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added base class for data storage
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/****************************************************************************
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*
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* Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name ECL nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file estimator_base.h
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* Definition of base class for attitude estimators
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*
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* @author Roman Bast <bastroman@gmail.com>
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*
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*/
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#include <stdint.h>
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#include <matrix/matrix/math.hpp>
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#include <lib/geo/geo.h>
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#include "RingBuffer.h"
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struct gps_message {
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uint64_t time_usec;
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int32_t lat; // Latitude in 1E-7 degrees
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int32_t lon; // Longitude in 1E-7 degrees
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int32_t alt; // Altitude in 1E-3 meters (millimeters) above MSL
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uint8_t fix_type; // 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: RTCM code differential, 5: Real-Time
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float eph; // GPS HDOP horizontal dilution of position in m
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float epv; // GPS VDOP horizontal dilution of position in m
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uint64_t time_usec_vel; // Timestamp for velocity informations
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float vel_m_s; // GPS ground speed (m/s)
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float vel_ned[3]; // GPS ground speed NED
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bool vel_ned_valid; // GPS ground speed is valid
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};
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class EstimatorBase
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{
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public:
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EstimatorBase();
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~EstimatorBase();
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// set delta angle imu data
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void setIMUData(uint64_t time_usec, uint64_t delta_ang_dt, uint64_t delta_vel_dt, float *delta_ang, float *delta_vel);
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// set magnetometer data
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void setMagData(uint64_t time_usec, float *data);
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// set gps data
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void setGpsData(uint64_t time_usec, struct gps_message *gps);
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// set baro data
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void setBaroData(uint64_t time_usec, float *data);
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// set airspeed data
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void setAirspeedData(uint64_t time_usec, float *data);
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// set range data
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void setRangeData(uint64_t time_usec, float *data);
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// set optical flow data
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void setOpticalFlowData(uint64_t time_usec, float *data);
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protected:
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typedef matrix::Vector<float, 2> Vector2f;
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typedef matrix::Vector<float, 3> Vector3f;
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typedef matrix::Quaternion<float> Quaternion;
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typedef matrix::Matrix<float, 3, 3> Matrix3f;
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struct stateSample {
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Vector3f ang_error;
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Vector3f vel;
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Vector3f pos;
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Vector3f gyro_bias;
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Vector3f gyro_scale;
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float accel_z_bias;
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Vector3f mag_I;
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Vector3f mag_B;
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Vector2f wind_vel;
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Quaternion quat_nominal;
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} _state;
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struct outputSample {
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Quaternion quat_nominal;
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Vector3f vel;
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Vector3f pos;
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};
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struct imuSample {
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Vector3f delta_ang;
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Vector3f delta_vel;
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float delta_ang_dt;
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float delta_vel_dt;
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uint32_t time_us;
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};
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struct gpsSample {
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Vector2f pos;
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float hgt;
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Vector3f vel;
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uint32_t time_us;
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};
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struct magSample {
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Vector3f mag;
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uint32_t time_us;
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};
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struct baroSample {
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float hgt;
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uint32_t time_us;
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};
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struct rangeSample {
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float rng;
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uint32_t time_us;
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};
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struct airspeedSample {
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float airspeed;
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uint32_t time_us;
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};
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struct flowSample {
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Vector2f flowRadXY;
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Vector2f flowRadXYcomp;
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uint32_t time_us;
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};
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struct {
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uint32_t mag_delay_ms;
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uint32_t baro_delay_ms;
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uint32_t gps_delay_ms;
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uint32_t airspeed_delay_ms;
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float requiredEph;
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float requiredEpv;
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} _params;
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static const uint8_t OBS_BUFFER_LENGTH = 5;
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static const uint8_t IMU_BUFFER_LENGTH = 25;
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static const unsigned FILTER_UPDATE_PERRIOD_MS = 10;
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float _dt_imu_avg;
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uint32_t _imu_time_last;
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imuSample _imu_sample_delayed;
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imuSample _imu_down_sampled;
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Quaternion
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_q_down_sampled;
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magSample _mag_sample_delayed;
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baroSample _baro_sample_delayed;
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gpsSample _gps_sample_delayed;
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rangeSample _range_sample_delayed;
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airspeedSample _airspeed_sample_delayed;
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flowSample _flow_sample_delayed;
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struct map_projection_reference_s _posRef;
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float _gps_alt_ref;
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uint32_t _imu_ticks;
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bool _imu_updated;
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bool _start_predict_enabled;
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bool _initialised;
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bool _gps_initialised;
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bool _gps_speed_valid;
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RingBuffer<imuSample> _imu_buffer;
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RingBuffer<gpsSample> _gps_buffer;
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RingBuffer<magSample> _mag_buffer;
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RingBuffer<baroSample> _baro_buffer;
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RingBuffer<rangeSample> _range_buffer;
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RingBuffer<airspeedSample> _airspeed_buffer;
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RingBuffer<flowSample> _flow_buffer;
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RingBuffer<outputSample> _output_buffer;
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uint64_t _time_last_imu;
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uint64_t _time_last_gps;
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uint64_t _time_last_mag;
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uint64_t _time_last_baro;
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uint64_t _time_last_range;
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uint64_t _time_last_airspeed;
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void initialiseVariables(uint64_t timestamp);
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void initialiseGPS(struct gps_message *gps);
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bool gps_is_good(struct gps_message *gps);
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public:
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void printIMU(struct imuSample *data);
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void printStoredIMU();
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void printQuaternion(Quaternion &q);
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void print_imu_avg_time();
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void printMag(struct magSample *data);
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void printStoredMag();
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void printBaro(struct baroSample *data);
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void printStoredBaro();
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void printGps(struct gpsSample *data);
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void printStoredGps();
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};
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