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3afdc7e41c
config plugin updates. Has not been tested in flight yet although seems sensible so please be careful when using this code. git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3166 ebee16cc-31ac-478f-84a7-5cbb03baadba
80 lines
3.2 KiB
C
80 lines
3.2 KiB
C
/**
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******************************************************************************
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*
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* @file CoordinateConverions.h
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010.
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* @brief Header for Coordinate conversions library in CoordinateConversions.c
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* - all angles in deg
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* - distances in meters
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* - altitude above WGS-84 elipsoid
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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 COORDINATECONVERSIONS_H_
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#define COORDINATECONVERSIONS_H_
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// ****** convert Lat,Lon,Alt to ECEF ************
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void LLA2ECEF(double LLA[3], double ECEF[3]);
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// ****** convert ECEF to Lat,Lon,Alt (ITERATIVE!) *********
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uint16_t ECEF2LLA(double ECEF[3], double LLA[3]);
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void RneFromLLA(double LLA[3], float Rne[3][3]);
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// ****** find rotation matrix from rotation vector
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void Rv2Rot(float Rv[3], float R[3][3]);
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// ****** find roll, pitch, yaw from quaternion ********
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void Quaternion2RPY(const float q[4], float rpy[3]);
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// ****** find quaternion from roll, pitch, yaw ********
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void RPY2Quaternion(const float rpy[3], float q[4]);
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//** Find Rbe, that rotates a vector from earth fixed to body frame, from quaternion **
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void Quaternion2R(float q[4], float Rbe[3][3]);
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// ****** Express LLA in a local NED Base Frame ********
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void LLA2Base(double LLA[3], double BaseECEF[3], float Rne[3][3], float NED[3]);
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// ****** Express ECEF in a local NED Base Frame ********
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void ECEF2Base(double ECEF[3], double BaseECEF[3], float Rne[3][3], float NED[3]);
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// ****** convert Rotation Matrix to Quaternion ********
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// ****** if R converts from e to b, q is rotation from e to b ****
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void R2Quaternion(float R[3][3], float q[4]);
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// ****** Rotation Matrix from Two Vector Directions ********
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// ****** given two vector directions (v1 and v2) known in two frames (b and e) find Rbe ***
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// ****** solution is approximate if can't be exact ***
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uint8_t RotFrom2Vectors(const float v1b[3], const float v1e[3], const float v2b[3], const float v2e[3], float Rbe[3][3]);
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// ****** Vector Cross Product ********
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void CrossProduct(const float v1[3], const float v2[3], float result[3]);
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// ****** Vector Magnitude ********
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float VectorMagnitude(const float v[3]);
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void quat_inverse(float q[4]);
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void quat_copy(const float q[4], float qnew[4]);
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void quat_mult(const float q1[4], const float q2[4], float qout[4]);
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void rot_mult(float R[3][3], const float vec[3], float vec_out[3]);
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#endif // COORDINATECONVERSIONS_H_
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