/**************************************************************************** * * Copyright (c) 2013, 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 launchdetection_params.c * * Parameters for launchdetection * * @author Thomas Gubler */ #include #include /* * Catapult launch detection parameters, accessible via MAVLink * */ /** * Enable launch detection. * * @min 0 * @max 1 * @group Launch detection */ PARAM_DEFINE_INT32(LAUN_ALL_ON, 0); /** * Catapult accelerometer theshold. * * LAUN_CAT_A * LAUN_CAT_T serves as threshold to trigger launch detection. * * @min 0 * @group Launch detection */ PARAM_DEFINE_FLOAT(LAUN_CAT_A, 30.0f); /** * Catapult time theshold. * * LAUN_CAT_A * LAUN_CAT_T serves as threshold to trigger launch detection. * * @min 0 * @group Launch detection */ PARAM_DEFINE_FLOAT(LAUN_CAT_T, 0.05f); /** * Motor delay * * Delay between starting attitude control and powering up the throttle (giving throttle control to the controller) * Before this timespan is up the throttle will be set to LAUN_THR_PRE, set to 0 to deactivate * * @unit seconds * @min 0 * @group Launch detection */ PARAM_DEFINE_FLOAT(LAUN_CAT_MDEL, 0.0f); /** * Maximum pitch before the throttle is powered up (during motor delay phase) * * This is an extra limit for the maximum pitch which is imposed in the phase before the throttle turns on. * This allows to limit the maximum pitch angle during a bungee launch (make the launch less steep). * * @unit deg * @min 0 * @max 45 * @group Launch detection */ PARAM_DEFINE_FLOAT(LAUN_CAT_PMAX, 30.0f); /** * Throttle setting while detecting launch. * * The throttle is set to this value while the system is waiting for the take-off. * * @min 0 * @max 1 * @group Launch detection */ PARAM_DEFINE_FLOAT(LAUN_THR_PRE, 0.0f);