#include "Copter.h" /* autotune mode is a wrapper around the AC_AutoTune library */ #if AUTOTUNE_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(); // disarm when the landing detector says we've landed and spool state is ground idle if (copter.ap.land_complete && motors->get_spool_state() == AP_Motors::SpoolState::GROUND_IDLE) { copter.arming.disarm(AP_Arming::Method::LANDED); } // if not armed set throttle to zero and exit immediately if (copter.ap.land_complete) { copter.flightmode->make_safe_ground_handling(); return; } // 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::exit() { autotune.stop(); } #endif // AUTOTUNE_ENABLED