| line | stmt | bran | cond | sub | pod | time | code | 
| 1 |  |  |  |  |  |  | #include "erfa.h" | 
| 2 |  |  |  |  |  |  |  | 
| 3 | 0 |  |  |  |  |  | void eraApcg(double date1, double date2, | 
| 4 |  |  |  |  |  |  | double ebpv[2][3], double ehp[3], | 
| 5 |  |  |  |  |  |  | eraASTROM *astrom) | 
| 6 |  |  |  |  |  |  | /* | 
| 7 |  |  |  |  |  |  | **  - - - - - - - - | 
| 8 |  |  |  |  |  |  | **   e r a A p c g | 
| 9 |  |  |  |  |  |  | **  - - - - - - - - | 
| 10 |  |  |  |  |  |  | ** | 
| 11 |  |  |  |  |  |  | **  For a geocentric observer, prepare star-independent astrometry | 
| 12 |  |  |  |  |  |  | **  parameters for transformations between ICRS and GCRS coordinates. | 
| 13 |  |  |  |  |  |  | **  The Earth ephemeris is supplied by the caller. | 
| 14 |  |  |  |  |  |  | ** | 
| 15 |  |  |  |  |  |  | **  The parameters produced by this function are required in the | 
| 16 |  |  |  |  |  |  | **  parallax, light deflection and aberration parts of the astrometric | 
| 17 |  |  |  |  |  |  | **  transformation chain. | 
| 18 |  |  |  |  |  |  | ** | 
| 19 |  |  |  |  |  |  | **  Given: | 
| 20 |  |  |  |  |  |  | **     date1  double       TDB as a 2-part... | 
| 21 |  |  |  |  |  |  | **     date2  double       ...Julian Date (Note 1) | 
| 22 |  |  |  |  |  |  | **     ebpv   double[2][3] Earth barycentric pos/vel (au, au/day) | 
| 23 |  |  |  |  |  |  | **     ehp    double[3]    Earth heliocentric position (au) | 
| 24 |  |  |  |  |  |  | ** | 
| 25 |  |  |  |  |  |  | **  Returned: | 
| 26 |  |  |  |  |  |  | **     astrom eraASTROM*   star-independent astrometry parameters: | 
| 27 |  |  |  |  |  |  | **      pmt    double       PM time interval (SSB, Julian years) | 
| 28 |  |  |  |  |  |  | **      eb     double[3]    SSB to observer (vector, au) | 
| 29 |  |  |  |  |  |  | **      eh     double[3]    Sun to observer (unit vector) | 
| 30 |  |  |  |  |  |  | **      em     double       distance from Sun to observer (au) | 
| 31 |  |  |  |  |  |  | **      v      double[3]    barycentric observer velocity (vector, c) | 
| 32 |  |  |  |  |  |  | **      bm1    double       sqrt(1-|v|^2): reciprocal of Lorenz factor | 
| 33 |  |  |  |  |  |  | **      bpn    double[3][3] bias-precession-nutation matrix | 
| 34 |  |  |  |  |  |  | **      along  double       unchanged | 
| 35 |  |  |  |  |  |  | **      xpl    double       unchanged | 
| 36 |  |  |  |  |  |  | **      ypl    double       unchanged | 
| 37 |  |  |  |  |  |  | **      sphi   double       unchanged | 
| 38 |  |  |  |  |  |  | **      cphi   double       unchanged | 
| 39 |  |  |  |  |  |  | **      diurab double       unchanged | 
| 40 |  |  |  |  |  |  | **      eral   double       unchanged | 
| 41 |  |  |  |  |  |  | **      refa   double       unchanged | 
| 42 |  |  |  |  |  |  | **      refb   double       unchanged | 
| 43 |  |  |  |  |  |  | ** | 
| 44 |  |  |  |  |  |  | **  Notes: | 
| 45 |  |  |  |  |  |  | ** | 
| 46 |  |  |  |  |  |  | **  1) The TDB date date1+date2 is a Julian Date, apportioned in any | 
| 47 |  |  |  |  |  |  | **     convenient way between the two arguments.  For example, | 
| 48 |  |  |  |  |  |  | **     JD(TDB)=2450123.7 could be expressed in any of these ways, among | 
| 49 |  |  |  |  |  |  | **     others: | 
| 50 |  |  |  |  |  |  | ** | 
| 51 |  |  |  |  |  |  | **            date1          date2 | 
| 52 |  |  |  |  |  |  | ** | 
| 53 |  |  |  |  |  |  | **         2450123.7           0.0       (JD method) | 
| 54 |  |  |  |  |  |  | **         2451545.0       -1421.3       (J2000 method) | 
| 55 |  |  |  |  |  |  | **         2400000.5       50123.2       (MJD method) | 
| 56 |  |  |  |  |  |  | **         2450123.5           0.2       (date & time method) | 
| 57 |  |  |  |  |  |  | ** | 
| 58 |  |  |  |  |  |  | **     The JD method is the most natural and convenient to use in cases | 
| 59 |  |  |  |  |  |  | **     where the loss of several decimal digits of resolution is | 
| 60 |  |  |  |  |  |  | **     acceptable.  The J2000 method is best matched to the way the | 
| 61 |  |  |  |  |  |  | **     argument is handled internally and will deliver the optimum | 
| 62 |  |  |  |  |  |  | **     resolution.  The MJD method and the date & time methods are both | 
