| 1 | #include "erfa.h"
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| 2 |
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| 3 | void eraAticqn(double ri, double di, eraASTROM *astrom,
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| 4 | int n, eraLDBODY b[], double *rc, double *dc)
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| 5 | /*
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| 6 | ** - - - - - - - - -
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| 7 | ** e r a A t i c q n
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| 8 | ** - - - - - - - - -
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| 9 | **
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| 10 | ** Quick CIRS to ICRS astrometric place transformation, given the star-
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| 11 | ** independent astrometry parameters plus a list of light-deflecting
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| 12 | ** bodies.
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| 13 | **
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| 14 | ** Use of this function is appropriate when efficiency is important and
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| 15 | ** where many star positions are all to be transformed for one date.
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| 16 | ** The star-independent astrometry parameters can be obtained by
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| 17 | ** calling one of the functions eraApci[13], eraApcg[13], eraApco[13]
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| 18 | ** or eraApcs[13].
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| 19 | *
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| 20 | * If the only light-deflecting body to be taken into account is the
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| 21 | * Sun, the eraAticq function can be used instead.
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| 22 | **
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| 23 | ** Given:
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| 24 | ** ri,di double CIRS RA,Dec (radians)
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| 25 | ** astrom eraASTROM* star-independent astrometry parameters:
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| 26 | ** pmt double PM time interval (SSB, Julian years)
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| 27 | ** eb double[3] SSB to observer (vector, au)
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| 28 | ** eh double[3] Sun to observer (unit vector)
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| 29 | ** em double distance from Sun to observer (au)
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| 30 | ** v double[3] barycentric observer velocity (vector, c)
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| 31 | ** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
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| 32 | ** bpn double[3][3] bias-precession-nutation matrix
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| 33 | ** along double longitude + s' (radians)
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| 34 | ** xpl double polar motion xp wrt local meridian (radians)
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| 35 | ** ypl double polar motion yp wrt local meridian (radians)
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| 36 | ** sphi double sine of geodetic latitude
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| 37 | ** cphi double cosine of geodetic latitude
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| 38 | ** diurab double magnitude of diurnal aberration vector
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| 39 | ** eral double "local" Earth rotation angle (radians)
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| 40 | ** refa double refraction constant A (radians)
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| 41 | ** refb double refraction constant B (radians)
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| 42 | ** n int number of bodies (Note 3)
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| 43 | ** b eraLDBODY[n] data for each of the n bodies (Notes 3,4):
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| 44 | ** bm double mass of the body (solar masses, Note 5)
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| 45 | ** dl double deflection limiter (Note 6)
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| 46 | ** pv [2][3] barycentric PV of the body (au, au/day)
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| 47 | **
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| 48 | ** Returned:
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| 49 | ** rc,dc double ICRS astrometric RA,Dec (radians)
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| 50 | **
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| 51 | ** Notes:
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| 52 | **
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| 53 | ** 1) Iterative techniques are used for the aberration and light
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| 54 | ** deflection corrections so that the functions eraAticqn and
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| 55 | ** eraAtciqn are accurate inverses; even at the edge of the Sun's
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| 56 | ** disk the discrepancy is only about 1 nanoarcsecond.
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| 57 | **
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| 58 | ** 2) If the only light-deflecting body to be taken into account is the
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| 59 | ** Sun, the eraAticq function can be used instead.
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| 60 | **
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| 61 | ** 3) The struct b contains n entries, one for each body to be
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| 62 | ** considered. If n = 0, no gravitational light deflection will be
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| 63 | ** applied, not even for the Sun.
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| 64 | **
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| 65 | ** 4) The struct b should include an entry for the Sun as well as for
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| 66 | ** any planet or other body to be taken into account. The entries
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| 67 | ** should be in the order in which the light passes the body.
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| 68 | **
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| 69 | ** 5) In the entry in the b struct for body i, the mass parameter
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| 70 | ** b[i].bm can, as required, be adjusted in order to allow for such
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| 71 | ** effects as quadrupole field.
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| 72 | **
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| 73 | ** 6) The deflection limiter parameter b[i].dl is phi^2/2, where phi is
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| 74 | ** the angular separation (in radians) between star and body at
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| 75 | ** which limiting is applied. As phi shrinks below the chosen
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| 76 | ** threshold, the deflection is artificially reduced, reaching zero
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| 77 | ** for phi = 0. Example values suitable for a terrestrial
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| 78 | ** observer, together with masses, are as follows:
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| 79 | **
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| 80 | ** body i b[i].bm b[i].dl
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| 81 | **
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| 82 | ** Sun 1.0 6e-6
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| 83 | ** Jupiter 0.00095435 3e-9
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| 84 | ** Saturn 0.00028574 3e-10
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| 85 | **
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| 86 | ** 7) For efficiency, validation of the contents of the b array is
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| 87 | ** omitted. The supplied masses must be greater than zero, the
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| 88 | ** position and velocity vectors must be right, and the deflection
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| 89 | ** limiter greater than zero.
