1 | #include "erfa.h"
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2 |
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3 | void eraLdn(int n, eraLDBODY b[], double ob[3], double sc[3],
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4 | double sn[3])
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5 | /*+
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6 | ** - - - - - - -
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7 | ** e r a L d n
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8 | ** - - - - - - -
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9 | **
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10 | ** For a star, apply light deflection by multiple solar-system bodies,
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11 | ** as part of transforming coordinate direction into natural direction.
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12 | **
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13 | ** Given:
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14 | ** n int number of bodies (note 1)
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15 | ** b eraLDBODY[n] data for each of the n bodies (Notes 1,2):
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16 | ** bm double mass of the body (solar masses, Note 3)
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17 | ** dl double deflection limiter (Note 4)
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18 | ** pv [2][3] barycentric PV of the body (au, au/day)
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19 | ** ob double[3] barycentric position of the observer (au)
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20 | ** sc double[3] observer to star coord direction (unit vector)
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21 | **
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22 | ** Returned:
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23 | ** sn double[3] observer to deflected star (unit vector)
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24 | **
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25 | ** 1) The array b contains n entries, one for each body to be
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26 | ** considered. If n = 0, no gravitational light deflection will be
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27 | ** applied, not even for the Sun.
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28 | **
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29 | ** 2) The array b should include an entry for the Sun as well as for
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30 | ** any planet or other body to be taken into account. The entries
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31 | ** should be in the order in which the light passes the body.
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32 | **
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33 | ** 3) In the entry in the b array for body i, the mass parameter
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34 | ** b[i].bm can, as required, be adjusted in order to allow for such
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35 | ** effects as quadrupole field.
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36 | **
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37 | ** 4) The deflection limiter parameter b[i].dl is phi^2/2, where phi is
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38 | ** the angular separation (in radians) between star and body at
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39 | ** which limiting is applied. As phi shrinks below the chosen
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40 | ** threshold, the deflection is artificially reduced, reaching zero
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41 | ** for phi = 0. Example values suitable for a terrestrial
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42 | ** observer, together with masses, are as follows:
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43 | **
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44 | ** body i b[i].bm b[i].dl
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45 | **
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46 | ** Sun 1.0 6e-6
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47 | ** Jupiter 0.00095435 3e-9
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48 | ** Saturn 0.00028574 3e-10
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49 | **
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50 | ** 5) For cases where the starlight passes the body before reaching the
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51 | ** observer, the body is placed back along its barycentric track by
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52 | ** the light time from that point to the observer. For cases where
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53 | ** the body is "behind" the observer no such shift is applied. If
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54 | ** a different treatment is preferred, the user has the option of
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55 | ** instead using the eraLd function. Similarly, eraLd can be used
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56 | ** for cases where the source is nearby, not a star.
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57 | **
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58 | ** 6) The returned vector sn is not normalized, but the consequential
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59 | ** departure from unit magnitude is always negligible.
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60 | **
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61 | ** 7) The arguments sc and sn can be the same array.
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62 | **
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63 | ** 8) For efficiency, validation is omitted. The supplied masses must
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64 | ** be greater than zero, the position and velocity vectors must be
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65 | ** right, and the deflection limiter greater than zero.
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66 | **
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67 | ** Reference:
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68 | **
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69 | ** Urban, S. & Seidelmann, P. K. (eds), Explanatory Supplement to
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70 | ** the Astronomical Almanac, 3rd ed., University Science Books
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71 | ** (2013), Section 7.2.4.
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72 | **
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73 | ** Called:
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74 | ** eraCp copy p-vector
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75 | ** eraPdp scalar product of two p-vectors
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76 | ** eraPmp p-vector minus p-vector
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77 | ** eraPpsp p-vector plus scaled p-vector
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78 | ** eraPn decompose p-vector into modulus and direction
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79 | ** eraLd light deflection by a solar-system body
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80 | **
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81 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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82 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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83 | */
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84 | {
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85 | /* Light time for 1 AU (days) */
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86 | const double CR = ERFA_AULT/ERFA_DAYSEC;
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87 |
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88 | int i;
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89 | double v[3], dt, ev[3], em, e[3];
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90 |
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91 |
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92 | /* Star direction prior to deflection. */
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93 | eraCp(sc, sn);
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94 |
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95 | /* Body by body. */
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96 | for ( i = 0; i < n; i++ ) {
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97 |
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98 | /* Body to observer vector at epoch of observation (au). */
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99 | eraPmp ( ob, b[i].pv[0], v );
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100 |
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101 | /* Minus the time since the light passed the body (days). */
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102 | dt = eraPdp(sn,v) * CR;
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103 |
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104 | /* Neutralize if the star is "behind" the observer. */
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105 | dt = ERFA_GMIN(dt, 0.0);
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106 |
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107 | /* Backtrack the body to the time the light was passing the body. */
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108 | eraPpsp(v, -dt, b[i].pv[1], ev);
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109 |
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110 | /* Body to observer vector as magnitude and direction. */
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111 | eraPn(ev, &em, e);
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112 |
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113 | /* Apply light deflection for this body. */
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114 | eraLd ( b[i].bm, sn, sn, e, em, b[i].dl, sn );
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115 |
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116 | /* Next body. */
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117 | }
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118 |
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119 | /* Finished. */
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120 |
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121 | }
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122 | /*----------------------------------------------------------------------
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123 | **
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124 | **
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125 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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126 | ** All rights reserved.
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127 | **
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128 | ** This library is derived, with permission, from the International
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129 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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130 | ** available from http://www.iausofa.org.
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131 | **
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132 | ** The ERFA version is intended to retain identical functionality to
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133 | ** the SOFA library, but made distinct through different function and
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134 | ** file names, as set out in the SOFA license conditions. The SOFA
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135 | ** original has a role as a reference standard for the IAU and IERS,
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136 | ** and consequently redistribution is permitted only in its unaltered
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137 | ** state. The ERFA version is not subject to this restriction and
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138 | ** therefore can be included in distributions which do not support the
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139 | ** concept of "read only" software.
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140 | **
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141 | ** Although the intent is to replicate the SOFA API (other than
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142 | ** replacement of prefix names) and results (with the exception of
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143 | ** bugs; any that are discovered will be fixed), SOFA is not
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144 | ** responsible for any errors found in this version of the library.
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145 | **
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146 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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147 | ** that you are using a library derived from SOFA, rather than SOFA
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148 | ** itself.
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149 | **
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150 | **
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151 | ** TERMS AND CONDITIONS
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152 | **
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153 | ** Redistribution and use in source and binary forms, with or without
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154 | ** modification, are permitted provided that the following conditions
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155 | ** are met:
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156 | **
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157 | ** 1 Redistributions of source code must retain the above copyright
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158 | ** notice, this list of conditions and the following disclaimer.
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159 | **
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160 | ** 2 Redistributions in binary form must reproduce the above copyright
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161 | ** notice, this list of conditions and the following disclaimer in
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162 | ** the documentation and/or other materials provided with the
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163 | ** distribution.
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164 | **
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165 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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166 | ** the International Astronomical Union nor the names of its
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167 | ** contributors may be used to endorse or promote products derived
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168 | ** from this software without specific prior written permission.
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169 | **
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170 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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171 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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172 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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173 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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174 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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175 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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176 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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177 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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178 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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179 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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180 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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181 | ** POSSIBILITY OF SUCH DAMAGE.
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182 | **
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183 | */
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