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