| 63 |  |  |  |  |  |  | **     good compromises between resolution and convenience.  For most | 
| 64 |  |  |  |  |  |  | **     applications of this function the choice will not be at all | 
| 65 |  |  |  |  |  |  | **     critical. | 
| 66 |  |  |  |  |  |  | ** | 
| 67 |  |  |  |  |  |  | **     TT can be used instead of TDB without any significant impact on | 
| 68 |  |  |  |  |  |  | **     accuracy. | 
| 69 |  |  |  |  |  |  | ** | 
| 70 |  |  |  |  |  |  | **  2) All the vectors are with respect to BCRS axes. | 
| 71 |  |  |  |  |  |  | ** | 
| 72 |  |  |  |  |  |  | **  3) This is one of several functions that inserts into the astrom | 
| 73 |  |  |  |  |  |  | **     structure star-independent parameters needed for the chain of | 
| 74 |  |  |  |  |  |  | **     astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed. | 
| 75 |  |  |  |  |  |  | ** | 
| 76 |  |  |  |  |  |  | **     The various functions support different classes of observer and | 
| 77 |  |  |  |  |  |  | **     portions of the transformation chain: | 
| 78 |  |  |  |  |  |  | ** | 
| 79 |  |  |  |  |  |  | **          functions         observer        transformation | 
| 80 |  |  |  |  |  |  | ** | 
| 81 |  |  |  |  |  |  | **       eraApcg eraApcg13    geocentric      ICRS <-> GCRS | 
| 82 |  |  |  |  |  |  | **       eraApci eraApci13    terrestrial     ICRS <-> CIRS | 
| 83 |  |  |  |  |  |  | **       eraApco eraApco13    terrestrial     ICRS <-> observed | 
| 84 |  |  |  |  |  |  | **       eraApcs eraApcs13    space           ICRS <-> GCRS | 
| 85 |  |  |  |  |  |  | **       eraAper eraAper13    terrestrial     update Earth rotation | 
| 86 |  |  |  |  |  |  | **       eraApio eraApio13    terrestrial     CIRS <-> observed | 
| 87 |  |  |  |  |  |  | ** | 
| 88 |  |  |  |  |  |  | **     Those with names ending in "13" use contemporary ERFA models to | 
| 89 |  |  |  |  |  |  | **     compute the various ephemerides.  The others accept ephemerides | 
| 90 |  |  |  |  |  |  | **     supplied by the caller. | 
| 91 |  |  |  |  |  |  | ** | 
| 92 |  |  |  |  |  |  | **     The transformation from ICRS to GCRS covers space motion, | 
| 93 |  |  |  |  |  |  | **     parallax, light deflection, and aberration.  From GCRS to CIRS | 
| 94 |  |  |  |  |  |  | **     comprises frame bias and precession-nutation.  From CIRS to | 
| 95 |  |  |  |  |  |  | **     observed takes account of Earth rotation, polar motion, diurnal | 
| 96 |  |  |  |  |  |  | **     aberration and parallax (unless subsumed into the ICRS <-> GCRS | 
| 97 |  |  |  |  |  |  | **     transformation), and atmospheric refraction. | 
| 98 |  |  |  |  |  |  | ** | 
| 99 |  |  |  |  |  |  | **  4) The context structure astrom produced by this function is used by | 
| 100 |  |  |  |  |  |  | **     eraAtciq* and eraAticq*. | 
| 101 |  |  |  |  |  |  | ** | 
| 102 |  |  |  |  |  |  | **  Called: | 
| 103 |  |  |  |  |  |  | **     eraApcs      astrometry parameters, ICRS-GCRS, space observer | 
| 104 |  |  |  |  |  |  | ** | 
| 105 |  |  |  |  |  |  | **  Copyright (C) 2013-2020, NumFOCUS Foundation. | 
| 106 |  |  |  |  |  |  | **  Derived, with permission, from the SOFA library.  See notes at end of file. | 
| 107 |  |  |  |  |  |  | */ | 
| 108 |  |  |  |  |  |  | { | 
| 109 |  |  |  |  |  |  | /* Geocentric observer */ | 
| 110 | 0 |  |  |  |  |  | double pv[2][3] = { { 0.0, 0.0, 0.0 }, | 
| 111 |  |  |  |  |  |  | { 0.0, 0.0, 0.0 } }; | 
| 112 |  |  |  |  |  |  |  | 
| 113 |  |  |  |  |  |  |  | 
| 114 |  |  |  |  |  |  | /* Compute the star-independent astrometry parameters. */ | 
| 115 | 0 |  |  |  |  |  | eraApcs(date1, date2, pv, ebpv, ehp, astrom); | 
| 116 |  |  |  |  |  |  |  | 
| 117 |  |  |  |  |  |  | /* Finished. */ | 
| 118 |  |  |  |  |  |  |  | 
| 119 | 0 |  |  |  |  |  | } | 
| 120 |  |  |  |  |  |  | /*---------------------------------------------------------------------- | 
| 121 |  |  |  |  |  |  | ** | 
| 122 |  |  |  |  |  |  | ** | 
| 123 |  |  |  |  |  |  | **  Copyright (C) 2013-2020, NumFOCUS Foundation. | 
| 124 |  |  |  |  |  |  | **  All rights reserved. | 
| 125 |  |  |  |  |  |  | ** | 
| 126 |  |  |  |  |  |  | **  This library is derived, with permission, from the International | 
