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gnss-sdr/src/algorithms/libs/rtklib/rtklib_ephemeris.h
2020-07-28 16:57:15 +02:00

76 lines
2.9 KiB
C

/*!
* \file rtklib_ephemeris.h
* \brief satellite ephemeris and clock functions
* \authors <ul>
* <li> 2007-2013, T. Takasu
* <li> 2017, Javier Arribas
* <li> 2017, Carles Fernandez
* </ul>
*
* This is a derived work from RTKLIB http://www.rtklib.com/
* The original source code at https://github.com/tomojitakasu/RTKLIB is
* released under the BSD 2-clause license with an additional exclusive clause
* that does not apply here. This additional clause is reproduced below:
*
* " The software package includes some companion executive binaries or shared
* libraries necessary to execute APs on Windows. These licenses succeed to the
* original ones of these software. "
*
* Neither the executive binaries nor the shared libraries are required by, used
* or included in GNSS-SDR.
*
* -----------------------------------------------------------------------------
* Copyright (C) 2007-2013, T. Takasu
* Copyright (C) 2017, Javier Arribas
* Copyright (C) 2017, Carles Fernandez
* All rights reserved.
*
* SPDX-License-Identifier: BSD-2-Clause
*
* -----------------------------------------------------------------------------
*/
#ifndef GNSS_SDR_RTKLIB_EPHEMERIS_H
#define GNSS_SDR_RTKLIB_EPHEMERIS_H
#include "rtklib.h"
double var_uraeph(int ura);
double var_urassr(int ura);
void alm2pos(gtime_t time, const alm_t *alm, double *rs, double *dts);
double eph2clk(gtime_t time, const eph_t *eph);
void eph2pos(gtime_t time, const eph_t *eph, double *rs, double *dts,
double *var);
void deq(const double *x, double *xdot, const double *acc);
void glorbit(double t, double *x, const double *acc);
double geph2clk(gtime_t time, const geph_t *geph);
void geph2pos(gtime_t time, const geph_t *geph, double *rs, double *dts,
double *var);
double seph2clk(gtime_t time, const seph_t *seph);
void seph2pos(gtime_t time, const seph_t *seph, double *rs, double *dts,
double *var);
eph_t *seleph(gtime_t time, int sat, int iode, const nav_t *nav);
geph_t *selgeph(gtime_t time, int sat, int iode, const nav_t *nav);
seph_t *selseph(gtime_t time, int sat, const nav_t *nav);
int ephclk(gtime_t time, gtime_t teph, int sat, const nav_t *nav,
double *dts);
// satellite position and clock by broadcast ephemeris
int ephpos(gtime_t time, gtime_t teph, int sat, const nav_t *nav,
int iode, double *rs, double *dts, double *var, int *svh);
int satpos_sbas(gtime_t time, gtime_t teph, int sat, const nav_t *nav,
double *rs, double *dts, double *var, int *svh);
int satpos_ssr(gtime_t time, gtime_t teph, int sat, const nav_t *nav,
int opt, double *rs, double *dts, double *var, int *svh);
int satpos(gtime_t time, gtime_t teph, int sat, int ephopt,
const nav_t *nav, double *rs, double *dts, double *var,
int *svh);
void satposs(gtime_t teph, const obsd_t *obs, int n, const nav_t *nav,
int ephopt, double *rs, double *dts, double *var, int *svh);
#endif // GNSS_SDR_RTKLIB_EPHEMERIS_H