LCOV - code coverage report

Current view: top level - AC_AttitudeControl - AC_AttitudeControl_Multi_6DoF.cpp (source / functions) Hit Total Coverage Test: lcov.info Lines: 40 72 55.6 % Date: 2026-09-09 11:02:08 Functions: 6 13 46.2 %

Function Name	Hit count
AC_AttitudeControl_Multi_6DoF::input_quaternion(QuaternionT<float>&, Vector3<float>)	0
AC_AttitudeControl_Multi_6DoF::input_rate_bf_roll_pitch_yaw_rads(float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_rate_bf_roll_pitch_yaw_2_rads(float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_rate_bf_roll_pitch_yaw_3_rads(float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_euler_rate_roll_pitch_yaw_rads(float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_angle_step_bf_roll_pitch_yaw_rad(float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_euler_rate_yaw_euler_angle_pitch_bf_roll_rad(bool, float, float, float)	0
AC_AttitudeControl_Multi_6DoF::input_thrust_vector_heading_rad(Vector3<float> const&, float, float)	6664
AC_AttitudeControl_Multi_6DoF::input_euler_angle_roll_pitch_yaw_rad(float, float, float, bool)	6664
AC_AttitudeControl_Multi_6DoF::input_thrust_vector_rate_heading_rads(Vector3<float> const&, float, bool)	24871
AC_AttitudeControl_Multi_6DoF::input_euler_angle_roll_pitch_euler_rate_yaw_rad(float, float, float)	42204
AC_AttitudeControl_Multi_6DoF::set_forward_lateral_rad(float&, float&)	48868
AC_AttitudeControl_Multi_6DoF::rate_controller_run()	49958

Generated by: LCOV version 1.14