/**************************************************************************** * * 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 vtol_att_control_params.c * Parameters for vtol attitude controller. * * @author Roman Bapst */ #include /** * VTOL number of engines * * @min 1.0 * @group VTOL Attitude Control */ PARAM_DEFINE_INT32(VT_MOT_COUNT,0); /** * Idle speed of VTOL when in multicopter mode * * @min 900 * @group VTOL Attitude Control */ PARAM_DEFINE_INT32(VT_IDLE_PWM_MC,900); /** * Minimum airspeed in multicopter mode * * This is the minimum speed of the air flowing over the control surfaces. * * @min 0.0 * @group VTOL Attitude Control */ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_MIN,2.0f); /** * Maximum airspeed in multicopter mode * * This is the maximum speed of the air flowing over the control surfaces. * * @min 0.0 * @group VTOL Attitude Control */ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_MAX,30.0f); /** * Trim airspeed when in multicopter mode * * This is the airflow over the control surfaces for which no airspeed scaling is applied in multicopter mode. * * @min 0.0 * @group VTOL Attitude Control */ PARAM_DEFINE_FLOAT(VT_MC_ARSPD_TRIM,10.0f); /** * Permanent stabilization in fw mode * * If set to one this parameter will cause permanent attitude stabilization in fw mode. * This parameter has been introduced for pure convenience sake. * * @min 0.0 * @max 1.0 * @group VTOL Attitude Control */ PARAM_DEFINE_INT32(VT_FW_PERM_STAB,0);