/**************************************************************************** * * Copyright (c) 2013-2015 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file FixedwingLandDetector.cpp * Land detection algorithm for fixedwings * * @author Johan Jansen */ #include "FixedwingLandDetector.h" #include #include FixedwingLandDetector::FixedwingLandDetector() : LandDetector(), _paramHandle(), _params(), _vehicleLocalPositionSub(-1), _vehicleLocalPosition({}), _airspeedSub(-1), _airspeed({}), _parameterSub(-1), _velocity_xy_filtered(0.0f), _velocity_z_filtered(0.0f), _airspeed_filtered(0.0f), _landDetectTrigger(0) { _paramHandle.maxVelocity = param_find("LNDFW_VEL_XY_MAX"); _paramHandle.maxClimbRate = param_find("LNDFW_VEL_Z_MAX"); _paramHandle.maxAirSpeed = param_find("LNDFW_AIRSPD_MAX"); } void FixedwingLandDetector::initialize() { // Subscribe to local position and airspeed data _vehicleLocalPositionSub = orb_subscribe(ORB_ID(vehicle_local_position)); _airspeedSub = orb_subscribe(ORB_ID(airspeed)); updateParameterCache(true); } void FixedwingLandDetector::updateSubscriptions() { orb_update(ORB_ID(vehicle_local_position), _vehicleLocalPositionSub, &_vehicleLocalPosition); orb_update(ORB_ID(airspeed), _airspeedSub, &_airspeed); } bool FixedwingLandDetector::update() { // First poll for new data from our subscriptions updateSubscriptions(); const uint64_t now = hrt_absolute_time(); bool landDetected = false; // TODO: reset filtered values on arming? _velocity_xy_filtered = 0.95f * _velocity_xy_filtered + 0.05f * sqrtf(_vehicleLocalPosition.vx * _vehicleLocalPosition.vx + _vehicleLocalPosition.vy * _vehicleLocalPosition.vy); _velocity_z_filtered = 0.95f * _velocity_z_filtered + 0.05f * fabsf(_vehicleLocalPosition.vz); _airspeed_filtered = 0.95f * _airspeed_filtered + 0.05f * _airspeed.true_airspeed_m_s; // crude land detector for fixedwing if (_velocity_xy_filtered < _params.maxVelocity && _velocity_z_filtered < _params.maxClimbRate && _airspeed_filtered < _params.maxAirSpeed) { // these conditions need to be stable for a period of time before we trust them if (now > _landDetectTrigger) { landDetected = true; } } else { // reset land detect trigger _landDetectTrigger = now + LAND_DETECTOR_TRIGGER_TIME; } return landDetected; } void FixedwingLandDetector::updateParameterCache(const bool force) { bool updated; parameter_update_s paramUpdate; orb_check(_parameterSub, &updated); if (updated) { orb_copy(ORB_ID(parameter_update), _parameterSub, ¶mUpdate); } if (updated || force) { param_get(_paramHandle.maxVelocity, &_params.maxVelocity); param_get(_paramHandle.maxClimbRate, &_params.maxClimbRate); param_get(_paramHandle.maxAirSpeed, &_params.maxAirSpeed); } }