/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #include "Copter.h" /* * control_brake.pde - init and run calls for brake flight mode */ // brake_init - initialise brake controller bool Copter::brake_init(bool ignore_checks) { if (position_ok() || optflow_position_ok() || ignore_checks) { // set desired acceleration to zero wp_nav.clear_pilot_desired_acceleration(); // set target to current position wp_nav.init_brake_target(BRAKE_MODE_DECEL_RATE); // initialize vertical speed and acceleration pos_control.set_speed_z(0, 0); pos_control.set_accel_z(BRAKE_MODE_DECEL_RATE); // initialise altitude target to stopping point pos_control.set_target_to_stopping_point_z(); return true; }else{ return false; } } // brake_run - runs the brake controller // should be called at 100hz or more void Copter::brake_run() { float target_yaw_rate = 0; float target_climb_rate = 0; // if not auto armed set throttle to zero and exit immediately if(!ap.auto_armed) { wp_nav.init_brake_target(BRAKE_MODE_DECEL_RATE); attitude_control.set_throttle_out_unstabilized(0,true,g.throttle_filt); pos_control.relax_alt_hold_controllers(get_throttle_pre_takeoff(0)-throttle_average); return; } // relax stop target if we might be landed if (ap.land_complete_maybe) { wp_nav.loiter_soften_for_landing(); } // if landed immediately disarm if (ap.land_complete) { init_disarm_motors(); } // run brake controller wp_nav.update_brake(ekfGndSpdLimit, ekfNavVelGainScaler); // call attitude controller attitude_control.angle_ef_roll_pitch_rate_ef_yaw(wp_nav.get_roll(), wp_nav.get_pitch(), target_yaw_rate); // body-frame rate controller is run directly from 100hz loop // update altitude target and call position controller pos_control.set_alt_target_from_climb_rate(target_climb_rate, G_Dt); pos_control.update_z_controller(); }