1 | #include "erfa.h"
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2 |
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3 | void eraLd(double bm, double p[3], double q[3], double e[3],
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4 | double em, double dlim, double p1[3])
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5 | /*
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6 | ** - - - - - -
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7 | ** e r a L d
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8 | ** - - - - - -
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9 | **
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10 | ** Apply light deflection by a solar-system body, as part of
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11 | ** transforming coordinate direction into natural direction.
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12 | **
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13 | ** Given:
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14 | ** bm double mass of the gravitating body (solar masses)
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15 | ** p double[3] direction from observer to source (unit vector)
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16 | ** q double[3] direction from body to source (unit vector)
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17 | ** e double[3] direction from body to observer (unit vector)
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18 | ** em double distance from body to observer (au)
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19 | ** dlim double deflection limiter (Note 4)
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20 | **
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21 | ** Returned:
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22 | ** p1 double[3] observer to deflected source (unit vector)
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23 | **
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24 | ** Notes:
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25 | **
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26 | ** 1) The algorithm is based on Expr. (70) in Klioner (2003) and
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27 | ** Expr. (7.63) in the Explanatory Supplement (Urban & Seidelmann
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28 | ** 2013), with some rearrangement to minimize the effects of machine
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29 | ** precision.
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30 | **
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31 | ** 2) The mass parameter bm can, as required, be adjusted in order to
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32 | ** allow for such effects as quadrupole field.
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33 | **
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34 | ** 3) The barycentric position of the deflecting body should ideally
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35 | ** correspond to the time of closest approach of the light ray to
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36 | ** the body.
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37 | **
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38 | ** 4) The deflection limiter parameter dlim is phi^2/2, where phi is
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39 | ** the angular separation (in radians) between source and body at
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40 | ** which limiting is applied. As phi shrinks below the chosen
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41 | ** threshold, the deflection is artificially reduced, reaching zero
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42 | ** for phi = 0.
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43 | **
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44 | ** 5) The returned vector p1 is not normalized, but the consequential
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45 | ** departure from unit magnitude is always negligible.
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46 | **
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47 | ** 6) The arguments p and p1 can be the same array.
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48 | **
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49 | ** 7) To accumulate total light deflection taking into account the
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50 | ** contributions from several bodies, call the present function for
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51 | ** each body in succession, in decreasing order of distance from the
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52 | ** observer.
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53 | **
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54 | ** 8) For efficiency, validation is omitted. The supplied vectors must
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55 | ** be of unit magnitude, and the deflection limiter non-zero and
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56 | ** positive.
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57 | **
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58 | ** References:
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59 | **
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60 | ** Urban, S. & Seidelmann, P. K. (eds), Explanatory Supplement to
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61 | ** the Astronomical Almanac, 3rd ed., University Science Books
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62 | ** (2013).
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63 | **
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64 | ** Klioner, Sergei A., "A practical relativistic model for micro-
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65 | ** arcsecond astrometry in space", Astr. J. 125, 1580-1597 (2003).
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66 | **
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67 | ** Called:
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68 | ** eraPdp scalar product of two p-vectors
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69 | ** eraPxp vector product of two p-vectors
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70 | **
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71 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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72 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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73 | */
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74 | {
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75 | int i;
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76 | double qpe[3], qdqpe, w, eq[3], peq[3];
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77 |
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78 |
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79 | /* q . (q + e). */
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80 | for (i = 0; i < 3; i++) {
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81 | qpe[i] = q[i] + e[i];
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82 | }
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83 | qdqpe = eraPdp(q, qpe);
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84 |
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85 | /* 2 x G x bm / ( em x c^2 x ( q . (q + e) ) ). */
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86 | w = bm * ERFA_SRS / em / ERFA_GMAX(qdqpe,dlim);
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87 |
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88 | /* p x (e x q). */
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89 | eraPxp(e, q, eq);
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90 | eraPxp(p, eq, peq);
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91 |
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92 | /* Apply the deflection. */
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93 | for (i = 0; i < 3; i++) {
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94 | p1[i] = p[i] + w*peq[i];
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95 | }
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96 |
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97 | /* Finished. */
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98 |
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99 | }
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100 | /*----------------------------------------------------------------------
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101 | **
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102 | **
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103 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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104 | ** All rights reserved.
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105 | **
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106 | ** This library is derived, with permission, from the International
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107 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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108 | ** available from http://www.iausofa.org.
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109 | **
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110 | ** The ERFA version is intended to retain identical functionality to
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111 | ** the SOFA library, but made distinct through different function and
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112 | ** file names, as set out in the SOFA license conditions. The SOFA
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113 | ** original has a role as a reference standard for the IAU and IERS,
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114 | ** and consequently redistribution is permitted only in its unaltered
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115 | ** state. The ERFA version is not subject to this restriction and
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116 | ** therefore can be included in distributions which do not support the
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117 | ** concept of "read only" software.
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118 | **
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119 | ** Although the intent is to replicate the SOFA API (other than
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120 | ** replacement of prefix names) and results (with the exception of
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121 | ** bugs; any that are discovered will be fixed), SOFA is not
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122 | ** responsible for any errors found in this version of the library.
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123 | **
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124 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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125 | ** that you are using a library derived from SOFA, rather than SOFA
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126 | ** itself.
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127 | **
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128 | **
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129 | ** TERMS AND CONDITIONS
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130 | **
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131 | ** Redistribution and use in source and binary forms, with or without
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132 | ** modification, are permitted provided that the following conditions
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133 | ** are met:
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134 | **
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135 | ** 1 Redistributions of source code must retain the above copyright
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136 | ** notice, this list of conditions and the following disclaimer.
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137 | **
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138 | ** 2 Redistributions in binary form must reproduce the above copyright
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139 | ** notice, this list of conditions and the following disclaimer in
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140 | ** the documentation and/or other materials provided with the
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141 | ** distribution.
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142 | **
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143 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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144 | ** the International Astronomical Union nor the names of its
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145 | ** contributors may be used to endorse or promote products derived
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146 | ** from this software without specific prior written permission.
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147 | **
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148 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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149 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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150 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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151 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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152 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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153 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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154 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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155 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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156 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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157 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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158 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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159 | ** POSSIBILITY OF SUCH DAMAGE.
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160 | **
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161 | */
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