplication clean up

ArduPilot · Sep 16, 2024 · ea22663 · ea22663
1 parent 5e27e31
commit ea22663
Showing 1 changed file with 2 additions and 2 deletions.
diff --git a/libraries/AC_AttitudeControl/AC_AttitudeControl.cpp b/libraries/AC_AttitudeControl/AC_AttitudeControl.cpp
@@ -500,7 +500,7 @@ void AC_AttitudeControl::input_rate_bf_roll_pitch_yaw(float roll_rate_bf_cds, fl
     } else {
         // When feedforward is not enabled, the quaternion is calculated and is input into the target and the feedforward rate is zeroed.
         Quaternion attitude_target_update;
-        attitude_target_update.from_axis_angle(Vector3f{roll_rate_rads * _dt, pitch_rate_rads * _dt, yaw_rate_rads * _dt});
+        attitude_target_update.from_axis_angle(Vector3f{roll_rate_rads, pitch_rate_rads, yaw_rate_rads} * _dt);
         _attitude_target = _attitude_target * attitude_target_update;
         _attitude_target.normalize();
 
@@ -557,7 +557,7 @@ void AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_3(float roll_rate_bf_cds,
     }
 
     Vector3f gyro_latest = _ahrs.get_gyro_latest();
-    attitude_ang_error_update_quat.from_axis_angle(Vector3f{(_ang_vel_target.x-gyro_latest.x) * _dt, (_ang_vel_target.y-gyro_latest.y) * _dt, (_ang_vel_target.z-gyro_latest.z) * _dt});
+    attitude_ang_error_update_quat.from_axis_angle((_ang_vel_target - gyro_latest) * _dt);
     _attitude_ang_error = attitude_ang_error_update_quat * _attitude_ang_error;
     _attitude_ang_error.normalize();