| 127 |  |  |  |  |  |  | **  Astronomical Union's "Standards of Fundamental Astronomy" library, | 
| 128 |  |  |  |  |  |  | **  available from http://www.iausofa.org. | 
| 129 |  |  |  |  |  |  | ** | 
| 130 |  |  |  |  |  |  | **  The ERFA version is intended to retain identical functionality to | 
| 131 |  |  |  |  |  |  | **  the SOFA library, but made distinct through different function and | 
| 132 |  |  |  |  |  |  | **  file names, as set out in the SOFA license conditions.  The SOFA | 
| 133 |  |  |  |  |  |  | **  original has a role as a reference standard for the IAU and IERS, | 
| 134 |  |  |  |  |  |  | **  and consequently redistribution is permitted only in its unaltered | 
| 135 |  |  |  |  |  |  | **  state.  The ERFA version is not subject to this restriction and | 
| 136 |  |  |  |  |  |  | **  therefore can be included in distributions which do not support the | 
| 137 |  |  |  |  |  |  | **  concept of "read only" software. | 
| 138 |  |  |  |  |  |  | ** | 
| 139 |  |  |  |  |  |  | **  Although the intent is to replicate the SOFA API (other than | 
| 140 |  |  |  |  |  |  | **  replacement of prefix names) and results (with the exception of | 
| 141 |  |  |  |  |  |  | **  bugs;  any that are discovered will be fixed), SOFA is not | 
| 142 |  |  |  |  |  |  | **  responsible for any errors found in this version of the library. | 
| 143 |  |  |  |  |  |  | ** | 
| 144 |  |  |  |  |  |  | **  If you wish to acknowledge the SOFA heritage, please acknowledge | 
| 145 |  |  |  |  |  |  | **  that you are using a library derived from SOFA, rather than SOFA | 
| 146 |  |  |  |  |  |  | **  itself. | 
| 147 |  |  |  |  |  |  | ** | 
| 148 |  |  |  |  |  |  | ** | 
| 149 |  |  |  |  |  |  | **  TERMS AND CONDITIONS | 
| 150 |  |  |  |  |  |  | ** | 
| 151 |  |  |  |  |  |  | **  Redistribution and use in source and binary forms, with or without | 
| 152 |  |  |  |  |  |  | **  modification, are permitted provided that the following conditions | 
| 153 |  |  |  |  |  |  | **  are met: | 
| 154 |  |  |  |  |  |  | ** | 
| 155 |  |  |  |  |  |  | **  1 Redistributions of source code must retain the above copyright | 
| 156 |  |  |  |  |  |  | **    notice, this list of conditions and the following disclaimer. | 
| 157 |  |  |  |  |  |  | ** | 
| 158 |  |  |  |  |  |  | **  2 Redistributions in binary form must reproduce the above copyright | 
| 159 |  |  |  |  |  |  | **    notice, this list of conditions and the following disclaimer in | 
| 160 |  |  |  |  |  |  | **    the documentation and/or other materials provided with the | 
| 161 |  |  |  |  |  |  | **    distribution. | 
| 162 |  |  |  |  |  |  | ** | 
| 163 |  |  |  |  |  |  | **  3 Neither the name of the Standards Of Fundamental Astronomy Board, | 
| 164 |  |  |  |  |  |  | **    the International Astronomical Union nor the names of its | 
| 165 |  |  |  |  |  |  | **    contributors may be used to endorse or promote products derived | 
| 166 |  |  |  |  |  |  | **    from this software without specific prior written permission. | 
| 167 |  |  |  |  |  |  | ** | 
| 168 |  |  |  |  |  |  | **  THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS | 
| 169 |  |  |  |  |  |  | **  "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT | 
| 170 |  |  |  |  |  |  | **  LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS | 
| 171 |  |  |  |  |  |  | **  FOR A PARTICULAR PURPOSE ARE DISCLAIMED.  IN NO EVENT SHALL THE | 
| 172 |  |  |  |  |  |  | **  COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, | 
| 173 |  |  |  |  |  |  | **  INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, | 
| 174 |  |  |  |  |  |  | **  BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; | 
| 175 |  |  |  |  |  |  | **  LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER | 
| 176 |  |  |  |  |  |  | **  CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT | 
| 177 |  |  |  |  |  |  | **  LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN | 
| 178 |  |  |  |  |  |  | **  ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE | 
| 179 |  |  |  |  |  |  | **  POSSIBILITY OF SUCH DAMAGE. | 
| 180 |  |  |  |  |  |  | ** | 
| 181 |  |  |  |  |  |  | */ |