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LibrePilot/flight/libraries/inc/insgps.h

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/**
******************************************************************************
* @addtogroup AHRS
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* @{
* @addtogroup INSGPS
* @{
* @brief INSGPS is a joint attitude and position estimation EKF
*
* @file insgps.h
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
* @brief Include file of the INSGPS exposed functionality.
*
* @see The GNU Public License (GPL) Version 3
*
*****************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#ifndef INSGPS_H_
#define INSGPS_H_
#include "stdint.h"
/**
* @addtogroup Constants
* @{
*/
#define POS_SENSORS 0x007
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#define HORIZ_POS_SENSORS 0x003
#define VER_POS_SENSORS 0x004
#define HORIZ_SENSORS 0x018
#define VERT_SENSORS 0x020
#define MAG_SENSORS 0x1C0
#define BARO_SENSOR 0x200
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#define FULL_SENSORS 0x3FF
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/**
* @}
*/
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// Exposed Function Prototypes
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void INSGPSInit();
void INSStatePrediction(float gyro_data[3], float accel_data[3], float dT);
void INSCovariancePrediction(float dT);
void INSCorrection(float mag_data[3], float Pos[3], float Vel[3], float BaroAlt, uint16_t SensorsUsed);
void INSResetP(float PDiag[13]);
void INSGetP(float PDiag[13]);
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void INSSetState(float pos[3], float vel[3], float q[4], float gyro_bias[3], float accel_bias[3]);
void INSSetPosVelVar(float PosVar[3], float VelVar[3]);
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void INSSetGyroBias(float gyro_bias[3]);
void INSSetAccelVar(float accel_var[3]);
void INSSetGyroVar(float gyro_var[3]);
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void INSSetGyroBiasVar(float gyro_bias_var[3]);
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void INSSetMagNorth(float B[3]);
void INSSetMagVar(float scaled_mag_var[3]);
void INSSetBaroVar(float baro_var);
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void INSPosVelReset(float pos[3], float vel[3]);
void MagCorrection(float mag_data[3]);
void MagVelBaroCorrection(float mag_data[3], float Vel[3], float BaroAlt);
void FullCorrection(float mag_data[3], float Pos[3], float Vel[3],
float BaroAlt);
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void GpsBaroCorrection(float Pos[3], float Vel[3], float BaroAlt);
void GpsMagCorrection(float mag_data[3], float Pos[3], float Vel[2]);
void VelBaroCorrection(float Vel[3], float BaroAlt);
uint16_t ins_get_num_states();
// Nav structure containing current solution
extern struct NavStruct {
float Pos[3]; // Position in meters and relative to a local NED frame
float Vel[3]; // Velocity in meters and in NED
float q[4]; // unit quaternion rotation relative to NED
float gyro_bias[3];
float accel_bias[3];
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} Nav;
/**
* @}
* @}
*/
#endif /* EKF_H_ */