/**************************************************************************** * * 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 mc_att_control_params.h * Parameters for multicopter attitude controller. * * @author Tobias Naegeli * @author Lorenz Meier * @author Anton Babushkin * @author Thomas Gubler */ #pragma once #define PARAM_MC_ROLL_P_DEFAULT 6.0f #define PARAM_MC_ROLLRATE_P_DEFAULT 0.1f #define PARAM_MC_ROLLRATE_I_DEFAULT 0.0f #define PARAM_MC_ROLLRATE_D_DEFAULT 0.002f #define PARAM_MC_PITCH_P_DEFAULT 6.0f #define PARAM_MC_PITCHRATE_P_DEFAULT 0.1f #define PARAM_MC_PITCHRATE_I_DEFAULT 0.0f #define PARAM_MC_PITCHRATE_D_DEFAULT 0.002f #define PARAM_MC_YAW_P_DEFAULT 2.0f #define PARAM_MC_YAWRATE_P_DEFAULT 0.3f #define PARAM_MC_YAWRATE_I_DEFAULT 0.0f #define PARAM_MC_YAWRATE_D_DEFAULT 0.0f #define PARAM_MC_YAW_FF_DEFAULT 0.5f #define PARAM_MC_YAWRATE_MAX_DEFAULT 120.0f #define PARAM_MC_MAN_R_MAX_DEFAULT 35.0f #define PARAM_MC_MAN_P_MAX_DEFAULT 35.0f #define PARAM_MC_MAN_Y_MAX_DEFAULT 120.0f #define PARAM_MC_ACRO_R_MAX_DEFAULT 35.0f #define PARAM_MC_ACRO_P_MAX_DEFAULT 35.0f #define PARAM_MC_ACRO_Y_MAX_DEFAULT 120.0f