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+#include "erfa.h"
+
+void eraApcs(double date1, double date2, double pv[2][3],
+ double ebpv[2][3], double ehp[3],
+ eraASTROM *astrom)
+/*
+** - - - - - - - -
+** e r a A p c s
+** - - - - - - - -
+**
+** For an observer whose geocentric position and velocity are known,
+** prepare star-independent astrometry parameters for transformations
+** between ICRS and GCRS. The Earth ephemeris is supplied by the
+** caller.
+**
+** The parameters produced by this function are required in the space
+** motion, parallax, light deflection and aberration parts of the
+** astrometric transformation chain.
+**
+** Given:
+** date1 double TDB as a 2-part...
+** date2 double ...Julian Date (Note 1)
+** pv double[2][3] observer's geocentric pos/vel (m, m/s)
+** ebpv double[2][3] Earth barycentric PV (au, au/day)
+** ehp double[3] Earth heliocentric P (au)
+**
+** Returned:
+** astrom eraASTROM* star-independent astrometry parameters:
+** pmt double PM time interval (SSB, Julian years)
+** eb double[3] SSB to observer (vector, au)
+** eh double[3] Sun to observer (unit vector)
+** em double distance from Sun to observer (au)
+** v double[3] barycentric observer velocity (vector, c)
+** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
+** bpn double[3][3] bias-precession-nutation matrix
+** along double unchanged
+** xpl double unchanged
+** ypl double unchanged
+** sphi double unchanged
+** cphi double unchanged
+** diurab double unchanged
+** eral double unchanged
+** refa double unchanged
+** refb double unchanged
+**
+** Notes:
+**
+** 1) The TDB date date1+date2 is a Julian Date, apportioned in any
+** convenient way between the two arguments. For example,
+** JD(TDB)=2450123.7 could be expressed in any of these ways, among
+** others:
+**
+** date1 date2
+**
+** 2450123.7 0.0 (JD method)
+** 2451545.0 -1421.3 (J2000 method)
+** 2400000.5 50123.2 (MJD method)
+** 2450123.5 0.2 (date & time method)
+**
+** The JD method is the most natural and convenient to use in cases
+** where the loss of several decimal digits of resolution is
+** acceptable. The J2000 method is best matched to the way the
+** argument is handled internally and will deliver the optimum
+** resolution. The MJD method and the date & time methods are both
+** good compromises between resolution and convenience. For most
+** applications of this function the choice will not be at all
+** critical.
+**
+** TT can be used instead of TDB without any significant impact on
+** accuracy.
+**
+** 2) All the vectors are with respect to BCRS axes.
+**
+** 3) Providing separate arguments for (i) the observer's geocentric
+** position and velocity and (ii) the Earth ephemeris is done for
+** convenience in the geocentric, terrestrial and Earth orbit cases.
+** For deep space applications it maybe more convenient to specify
+** zero geocentric position and velocity and to supply the
+** observer's position and velocity information directly instead of
+** with respect to the Earth. However, note the different units:
+** m and m/s for the geocentric vectors, au and au/day for the
+** heliocentric and barycentric vectors.
+**
+** 4) In cases where the caller does not wish to provide the Earth
+** ephemeris, the function eraApcs13 can be used instead of the
+** present function. This computes the Earth ephemeris using the
+** ERFA function eraEpv00.
+**
+** 5) This is one of several functions that inserts into the astrom
+** structure star-independent parameters needed for the chain of
+** astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed.
+**
+** The various functions support different classes of observer and
+** portions of the transformation chain:
+**
+** functions observer transformation
+**
+** eraApcg eraApcg13 geocentric ICRS <-> GCRS
+** eraApci eraApci13 terrestrial ICRS <-> CIRS
+** eraApco eraApco13 terrestrial ICRS <-> observed
+** eraApcs eraApcs13 space ICRS <-> GCRS
+** eraAper eraAper13 terrestrial update Earth rotation
+** eraApio eraApio13 terrestrial CIRS <-> observed
+**
+** Those with names ending in "13" use contemporary ERFA models to
+** compute the various ephemerides. The others accept ephemerides
+** supplied by the caller.
