px4-firmware/EKF/ekf.h

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/****************************************************************************
*
* Copyright (c) 2015 Estimation and Control Library (ECL). All rights reserved.
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*
* Redistribution and use in source and binary forms, with or without
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*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
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* distribution.
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* used to endorse or promote products derived from this software
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/**
* @file ekf.h
* Class for core functions for ekf attitude and position estimator.
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*
* @author Roman Bast <bapstroman@gmail.com>
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*
*/
#include "estimator_base.h"
#define sq(_arg) powf(_arg, 2.0f)
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class Ekf : public EstimatorBase
{
public:
Ekf();
~Ekf();
bool update();
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private:
static const uint8_t _k_num_states = 24;
static constexpr float _k_earth_rate = 0.000072921f;
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bool _filter_initialised;
bool _earth_rate_initialised;
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bool _fuse_height; // true if there is new baro data
bool _fuse_pos; // true if there is new position data from gps
bool _fuse_vel; // true if there is new velocity data from gps
Vector3f _earth_rate_NED;
matrix::Dcm<float> _R_prev;
float P[_k_num_states][_k_num_states]; // state covariance matrix
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bool initialiseFilter(void);
void initialiseCovariance();
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void predictState();
void predictCovariance();
void fuseMag(uint8_t index);
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void fuseHeading();
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void fuseAirspeed();
void fuseRange();
void fuseVelPosHeight();
void resetVelocity();
void resetPosition();
void makeCovSymetrical();
void limitCov();
void printCovToFile(char const *filename);
void assertCovNiceness();
void makeSymmetrical();
void constrainStates();
void fuse(float *K, float innovation);
void printStates();
void calcEarthRateNED(Vector3f &omega, double lat_rad) const;
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};