MAV'RIC
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00001 /******************************************************************************* 00002 * Copyright (c) 2009-2016, MAV'RIC Development Team 00003 * All rights reserved. 00004 * 00005 * Redistribution and use in source and binary forms, with or without 00006 * modification, are permitted provided that the following conditions are met: 00007 * 00008 * 1. Redistributions of source code must retain the above copyright notice, 00009 * this list of conditions and the following disclaimer. 00010 * 00011 * 2. Redistributions in binary form must reproduce the above copyright notice, 00012 * this list of conditions and the following disclaimer in the documentation 00013 * and/or other materials provided with the distribution. 00014 * 00015 * 3. Neither the name of the copyright holder nor the names of its contributors 00016 * may be used to endorse or promote products derived from this software without 00017 * specific prior written permission. 00018 * 00019 * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" 00020 * AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE 00021 * IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE 00022 * ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR CONTRIBUTORS BE 00023 * LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR 00024 * CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF 00025 * SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS 00026 * INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN 00027 * CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) 00028 * ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE 00029 * POSSIBILITY OF SUCH DAMAGE. 00030 ******************************************************************************/ 00031 00032 /******************************************************************************* 00033 * \file attitude_controller_p2.h 00034 * 00035 * \author MAV'RIC Team 00036 * \author Julien Lecoeur 00037 * 00038 * \brief A simple quaternion based proportionnal squared controller for 00039 * attitude control. 00040 * 00041 * \details It takes as input the desired attitude, the estimated attitude and 00042 * the gyro rates. 00043 * The control scheme is the following: 00044 * - first the controller computes local roll pitch and yaw angular errors 00045 * ( \f$ qerror \f$ ) using quaternion formulation 00046 * - angular errors are multiplied by a proportional gain \f$ P_{q} \f$ 00047 * - feedback from the gyro is added to the output with gain \f$ P_{g} \f$ 00048 * 00049 * in short: 00050 * \f$ 00051 * output = (P_{q} . qerror) - (P_{g} . gyro) 00052 * \f$ 00053 * 00054 ******************************************************************************/ 00055 00056 00057 #ifndef ATTITUDE_CONTROLLER_P2_HPP_ 00058 #define ATTITUDE_CONTROLLER_P2_HPP_ 00059 00060 #include "control/attitude_error_estimator.hpp" 00061 #include "control/control_command.hpp" 00062 #include "sensing/ahrs.hpp" 00063 00064 00068 typedef struct 00069 { 00070 const AHRS* ahrs; 00071 const attitude_command_t* attitude_command; 00072 torque_command_t* torque_command; 00073 attitude_error_estimator_t attitude_error_estimator; 00074 float p_gain_angle[3]; 00075 float p_gain_rate[3]; 00076 } attitude_controller_p2_t; 00077 00078 00082 typedef struct 00083 { 00084 float p_gain_angle[3]; 00085 float p_gain_rate[3]; 00086 } attitude_controller_p2_conf_t; 00087 00088 00099 bool attitude_controller_p2_init(attitude_controller_p2_t* controller, const attitude_controller_p2_conf_t config, const attitude_command_t* attitude_command, torque_command_t* torque_command, const AHRS* ahrs); 00100 00101 00109 bool attitude_controller_p2_update(attitude_controller_p2_t* controller); 00110 00111 00112 #endif /* ATTITUDE_CONTROLLER_P2_HPP_ */