| 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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