MAV'RIC
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00001 /*******************************************************************************
00002  * Copyright (c) 2009-2016, MAV'RIC Development Team
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00010  *
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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
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00018  *
00019  * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS"
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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_ */
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