#include "Tracker.h" /** update_vehicle_position_estimate - updates estimate of vehicle positions should be called at 50hz */ void Tracker::update_vehicle_pos_estimate() { // calculate time since last actual position update float dt = (AP_HAL::micros() - vehicle.last_update_us) * 1.0e-6f; // if less than 5 seconds since last position update estimate the position if (dt < TRACKING_TIMEOUT_SEC) { // project the vehicle position to take account of lost radio packets vehicle.location_estimate = vehicle.location; float north_offset = vehicle.vel.x * dt; float east_offset = vehicle.vel.y * dt; vehicle.location_estimate.offset(north_offset, east_offset); vehicle.location_estimate.alt += vehicle.vel.z * 100.0f * dt; // set valid_location flag vehicle.location_valid = true; } else { // vehicle has been lost, set lost flag vehicle.location_valid = false; } } /** update_tracker_position - updates antenna tracker position from GPS location should be called at 50hz */ void Tracker::update_tracker_position() { Location temp_loc; // REVISIT: what if we lose lock during a mission and the antenna is moving? if (ahrs.get_position(temp_loc)) { stationary = false; current_loc = temp_loc; } } /** update_bearing_and_distance - updates bearing and distance to the vehicle should be called at 50hz */ void Tracker::update_bearing_and_distance() { // exit immediately if we do not have a valid vehicle position if (!vehicle.location_valid) { return; } // calculate bearing to vehicle // To-Do: remove need for check of control_mode if (control_mode != SCAN && !nav_status.manual_control_yaw) { nav_status.bearing = current_loc.get_bearing_to(vehicle.location_estimate) * 0.01f; } // calculate distance to vehicle nav_status.distance = current_loc.get_distance(vehicle.location_estimate); // calculate altitude difference to vehicle using gps if (g.alt_source == ALT_SOURCE_GPS){ nav_status.alt_difference_gps = (vehicle.location_estimate.alt - current_loc.alt) / 100.0f; } else { // g.alt_source == ALT_SOURCE_GPS_VEH_ONLY nav_status.alt_difference_gps = vehicle.relative_alt / 100.0f; } // calculate pitch to vehicle // To-Do: remove need for check of control_mode if (control_mode != SCAN && !nav_status.manual_control_pitch) { if (g.alt_source == ALT_SOURCE_BARO) { nav_status.pitch = degrees(atan2f(nav_status.alt_difference_baro, nav_status.distance)); } else { nav_status.pitch = degrees(atan2f(nav_status.alt_difference_gps, nav_status.distance)); } } } /** main antenna tracking code, called at 50Hz */ void Tracker::update_tracking(void) { // update vehicle position estimate update_vehicle_pos_estimate(); // update antenna tracker position from GPS update_tracker_position(); // update bearing and distance to vehicle update_bearing_and_distance(); // do not perform any servo updates until startup delay has passed if (g.startup_delay > 0 && AP_HAL::millis() - start_time_ms < g.startup_delay*1000) { return; } // do not perform updates if safety switch is disarmed (i.e. servos can't be moved) if (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) { return; } // do not move if we are not armed: if (!hal.util->get_soft_armed()) { return; } switch (control_mode) { case AUTO: if (vehicle.location_valid) { update_auto(); } else if (tracker.target_set) { update_scan(); } break; case MANUAL: update_manual(); break; case SCAN: update_scan(); break; case SERVO_TEST: case STOP: case INITIALISING: break; } } /** handle an updated position from the aircraft */ void Tracker::tracking_update_position(const mavlink_global_position_int_t &msg) { vehicle.location.lat = msg.lat; vehicle.location.lng = msg.lon; vehicle.location.alt = msg.alt/10; vehicle.relative_alt = msg.relative_alt/10; vehicle.vel = Vector3f(msg.vx/100.0f, msg.vy/100.0f, msg.vz/100.0f); vehicle.last_update_us = AP_HAL::micros(); vehicle.last_update_ms = AP_HAL::millis(); // log vehicle as GPS2 if (should_log(MASK_LOG_GPS)) { Log_Write_Vehicle_Pos(vehicle.location.lat, vehicle.location.lng, vehicle.location.alt, vehicle.vel); } } /** handle an updated pressure reading from the aircraft */ void Tracker::tracking_update_pressure(const mavlink_scaled_pressure_t &msg) { float local_pressure = barometer.get_pressure(); float aircraft_pressure = msg.press_abs*100.0f; // calculate altitude difference based on difference in barometric pressure float alt_diff = barometer.get_altitude_difference(local_pressure, aircraft_pressure); if (!isnan(alt_diff) && !isinf(alt_diff)) { nav_status.alt_difference_baro = alt_diff + nav_status.altitude_offset; if (nav_status.need_altitude_calibration) { // we have done a baro calibration - zero the altitude // difference to the aircraft nav_status.altitude_offset = -alt_diff; nav_status.alt_difference_baro = 0; nav_status.need_altitude_calibration = false; } } // log vehicle baro data Log_Write_Vehicle_Baro(aircraft_pressure, alt_diff); } /** handle a manual control message by using the data to command yaw and pitch */ void Tracker::tracking_manual_control(const mavlink_manual_control_t &msg) { nav_status.bearing = msg.x; nav_status.pitch = msg.y; nav_status.distance = 0.0; nav_status.manual_control_yaw = (msg.x != 0x7FFF); nav_status.manual_control_pitch = (msg.y != 0x7FFF); // z, r and buttons are not used } /** update_armed_disarmed - set armed LED if we have received a position update within the last 5 seconds */ void Tracker::update_armed_disarmed() { if (vehicle.last_update_ms != 0 && (AP_HAL::millis() - vehicle.last_update_ms) < TRACKING_TIMEOUT_MS) { AP_Notify::flags.armed = true; } else { AP_Notify::flags.armed = false; } }