/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* * control_ofloiter.pde - init and run calls for of_loiter (optical flow loiter) flight mode */ #if OPTFLOW == ENABLED // ofloiter_init - initialise ofloiter controller static bool ofloiter_init(bool ignore_checks) { if (g.optflow_enabled || ignore_checks) { // initialize vertical speed and acceleration pos_control.set_speed_z(-g.pilot_velocity_z_max, g.pilot_velocity_z_max); pos_control.set_accel_z(g.pilot_accel_z); // initialise altitude target to stopping point pos_control.set_target_to_stopping_point_z(); return true; }else{ return false; } } // ofloiter_run - runs the optical flow loiter controller // should be called at 100hz or more static void ofloiter_run() { int16_t target_roll, target_pitch; 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) { attitude_control.relax_bf_rate_controller(); attitude_control.set_yaw_target_to_current_heading(); attitude_control.set_throttle_out(0, false); pos_control.set_alt_target_to_current_alt(); reset_optflow_I(); return; } // process pilot inputs if (!failsafe.radio) { // apply SIMPLE mode transform to pilot inputs update_simple_mode(); // convert pilot input to lean angles 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 desired climb rate target_climb_rate = get_pilot_desired_climb_rate(g.rc_3.control_in); // check for pilot requested take-off if (ap.land_complete && target_climb_rate > 0) { // indicate we are taking off set_land_complete(false); // clear i term when we're taking off set_throttle_takeoff(); } } // when landed reset targets and output zero throttle if (ap.land_complete) { attitude_control.relax_bf_rate_controller(); attitude_control.set_yaw_target_to_current_heading(); // move throttle to between minimum and non-takeoff-throttle to keep us on the ground attitude_control.set_throttle_out(get_throttle_pre_takeoff(g.rc_3.control_in), false); pos_control.set_alt_target_to_current_alt(); reset_optflow_I(); }else{ // mix in user control with optical flow target_roll = get_of_roll(target_roll); target_pitch = get_of_pitch(target_pitch); // call attitude controller attitude_control.angle_ef_roll_pitch_rate_ef_yaw_smooth(target_roll, target_pitch, target_yaw_rate, get_smoothing_gain()); // run altitude controller if (sonar_alt_health >= SONAR_ALT_HEALTH_MAX) { // if sonar is ok, use surface tracking target_climb_rate = get_throttle_surface_tracking(target_climb_rate, pos_control.get_alt_target(), G_Dt); } // 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(); } } // calculate modified roll/pitch depending upon optical flow calculated position static int32_t get_of_roll(int32_t input_roll) { static float tot_x_cm = 0; // total distance from target static uint32_t last_of_roll_update = 0; int32_t new_roll = 0; int32_t p,i,d; // check if new optflow data available if( optflow.last_update != last_of_roll_update) { last_of_roll_update = optflow.last_update; // add new distance moved tot_x_cm += optflow.x_cm; // only stop roll if caller isn't modifying roll if( input_roll == 0 && current_loc.alt < 1500) { p = g.pid_optflow_roll.get_p(-tot_x_cm); i = g.pid_optflow_roll.get_i(-tot_x_cm,1.0f); // we could use the last update time to calculate the time change d = g.pid_optflow_roll.get_d(-tot_x_cm,1.0f); new_roll = p+i+d; }else{ g.pid_optflow_roll.reset_I(); tot_x_cm = 0; p = 0; // for logging i = 0; d = 0; } // limit amount of change and maximum angle of_roll = constrain_int32(new_roll, (of_roll-20), (of_roll+20)); } // limit max angle of_roll = constrain_int32(of_roll, -1000, 1000); return input_roll+of_roll; } static int32_t get_of_pitch(int32_t input_pitch) { static float tot_y_cm = 0; // total distance from target static uint32_t last_of_pitch_update = 0; int32_t new_pitch = 0; int32_t p,i,d; // check if new optflow data available if( optflow.last_update != last_of_pitch_update ) { last_of_pitch_update = optflow.last_update; // add new distance moved tot_y_cm += optflow.y_cm; // only stop roll if caller isn't modifying pitch if( input_pitch == 0 && current_loc.alt < 1500 ) { p = g.pid_optflow_pitch.get_p(tot_y_cm); i = g.pid_optflow_pitch.get_i(tot_y_cm, 1.0f); // we could use the last update time to calculate the time change d = g.pid_optflow_pitch.get_d(tot_y_cm, 1.0f); new_pitch = p + i + d; }else{ tot_y_cm = 0; g.pid_optflow_pitch.reset_I(); p = 0; // for logging i = 0; d = 0; } // limit amount of change of_pitch = constrain_int32(new_pitch, (of_pitch-20), (of_pitch+20)); } // limit max angle of_pitch = constrain_int32(of_pitch, -1000, 1000); return input_pitch+of_pitch; } // reset_optflow_I - reset optflow position hold I terms static void reset_optflow_I(void) { g.pid_optflow_roll.reset_I(); g.pid_optflow_pitch.reset_I(); of_roll = 0; of_pitch = 0; } #endif // OPTFLOW == ENABLED