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100 lines
3.3 KiB
C
100 lines
3.3 KiB
C
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup StateSetimation Module
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* @{
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*
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* @file stateestimation.h
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2011.
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* @brief Acquires sensor data and fuses it into attitude estimate for CC
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*
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* @see The GNU Public License (GPL) Version 3
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*
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*****************************************************************************/
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/*
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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#ifndef STATEESTIMATION_H
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#define STATEESTIMATION_H
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#include <openpilot.h>
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// Enumeration for filter result
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typedef enum {
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FILTERRESULT_UNINITIALISED = -1,
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FILTERRESULT_OK = 0,
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FILTERRESULT_WARNING = 1,
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FILTERRESULT_CRITICAL = 2,
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FILTERRESULT_ERROR = 3,
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} filterResult;
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typedef enum {
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SENSORUPDATES_gyro = 1 << 0,
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SENSORUPDATES_accel = 1 << 1,
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SENSORUPDATES_mag = 1 << 2,
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SENSORUPDATES_auxMag = 1 << 2,
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SENSORUPDATES_boardMag = 1 << 2,
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SENSORUPDATES_attitude = 1 << 3,
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SENSORUPDATES_pos = 1 << 4,
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SENSORUPDATES_vel = 1 << 5,
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SENSORUPDATES_airspeed = 1 << 6,
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SENSORUPDATES_baro = 1 << 7,
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SENSORUPDATES_lla = 1 << 8,
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} sensorUpdates;
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#define MAGSTATUS_ONBOARD 1
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#define MAGSTATUS_AUX 2
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#define MAGSTATUS_INVALID 0
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typedef struct {
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float gyro[3];
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float accel[3];
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float mag[3];
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float attitude[4];
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float pos[3];
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float vel[3];
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float airspeed[2];
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float baro[1];
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float auxMag[3];
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uint8_t magStatus;
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float boardMag[3];
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sensorUpdates updated;
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} stateEstimation;
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typedef struct stateFilterStruct {
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int32_t (*init)(struct stateFilterStruct *self);
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filterResult (*filter)(struct stateFilterStruct *self, stateEstimation *state);
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void *localdata;
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} stateFilter;
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int32_t filterMagInitialize(stateFilter *handle);
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int32_t filterBaroiInitialize(stateFilter *handle);
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int32_t filterBaroInitialize(stateFilter *handle);
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int32_t filterAltitudeInitialize(stateFilter *handle);
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int32_t filterAirInitialize(stateFilter *handle);
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int32_t filterStationaryInitialize(stateFilter *handle);
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int32_t filterLLAInitialize(stateFilter *handle);
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int32_t filterCFInitialize(stateFilter *handle);
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int32_t filterCFMInitialize(stateFilter *handle);
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int32_t filterEKF13iInitialize(stateFilter *handle);
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int32_t filterEKF13Initialize(stateFilter *handle);
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int32_t filterEKF16iInitialize(stateFilter *handle);
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int32_t filterEKF16Initialize(stateFilter *handle);
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#endif // STATEESTIMATION_H
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