/**************************************************************************** * * Copyright (c) 2014-2016 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 rtl_params.c * * Parameters for RTL * * @author Julian Oes */ /* * RTL parameters, accessible via MAVLink */ /** * RTL altitude * * Altitude to fly back in RTL in meters * * @unit m * @min 0 * @max 150 * @decimal 1 * @increment 0.5 * @group Return Mode */ PARAM_DEFINE_FLOAT(RTL_RETURN_ALT, 60); /** * Return mode loiter altitude * * Stay at this altitude above home position after RTL descending. * Land (i.e. slowly descend) from this altitude if autolanding allowed. * * @unit m * @min 2 * @max 100 * @decimal 1 * @increment 0.5 * @group Return Mode */ PARAM_DEFINE_FLOAT(RTL_DESCEND_ALT, 30); /** * Return mode delay * * Delay after descend before landing in Return mode. * If set to -1 the system will not land but loiter at RTL_DESCEND_ALT. * * @unit s * @min -1 * @max 300 * @decimal 1 * @increment 0.5 * @group Return Mode */ PARAM_DEFINE_FLOAT(RTL_LAND_DELAY, -1.0f); /** * Minimum distance to trigger rising to a safe altitude * * If the system is horizontally closer than this distance to home * it will land straight on home instead of raising to the return * altitude first. * * @unit m * @min 0.5 * @max 20 * @decimal 1 * @increment 0.5 * @group Return Mode */ PARAM_DEFINE_FLOAT(RTL_MIN_DIST, 5.0f); /** * Return type * * Fly straight to the home location or planned mission landing and land there or * use the planned mission to get to those points. * * @value 0 Return home via direct path * @value 1 Return to a planned mission landing, if available, via direct path, else return to home via direct path * @value 2 Return to a planned mission landing, if available, using the mission path, else return to home via the reverse mission path * @group Return Mode */ PARAM_DEFINE_INT32(RTL_TYPE, 0); /** * Half-angle of the RTL cone. * * Defines the half-angle of the cone which defines the vehicle RTL behavior. * * @unit degrees * @min 0 * @max 90 * @value 0 No cone, always climb to RTL_RETURN_ALT above home. * @value 25 25 degrees half cone angle. * @value 45 45 degrees half cone angle. * @value 65 65 degrees half cone angle. * @value 80 80 degrees half cone angle. * @value 90 Only climb to at least RTL_DESCEND_ALT above home. * @group Return Mode */ PARAM_DEFINE_INT32(RTL_CONE_ANG, 0);