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| 90 | **
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| 91 | ** Called:
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| 92 | ** eraS2c spherical coordinates to unit vector
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| 93 | ** eraTrxp product of transpose of r-matrix and p-vector
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| 94 | ** eraZp zero p-vector
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| 95 | ** eraAb stellar aberration
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| 96 | ** eraLdn light deflection by n bodies
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| 97 | ** eraC2s p-vector to spherical
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| 98 | ** eraAnp normalize angle into range +/- pi
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| 99 | **
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| 100 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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| 101 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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| 102 | */
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| 103 | {
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| 104 | int j, i;
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| 105 | double pi[3], ppr[3], pnat[3], pco[3], w, d[3], before[3], r2, r,
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| 106 | after[3];
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| 107 |
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| 108 |
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| 109 | /* CIRS RA,Dec to Cartesian. */
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| 110 | eraS2c(ri, di, pi);
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| 111 |
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| 112 | /* Bias-precession-nutation, giving GCRS proper direction. */
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| 113 | eraTrxp(astrom->bpn, pi, ppr);
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| 114 |
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| 115 | /* Aberration, giving GCRS natural direction. */
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| 116 | eraZp(d);
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| 117 | for (j = 0; j < 2; j++) {
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| 118 | r2 = 0.0;
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| 119 | for (i = 0; i < 3; i++) {
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| 120 | w = ppr[i] - d[i];
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| 121 | before[i] = w;
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| 122 | r2 += w*w;
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| 123 | }
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| 124 | r = sqrt(r2);
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| 125 | for (i = 0; i < 3; i++) {
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| 126 | before[i] /= r;
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| 127 | }
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| 128 | eraAb(before, astrom->v, astrom->em, astrom->bm1, after);
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| 129 | r2 = 0.0;
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| 130 | for (i = 0; i < 3; i++) {
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| 131 | d[i] = after[i] - before[i];
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| 132 | w = ppr[i] - d[i];
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| 133 | pnat[i] = w;
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| 134 | r2 += w*w;
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| 135 | }
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| 136 | r = sqrt(r2);
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| 137 | for (i = 0; i < 3; i++) {
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| 138 | pnat[i] /= r;
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| 139 | }
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| 140 | }
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| 141 |
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| 142 | /* Light deflection, giving BCRS coordinate direction. */
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| 143 | eraZp(d);
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| 144 | for (j = 0; j < 5; j++) {
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| 145 | r2 = 0.0;
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| 146 | for (i = 0; i < 3; i++) {
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| 147 | w = pnat[i] - d[i];
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| 148 | before[i] = w;
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| 149 | r2 += w*w;
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| 150 | }
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| 151 | r = sqrt(r2);
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| 152 | for (i = 0; i < 3; i++) {
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| 153 | before[i] /= r;
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| 154 | }
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| 155 | eraLdn(n, b, astrom->eb, before, after);
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| 156 | r2 = 0.0;
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| 157 | for (i = 0; i < 3; i++) {
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| 158 | d[i] = after[i] - before[i];
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| 159 | w = pnat[i] - d[i];
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| 160 | pco[i] = w;
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| 161 | r2 += w*w;
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| 162 | }
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| 163 | r = sqrt(r2);
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| 164 | for (i = 0; i < 3; i++) {
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| 165 | pco[i] /= r;
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| 166 | }
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| 167 | }
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| 168 |
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| 169 | /* ICRS astrometric RA,Dec. */
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| 170 | eraC2s(pco, &w, dc);
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| 171 | *rc = eraAnp(w);
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| 172 |
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| 173 | /* Finished. */
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| 174 |
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| 175 | }
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| 176 | /*----------------------------------------------------------------------
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| 177 | **
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| 178 | **
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| 179 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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| 180 | ** All rights reserved.
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| 181 | **
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| 182 | ** This library is derived, with permission, from the International
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| 183 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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| 184 | ** available from http://www.iausofa.org.
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| 185 | **
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| 186 | ** The ERFA version is intended to retain identical functionality to
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| 187 | ** the SOFA library, but made distinct through different function and
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| 188 | ** file names, as set out in the SOFA license conditions. The SOFA
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| 189 | ** original has a role as a reference standard for the IAU and IERS,
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| 190 | ** and consequently redistribution is permitted only in its unaltered
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| 191 | ** state. The ERFA version is not subject to this restriction and
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| 192 | ** therefore can be included in distributions which do not support the
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| 193 | ** concept of "read only" software.
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| 194 | **
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| 195 | ** Although the intent is to replicate the SOFA API (other than
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| 196 | ** replacement of prefix names) and results (with the exception of
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| 197 | ** bugs; any that are discovered will be fixed), SOFA is not
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| 198 | ** responsible for any errors found in this version of the library.
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| 199 | **
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| 200 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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| 201 | ** that you are using a library derived from SOFA, rather than SOFA
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| 202 | ** itself.
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| 203 | **
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| 204 | **
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| 205 | ** TERMS AND CONDITIONS
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| 206 | **
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| 207 | ** Redistribution and use in source and binary forms, with or without
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| 208 | ** modification, are permitted provided that the following conditions
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| 209 | ** are met:
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| 210 | **
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| 211 | ** 1 Redistributions of source code must retain the above copyright
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| 212 | ** notice, this list of conditions and the following disclaimer.
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| 213 | **
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| 214 | ** 2 Redistributions in binary form must reproduce the above copyright
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| 215 | ** notice, this list of conditions and the following disclaimer in
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| 216 | ** the documentation and/or other materials provided with the
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| 217 | ** distribution.
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| 218 | **
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| 219 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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| 220 | ** the International Astronomical Union nor the names of its
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| 221 | ** contributors may be used to endorse or promote products derived
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| 222 | ** from this software without specific prior written permission.
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| 223 | **
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| 224 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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| 225 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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| 226 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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| 227 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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| 228 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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| 229 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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| 230 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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| 231 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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| 232 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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| 233 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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| 234 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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| 235 | ** POSSIBILITY OF SUCH DAMAGE.
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| 236 | **
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| 237 | */
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