#include "Copter.h" /* autotune mode is a wrapper around the AC_AutoTune library */ #if AUTOTUNE_ENABLED == ENABLED bool AutoTune::init() { // only allow AutoTune from some flight modes, for example Stabilize, AltHold, PosHold or Loiter modes if (!copter.flightmode->allows_autotune()) { return false; } // ensure throttle is above zero if (copter.ap.throttle_zero) { return false; } // ensure we are flying if (!copter.motors->armed() || !copter.ap.auto_armed || copter.ap.land_complete) { return false; } // use position hold while tuning if we were in QLOITER bool position_hold = (copter.flightmode->mode_number() == Mode::Number::LOITER || copter.flightmode->mode_number() == Mode::Number::POSHOLD); return init_internals(position_hold, copter.attitude_control, copter.pos_control, copter.ahrs_view, &copter.inertial_nav); } void AutoTune::run() { // apply SIMPLE mode transform to pilot inputs copter.update_simple_mode(); // reset target lean angles and heading while landed if (copter.ap.land_complete) { // we are landed, shut down float target_climb_rate = get_pilot_desired_climb_rate_cms(); // set motors to spin-when-armed if throttle below deadzone, otherwise full range (but motors will only spin at min throttle) if (target_climb_rate < 0.0f) { copter.motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::GROUND_IDLE); } else { copter.motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED); } copter.attitude_control->reset_rate_controller_I_terms_smoothly(); copter.attitude_control->reset_yaw_target_and_rate(); float target_roll, target_pitch, target_yaw_rate; get_pilot_desired_rp_yrate_cd(target_roll, target_pitch, target_yaw_rate); copter.attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(target_roll, target_pitch, target_yaw_rate); copter.pos_control->relax_z_controller(0.0f); copter.pos_control->update_z_controller(); } else { // run autotune mode AC_AutoTune::run(); } } /* get stick input climb rate */ float AutoTune::get_pilot_desired_climb_rate_cms(void) const { float target_climb_rate = copter.get_pilot_desired_climb_rate(copter.channel_throttle->get_control_in()); // get avoidance adjusted climb rate target_climb_rate = copter.mode_autotune.get_avoidance_adjusted_climbrate(target_climb_rate); return target_climb_rate; } /* get stick roll, pitch and yaw rate */ void AutoTune::get_pilot_desired_rp_yrate_cd(float &des_roll_cd, float &des_pitch_cd, float &yaw_rate_cds) { copter.mode_autotune.get_pilot_desired_lean_angles(des_roll_cd, des_pitch_cd, copter.aparm.angle_max, copter.attitude_control->get_althold_lean_angle_max_cd()); yaw_rate_cds = copter.mode_autotune.get_pilot_desired_yaw_rate(copter.channel_yaw->norm_input_dz()); } /* setup z controller velocity and accel limits */ void AutoTune::init_z_limits() { // set vertical speed and acceleration limits copter.pos_control->set_max_speed_accel_z(-copter.get_pilot_speed_dn(), copter.g.pilot_speed_up, copter.g.pilot_accel_z); copter.pos_control->set_correction_speed_accel_z(-copter.get_pilot_speed_dn(), copter.g.pilot_speed_up, copter.g.pilot_accel_z); } #if HAL_LOGGING_ENABLED void AutoTune::log_pids() { copter.logger.Write_PID(LOG_PIDR_MSG, copter.attitude_control->get_rate_roll_pid().get_pid_info()); copter.logger.Write_PID(LOG_PIDP_MSG, copter.attitude_control->get_rate_pitch_pid().get_pid_info()); copter.logger.Write_PID(LOG_PIDY_MSG, copter.attitude_control->get_rate_yaw_pid().get_pid_info()); } #endif /* check if we have a good position estimate */ bool AutoTune::position_ok() { return copter.position_ok(); } /* initialise autotune mode */ bool ModeAutoTune::init(bool ignore_checks) { return autotune.init(); } void ModeAutoTune::run() { autotune.run(); } void ModeAutoTune::save_tuning_gains() { autotune.save_tuning_gains(); } void ModeAutoTune::exit() { autotune.stop(); } void ModeAutoTune::reset() { autotune.reset(); } #endif // AUTOTUNE_ENABLED == ENABLED