/*! * \file rtklib_preceph.h * \brief precise ephemeris and clock functions * \authors * * 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. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions are * met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in the * documentation and/or other materials provided with the distribution. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR * A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT * HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, * SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT * LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, * DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY * THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT * (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE * OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. * * * References : * [1] S.Hilla, The Extended Standard Product 3 Orbit Format (SP3-c), * 12 February, 2007 * [2] J.Ray, W.Gurtner, RINEX Extensions to Handle Clock Information, * 27 August, 1998 * [3] D.D.McCarthy, IERS Technical Note 21, IERS Conventions 1996, July 1996 * [4] D.A.Vallado, Fundamentals of Astrodynamics and Applications 2nd ed, * Space Technology Library, 2004 * *----------------------------------------------------------------------------*/ #ifndef GNSS_SDR_RTKLIB_PRECEPH_H_ #define GNSS_SDR_RTKLIB_PRECEPH_H_ #include "rtklib.h" const int NMAX = 10; /* order of polynomial interpolation */ const double MAXDTE = 900.0; /* max time difference to ephem time (s) */ const double EXTERR_CLK = 1e-3; /* extrapolation error for clock (m/s) */ const double EXTERR_EPH = 5e-7; /* extrapolation error for ephem (m/s^2) */ int code2sys(char code); int readsp3h(FILE *fp, gtime_t *time, char *type, int *sats, double *bfact, char *tsys); int addpeph(nav_t *nav, peph_t *peph); void readsp3b(FILE *fp, char type, int *sats, int ns, const double *bfact, char *tsys, int index, int opt, nav_t *nav); int cmppeph(const void *p1, const void *p2); void combpeph(nav_t *nav, int opt); void readsp3(const char *file, nav_t *nav, int opt); int readsap(const char *file, gtime_t time, nav_t *nav); int readdcbf(const char *file, nav_t *nav, const sta_t *sta); int readdcb(const char *file, nav_t *nav, const sta_t *sta); int addfcb(nav_t *nav, gtime_t ts, gtime_t te, int sat, const double *bias, const double *std); int readfcbf(const char *file, nav_t *nav); int readdcb(const char *file, nav_t *nav, const sta_t *sta); int addfcb(nav_t *nav, gtime_t ts, gtime_t te, int sat, const double *bias, const double *std); int readfcbf(const char *file, nav_t *nav); int cmpfcb(const void *p1, const void *p2); int readfcb(const char *file, nav_t *nav); double interppol(const double *x, double *y, int n); int pephpos(gtime_t time, int sat, const nav_t *nav, double *rs, double *dts, double *vare, double *varc); int pephclk(gtime_t time, int sat, const nav_t *nav, double *dts, double *varc); void satantoff(gtime_t time, const double *rs, int sat, const nav_t *nav, double *dant); int peph2pos(gtime_t time, int sat, const nav_t *nav, int opt, double *rs, double *dts, double *var); #endif // GNSS_SDR_RTKLIB_PRECEPH_H_