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LibrePilot/flight/AHRS/inc/insgps.h
peabody124 ebcb272da6 AHRS: Add a separate parameter for velocity and position variance and remove
indoor from the name since it's used for both indoor and outdoor mode now.
Increased default value to 0.4 to better reflect the GPS accuracy.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2156 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-11-26 15:57:08 +00:00

90 lines
2.8 KiB
C

/**
******************************************************************************
* @addtogroup AHRS
* @{
* @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
#define HORIZ_SENSORS 0x018
#define VERT_SENSORS 0x020
#define MAG_SENSORS 0x1C0
#define BARO_SENSOR 0x200
#define FULL_SENSORS 0x3FF
/**
* @}
*/
// Exposed Function Prototypes
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 INSSetState(float pos[3], float vel[3], float q[4], float gyro_bias[3]);
void INSSetPosVelVar(float PosVar, float VelVar);
void INSSetGyroBias(float gyro_bias[3]);
void INSSetAccelVar(float accel_var[3]);
void INSSetGyroVar(float gyro_var[3]);
void INSSetMagNorth(float B[3]);
void INSSetMagVar(float scaled_mag_var[3]);
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);
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);
// Nav structure containing current solution
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
} Nav;
/**
* @}
* @}
*/
#endif /* EKF_H_ */