+**
+** The transformation from ICRS to GCRS covers space motion,
+** parallax, light deflection, and aberration. From GCRS to CIRS
+** comprises frame bias and precession-nutation. From CIRS to
+** observed takes account of Earth rotation, polar motion, diurnal
+** aberration and parallax (unless subsumed into the ICRS <-> GCRS
+** transformation), and atmospheric refraction.
+**
+** 6) The context structure astrom produced by this function is used by
+** eraAtciq* and eraAticq*.
+**
+** Called:
+** eraCp copy p-vector
+** eraPm modulus of p-vector
+** eraPn decompose p-vector into modulus and direction
+** eraIr initialize r-matrix to identity
+**
+** Copyright (C) 2013-2016, NumFOCUS Foundation.
+** Derived, with permission, from the SOFA library. See notes at end of file.
+*/
+{
+/* au/d to m/s */
+ const double AUDMS = ERFA_DAU/ERFA_DAYSEC;
+
+/* Light time for 1 AU (day) */
+ const double CR = ERFA_AULT/ERFA_DAYSEC;
+
+ int i;
+ double dp, dv, pb[3], vb[3], ph[3], v2, w;
+
+
+/* Time since reference epoch, years (for proper motion calculation). */
+ astrom->pmt = ( (date1 - ERFA_DJ00) + date2 ) / ERFA_DJY;
+
+/* Adjust Earth ephemeris to observer. */
+ for (i = 0; i < 3; i++) {
+ dp = pv[0][i] / ERFA_DAU;
+ dv = pv[1][i] / AUDMS;
+ pb[i] = ebpv[0][i] + dp;
+ vb[i] = ebpv[1][i] + dv;
+ ph[i] = ehp[i] + dp;
+ }
+
+/* Barycentric position of observer (au). */
+ eraCp(pb, astrom->eb);
+
+/* Heliocentric direction and distance (unit vector and au). */
+ eraPn(ph, &astrom->em, astrom->eh);
+
+/* Barycentric vel. in units of c, and reciprocal of Lorenz factor. */
+ v2 = 0.0;
+ for (i = 0; i < 3; i++) {
+ w = vb[i] * CR;
+ astrom->v[i] = w;
+ v2 += w*w;
+ }
+ astrom->bm1 = sqrt(1.0 - v2);
+
+/* Reset the NPB matrix. */
+ eraIr(astrom->bpn);
+
+/* Finished. */
+
+}
+/*----------------------------------------------------------------------
+**
+**
+** Copyright (C) 2013-2016, NumFOCUS Foundation.
+** All rights reserved.
+**
+** This library is derived, with permission, from the International
+** Astronomical Union's "Standards of Fundamental Astronomy" library,
+** available from http://www.iausofa.org.
+**
+** The ERFA version is intended to retain identical functionality to
+** the SOFA library, but made distinct through different function and
+** file names, as set out in the SOFA license conditions. The SOFA
+** original has a role as a reference standard for the IAU and IERS,
+** and consequently redistribution is permitted only in its unaltered
+** state. The ERFA version is not subject to this restriction and
+** therefore can be included in distributions which do not support the
+** concept of "read only" software.
+**
+** Although the intent is to replicate the SOFA API (other than
+** replacement of prefix names) and results (with the exception of
+** bugs; any that are discovered will be fixed), SOFA is not
+** responsible for any errors found in this version of the library.
+**
+** If you wish to acknowledge the SOFA heritage, please acknowledge
+** that you are using a library derived from SOFA, rather than SOFA
+** itself.
+**
+**
+** TERMS AND CONDITIONS
+**
+** 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.
+**
+** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
+** the International Astronomical Union nor the names of its
+** contributors may be used to endorse or promote products derived
+** from this software without specific prior written permission.
+**
+** 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.
+**
+*/