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Diffstat (limited to 'src/modules/att_pos_estimator_ekf/KalmanNav.hpp')
| -rw-r--r-- | src/modules/att_pos_estimator_ekf/KalmanNav.hpp | 180 |
1 files changed, 180 insertions, 0 deletions
diff --git a/src/modules/att_pos_estimator_ekf/KalmanNav.hpp b/src/modules/att_pos_estimator_ekf/KalmanNav.hpp new file mode 100644 index 000000000..c2bf18115 --- /dev/null +++ b/src/modules/att_pos_estimator_ekf/KalmanNav.hpp @@ -0,0 +1,180 @@ +/**************************************************************************** + * + * Copyright (C) 2012 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 KalmanNav.hpp + * + * kalman filter navigation code + */ + +#pragma once + +//#define MATRIX_ASSERT +//#define VECTOR_ASSERT + +#include <nuttx/config.h> + +#include <mathlib/mathlib.h> +#include <controllib/blocks.hpp> +#include <controllib/block/BlockParam.hpp> +#include <controllib/block/UOrbSubscription.hpp> +#include <controllib/block/UOrbPublication.hpp> + +#include <uORB/topics/vehicle_attitude.h> +#include <uORB/topics/vehicle_global_position.h> +#include <uORB/topics/sensor_combined.h> +#include <uORB/topics/vehicle_gps_position.h> +#include <uORB/topics/parameter_update.h> + +#include <drivers/drv_hrt.h> +#include <poll.h> +#include <unistd.h> + +/** + * Kalman filter navigation class + * http://en.wikipedia.org/wiki/Extended_Kalman_filter + * Discrete-time extended Kalman filter + */ +class KalmanNav : public control::SuperBlock +{ +public: + /** + * Constructor + */ + KalmanNav(SuperBlock *parent, const char *name); + + /** + * Deconstuctor + */ + + virtual ~KalmanNav() {}; + /** + * The main callback function for the class + */ + void update(); + + + /** + * Publication update + */ + virtual void updatePublications(); + + /** + * State prediction + * Continuous, non-linear + */ + int predictState(float dt); + + /** + * State covariance prediction + * Continuous, linear + */ + int predictStateCovariance(float dt); + + /** + * Attitude correction + */ + int correctAtt(); + + /** + * Position correction + */ + int correctPos(); + + /** + * Overloaded update parameters + */ + virtual void updateParams(); +protected: + // kalman filter + math::Matrix F; /**< Jacobian(f,x), where dx/dt = f(x,u) */ + math::Matrix G; /**< noise shaping matrix for gyro/accel */ + math::Matrix P; /**< state covariance matrix */ + math::Matrix P0; /**< initial state covariance matrix */ + math::Matrix V; /**< gyro/ accel noise matrix */ + math::Matrix HAtt; /**< attitude measurement matrix */ + math::Matrix RAtt; /**< attitude measurement noise matrix */ + math::Matrix HPos; /**< position measurement jacobian matrix */ + math::Matrix RPos; /**< position measurement noise matrix */ + // attitude + math::Dcm C_nb; /**< direction cosine matrix from body to nav frame */ + math::Quaternion q; /**< quaternion from body to nav frame */ + // subscriptions + control::UOrbSubscription<sensor_combined_s> _sensors; /**< sensors sub. */ + control::UOrbSubscription<vehicle_gps_position_s> _gps; /**< gps sub. */ + control::UOrbSubscription<parameter_update_s> _param_update; /**< parameter update sub. */ + // publications + control::UOrbPublication<vehicle_global_position_s> _pos; /**< position pub. */ + control::UOrbPublication<vehicle_attitude_s> _att; /**< attitude pub. */ + // time stamps + uint64_t _pubTimeStamp; /**< output data publication time stamp */ + uint64_t _predictTimeStamp; /**< prediction time stamp */ + uint64_t _attTimeStamp; /**< attitude correction time stamp */ + uint64_t _outTimeStamp; /**< output time stamp */ + // frame count + uint16_t _navFrames; /**< navigation frames completed in output cycle */ + // miss counts + uint16_t _miss; /**< number of times fast prediction loop missed */ + // accelerations + float fN, fE, fD; /**< navigation frame acceleration */ + // states + enum {PHI = 0, THETA, PSI, VN, VE, VD, LAT, LON, ALT}; /**< state enumeration */ + float phi, theta, psi; /**< 3-2-1 euler angles */ + float vN, vE, vD; /**< navigation velocity, m/s */ + double lat, lon, alt; /**< lat, lon, alt, radians */ + // parameters + control::BlockParam<float> _vGyro; /**< gyro process noise */ + control::BlockParam<float> _vAccel; /**< accelerometer process noise */ + control::BlockParam<float> _rMag; /**< magnetometer measurement noise */ + control::BlockParam<float> _rGpsVel; /**< gps velocity measurement noise */ + control::BlockParam<float> _rGpsPos; /**< gps position measurement noise */ + control::BlockParam<float> _rGpsAlt; /**< gps altitude measurement noise */ + control::BlockParam<float> _rPressAlt; /**< press altitude measurement noise */ + control::BlockParam<float> _rAccel; /**< accelerometer measurement noise */ + control::BlockParam<float> _magDip; /**< magnetic inclination with level */ + control::BlockParam<float> _magDec; /**< magnetic declination, clockwise rotation */ + control::BlockParam<float> _g; /**< gravitational constant */ + control::BlockParam<float> _faultPos; /**< fault detection threshold for position */ + control::BlockParam<float> _faultAtt; /**< fault detection threshold for attitude */ + // status + bool _attitudeInitialized; + bool _positionInitialized; + uint16_t _attitudeInitCounter; + // accessors + int32_t getLatDegE7() { return int32_t(lat * 1.0e7 * M_RAD_TO_DEG); } + void setLatDegE7(int32_t val) { lat = val / 1.0e7 / M_RAD_TO_DEG; } + int32_t getLonDegE7() { return int32_t(lon * 1.0e7 * M_RAD_TO_DEG); } + void setLonDegE7(int32_t val) { lon = val / 1.0e7 / M_RAD_TO_DEG; } + int32_t getAltE3() { return int32_t(alt * 1.0e3); } + void setAltE3(int32_t val) { alt = double(val) / 1.0e3; } +}; |