|
Function Name  |
Hit count  |
| AC_AttitudeControl::get_rpy_srate(float&, float&, float&) |
2928 |
| AC_AttitudeControl::accel_limiting(bool) |
0 |
| AC_AttitudeControl::pre_arm_checks(char const*, char*, unsigned char) |
99876 |
| AC_AttitudeControl::input_quaternion(QuaternionT<float>&, Vector3<float>) |
98513 |
| AC_AttitudeControl::convert_parameters() |
1285 |
| AC_AttitudeControl::scale_I_to_angle_P() |
0 |
| AC_AttitudeControl::body_to_euler_limit(QuaternionT<float> const&, Vector3<float> const&) |
33562520 |
| AC_AttitudeControl::inertial_frame_reset() |
3590 |
| AC_AttitudeControl::max_rate_step_bf_yaw() |
2806 |
| AC_AttitudeControl::landed_gain_reduction(bool) |
30412448 |
| AC_AttitudeControl::max_rate_step_bf_roll() |
786 |
| AC_AttitudeControl::reset_target_and_rate(bool) |
16271 |
| AC_AttitudeControl::max_rate_step_bf_pitch() |
772 |
| AC_AttitudeControl::update_attitude_target() |
32955703 |
| AC_AttitudeControl::body_to_euler_derivative(QuaternionT<float> const&, Vector3<float> const&, Vector3<float>&) |
35566276 |
| AC_AttitudeControl::euler_derivative_to_body(QuaternionT<float> const&, Vector3<float> const&, Vector3<float>&) |
43492745 |
| AC_AttitudeControl::reset_yaw_target_and_rate(bool) |
11086303 |
| AC_AttitudeControl::relax_attitude_controllers() |
2709520 |
| AC_AttitudeControl::input_thrust_vector_heading(Vector3<float> const&, AC_AttitudeControl::HeadingCommand) |
11730957 |
| AC_AttitudeControl::attitude_controller_run_quat() |
32956174 |
| AC_AttitudeControl::rate_controller_target_reset() |
33074393 |
| AC_AttitudeControl::reset_rate_controller_I_terms() |
11544323 |
| AC_AttitudeControl::input_thrust_vector_heading_rad(Vector3<float> const&, float, float) |
2743232 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_cds(float, float, float) |
360 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_rads(float, float, float) |
113716 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_2_cds(float, float, float) |
9994 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_3_cds(float, float, float) |
0 |
| AC_AttitudeControl::input_euler_angle_roll_pitch_yaw_cd(float, float, float, bool) |
965469 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_2_rads(float, float, float) |
9994 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_3_rads(float, float, float) |
0 |
| AC_AttitudeControl::input_euler_angle_roll_pitch_yaw_rad(float, float, float, bool) |
2183113 |
| AC_AttitudeControl::input_euler_rate_roll_pitch_yaw_rads(float, float, float) |
0 |
| AC_AttitudeControl::update_ang_vel_target_from_att_error(Vector3<float> const&) |
32956174 |
| AC_AttitudeControl::input_thrust_vector_rate_heading_rads(Vector3<float> const&, float, bool) |
12695991 |
| AC_AttitudeControl::input_angle_step_bf_roll_pitch_yaw_rad(float, float, float) |
471 |
| AC_AttitudeControl::input_rate_step_bf_roll_pitch_yaw_rads(float, float, float) |
210919 |
| AC_AttitudeControl::reset_rate_controller_I_terms_smoothly() |
2502156 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_no_shaping_cds(float, float, float) |
414050 |
| AC_AttitudeControl::input_rate_bf_roll_pitch_yaw_no_shaping_rads(float, float, float) |
414050 |
| AC_AttitudeControl::input_euler_angle_roll_pitch_euler_rate_yaw_cd(float, float, float) |
2228903 |
| AC_AttitudeControl::input_euler_angle_roll_pitch_euler_rate_yaw_rad(float, float, float) |
15121138 |
| AC_AttitudeControl::ang_vel_limit(Vector3<float>&, float, float, float) const |
37634590 |
| AC_AttitudeControl::get_latest_gyro() const |
35665694 |
| AC_AttitudeControl::lean_angle_max_cd() const |
10678463 |
| AC_AttitudeControl::lean_angle_max_rad() const |
55927217 |
| AC_AttitudeControl::get_slew_yaw_max_rads() const |
14797186 |
| AC_AttitudeControl::attitude_command_model(float, float, float&, float&, float, float, float, float) const |
106487924 |
| AC_AttitudeControl::attitude_from_thrust_vector(Vector3<float>, float) const |
15470758 |
| AC_AttitudeControl::command_model_rate_predictor(Vector2<float> const&, Vector2<float>&, Vector2<float>&, float) const |
4579903 |
| AC_AttitudeControl::get_althold_lean_angle_max_cd() const |
843411 |
| AC_AttitudeControl::thrust_vector_rotation_angles(QuaternionT<float> const&, QuaternionT<float> const&, QuaternionT<float>&, Vector3<float>&, float&, float&) const |
48403797 |
| AC_AttitudeControl::get_althold_lean_angle_max_rad() const |
31746108 |
| AC_AttitudeControl::thrust_heading_rotation_angles(QuaternionT<float>&, QuaternionT<float> const&, Vector3<float>&, float&, float&) const |
32964574 |