1 | #include "erfa.h"
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2 |
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3 | void eraAtic13(double ri, double di, double date1, double date2,
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4 | double *rc, double *dc, double *eo)
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5 | /*
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6 | ** - - - - - - - - - -
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7 | ** e r a A t i c 1 3
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8 | ** - - - - - - - - - -
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9 | **
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10 | ** Transform star RA,Dec from geocentric CIRS to ICRS astrometric.
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11 | **
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12 | ** Given:
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13 | ** ri,di double CIRS geocentric RA,Dec (radians)
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14 | ** date1 double TDB as a 2-part...
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15 | ** date2 double ...Julian Date (Note 1)
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16 | **
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17 | ** Returned:
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18 | ** rc,dc double ICRS astrometric RA,Dec (radians)
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19 | ** eo double equation of the origins (ERA-GST, Note 4)
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20 | **
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21 | ** Notes:
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22 | **
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23 | ** 1) The TDB date date1+date2 is a Julian Date, apportioned in any
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24 | ** convenient way between the two arguments. For example,
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25 | ** JD(TDB)=2450123.7 could be expressed in any of these ways, among
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26 | ** others:
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27 | **
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28 | ** date1 date2
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29 | **
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30 | ** 2450123.7 0.0 (JD method)
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31 | ** 2451545.0 -1421.3 (J2000 method)
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32 | ** 2400000.5 50123.2 (MJD method)
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33 | ** 2450123.5 0.2 (date & time method)
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34 | **
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35 | ** The JD method is the most natural and convenient to use in cases
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36 | ** where the loss of several decimal digits of resolution is
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37 | ** acceptable. The J2000 method is best matched to the way the
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38 | ** argument is handled internally and will deliver the optimum
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39 | ** resolution. The MJD method and the date & time methods are both
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40 | ** good compromises between resolution and convenience. For most
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41 | ** applications of this function the choice will not be at all
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42 | ** critical.
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43 | **
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44 | ** TT can be used instead of TDB without any significant impact on
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45 | ** accuracy.
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46 | **
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47 | ** 2) Iterative techniques are used for the aberration and light
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48 | ** deflection corrections so that the functions eraAtic13 (or
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49 | ** eraAticq) and eraAtci13 (or eraAtciq) are accurate inverses;
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50 | ** even at the edge of the Sun's disk the discrepancy is only about
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51 | ** 1 nanoarcsecond.
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52 | **
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53 | ** 3) The available accuracy is better than 1 milliarcsecond, limited
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54 | ** mainly by the precession-nutation model that is used, namely
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55 | ** IAU 2000A/2006. Very close to solar system bodies, additional
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56 | ** errors of up to several milliarcseconds can occur because of
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57 | ** unmodeled light deflection; however, the Sun's contribution is
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58 | ** taken into account, to first order. The accuracy limitations of
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59 | ** the ERFA function eraEpv00 (used to compute Earth position and
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60 | ** velocity) can contribute aberration errors of up to
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61 | ** 5 microarcseconds. Light deflection at the Sun's limb is
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62 | ** uncertain at the 0.4 mas level.
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63 | **
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64 | ** 4) Should the transformation to (equinox based) J2000.0 mean place
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65 | ** be required rather than (CIO based) ICRS coordinates, subtract the
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66 | ** equation of the origins from the returned right ascension:
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67 | ** RA = RI - EO. (The eraAnp function can then be applied, as
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68 | ** required, to keep the result in the conventional 0-2pi range.)
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69 | **
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70 | ** Called:
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71 | ** eraApci13 astrometry parameters, ICRS-CIRS, 2013
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72 | ** eraAticq quick CIRS to ICRS astrometric
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73 | **
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74 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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75 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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76 | */
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77 | {
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78 | /* Star-independent astrometry parameters */
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79 | eraASTROM astrom;
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80 |
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81 |
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82 | /* Star-independent astrometry parameters. */
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83 | eraApci13(date1, date2, &astrom, eo);
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84 |
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85 | /* CIRS to ICRS astrometric. */
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86 | eraAticq(ri, di, &astrom, rc, dc);
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87 |
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88 | /* Finished. */
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89 |
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90 | }
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91 | /*----------------------------------------------------------------------
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92 | **
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93 | **
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94 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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95 | ** All rights reserved.
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96 | **
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97 | ** This library is derived, with permission, from the International
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98 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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99 | ** available from http://www.iausofa.org.
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100 | **
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101 | ** The ERFA version is intended to retain identical functionality to
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102 | ** the SOFA library, but made distinct through different function and
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103 | ** file names, as set out in the SOFA license conditions. The SOFA
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104 | ** original has a role as a reference standard for the IAU and IERS,
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105 | ** and consequently redistribution is permitted only in its unaltered
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106 | ** state. The ERFA version is not subject to this restriction and
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107 | ** therefore can be included in distributions which do not support the
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108 | ** concept of "read only" software.
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109 | **
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110 | ** Although the intent is to replicate the SOFA API (other than
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111 | ** replacement of prefix names) and results (with the exception of
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112 | ** bugs; any that are discovered will be fixed), SOFA is not
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113 | ** responsible for any errors found in this version of the library.
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114 | **
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115 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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116 | ** that you are using a library derived from SOFA, rather than SOFA
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117 | ** itself.
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118 | **
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119 | **
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120 | ** TERMS AND CONDITIONS
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121 | **
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122 | ** Redistribution and use in source and binary forms, with or without
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123 | ** modification, are permitted provided that the following conditions
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124 | ** are met:
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125 | **
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126 | ** 1 Redistributions of source code must retain the above copyright
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127 | ** notice, this list of conditions and the following disclaimer.
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128 | **
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129 | ** 2 Redistributions in binary form must reproduce the above copyright
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130 | ** notice, this list of conditions and the following disclaimer in
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131 | ** the documentation and/or other materials provided with the
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132 | ** distribution.
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133 | **
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134 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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135 | ** the International Astronomical Union nor the names of its
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136 | ** contributors may be used to endorse or promote products derived
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137 | ** from this software without specific prior written permission.
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138 | **
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139 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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140 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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141 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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142 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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143 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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144 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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145 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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146 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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147 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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148 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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149 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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150 | ** POSSIBILITY OF SUCH DAMAGE.
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151 | **
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152 | */
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