/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #if FRAME_CONFIG == HELI_FRAME /* * heli_control_stabilize.pde - init and run calls for stabilize flight mode for trad heli */ // stabilize_init - initialise stabilize controller static bool heli_stabilize_init(bool ignore_checks) { // set target altitude to zero for reporting // To-Do: make pos controller aware when it's active/inactive so it can always report the altitude error? pos_control.set_alt_target(0); return true; } // stabilize_run - runs the main stabilize controller // should be called at 100hz or more static void heli_stabilize_run() { int16_t target_roll, target_pitch; float target_yaw_rate; int16_t pilot_throttle_scaled; static bool init_targets_on_arming; // Tradheli should not reset roll, pitch, yaw targets when motors are not runup, because // we may be in autorotation flight. These should be reset only when transitioning from disarmed // to armed, because the pilot will have placed the helicopter down on the landing pad. This is so // that the servos move in a realistic fashion while disarmed for operational checks. // Also, unlike multicopters we do not set throttle (i.e. collective pitch) to zero so the swash servos move if(!motors.armed()) { init_targets_on_arming=true; attitude_control.set_yaw_target_to_current_heading(); } if(motors.armed() && init_targets_on_arming) { init_targets_on_arming=false; attitude_control.relax_bf_rate_controller(); } // apply SIMPLE mode transform to pilot inputs update_simple_mode(); // convert pilot input to lean angles // To-Do: convert get_pilot_desired_lean_angles to return angles as floats get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, target_roll, target_pitch); // get pilot's desired yaw rate target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in); // get pilot's desired throttle pilot_throttle_scaled = get_pilot_desired_collective(g.rc_3.control_in); // call attitude controller attitude_control.angle_ef_roll_pitch_rate_ef_yaw_smooth(target_roll, target_pitch, target_yaw_rate, get_smoothing_gain()); // output pilot's throttle - note that TradHeli does not used angle-boost attitude_control.set_throttle_out(pilot_throttle_scaled, false); } #endif //HELI_FRAME