/**************************************************************************** * * Copyright (c) 2014 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 gpsfailure_params.c * * Parameters for GPSF navigation mode * * @author Thomas Gubler */ #include #include /* * GPS Failure Navigation Mode parameters, accessible via MAVLink */ /** * Loiter time * * The amount of time in seconds the system should do open loop loiter and wait for gps recovery * before it goes into flight termination. * * @unit seconds * @min 0.0 * @group GPSF */ PARAM_DEFINE_FLOAT(NAV_GPSF_LT, 30.0f); /** * Open loop loiter roll * * Roll in degrees during the open loop loiter * * @unit deg * @min 0.0 * @max 30.0 * @group GPSF */ PARAM_DEFINE_FLOAT(NAV_GPSF_R, 15.0f); /** * Open loop loiter pitch * * Pitch in degrees during the open loop loiter * * @unit deg * @min -30.0 * @max 30.0 * @group GPSF */ PARAM_DEFINE_FLOAT(NAV_GPSF_P, 0.0f); /** * Open loop loiter thrust * * Thrust value which is set during the open loop loiter * * @min 0.0 * @max 1.0 * @group GPSF */ PARAM_DEFINE_FLOAT(NAV_GPSF_TR, 0.7f);