| 1 | #include "erfa.h"
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| 2 |
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| 3 | void eraAtioq(double ri, double di, eraASTROM *astrom,
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| 4 | double *aob, double *zob,
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| 5 | double *hob, double *dob, double *rob)
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| 6 | /*
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| 7 | ** - - - - - - - - -
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| 8 | ** e r a A t i o q
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| 9 | ** - - - - - - - - -
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| 10 | **
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| 11 | ** Quick CIRS to observed place transformation.
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| 12 | **
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| 13 | ** Use of this function is appropriate when efficiency is important and
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| 14 | ** where many star positions are all to be transformed for one date.
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| 15 | ** The star-independent astrometry parameters can be obtained by
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| 16 | ** calling eraApio[13] or eraApco[13].
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| 17 | **
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| 18 | ** Given:
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| 19 | ** ri double CIRS right ascension
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| 20 | ** di double CIRS declination
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| 21 | ** astrom eraASTROM* star-independent astrometry parameters:
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| 22 | ** pmt double PM time interval (SSB, Julian years)
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| 23 | ** eb double[3] SSB to observer (vector, au)
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| 24 | ** eh double[3] Sun to observer (unit vector)
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| 25 | ** em double distance from Sun to observer (au)
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| 26 | ** v double[3] barycentric observer velocity (vector, c)
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| 27 | ** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
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| 28 | ** bpn double[3][3] bias-precession-nutation matrix
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| 29 | ** along double longitude + s' (radians)
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| 30 | ** xpl double polar motion xp wrt local meridian (radians)
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| 31 | ** ypl double polar motion yp wrt local meridian (radians)
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| 32 | ** sphi double sine of geodetic latitude
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| 33 | ** cphi double cosine of geodetic latitude
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| 34 | ** diurab double magnitude of diurnal aberration vector
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| 35 | ** eral double "local" Earth rotation angle (radians)
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| 36 | ** refa double refraction constant A (radians)
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| 37 | ** refb double refraction constant B (radians)
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| 38 | **
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| 39 | ** Returned:
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| 40 | ** aob double* observed azimuth (radians: N=0,E=90)
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| 41 | ** zob double* observed zenith distance (radians)
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| 42 | ** hob double* observed hour angle (radians)
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| 43 | ** dob double* observed declination (radians)
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| 44 | ** rob double* observed right ascension (CIO-based, radians)
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| 45 | **
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| 46 | ** Notes:
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| 47 | **
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| 48 | ** 1) This function returns zenith distance rather than altitude in
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| 49 | ** order to reflect the fact that no allowance is made for
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| 50 | ** depression of the horizon.
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| 51 | **
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| 52 | ** 2) The accuracy of the result is limited by the corrections for
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| 53 | ** refraction, which use a simple A*tan(z) + B*tan^3(z) model.
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| 54 | ** Providing the meteorological parameters are known accurately and
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| 55 | ** there are no gross local effects, the predicted observed
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| 56 | ** coordinates should be within 0.05 arcsec (optical) or 1 arcsec
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| 57 | ** (radio) for a zenith distance of less than 70 degrees, better
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| 58 | ** than 30 arcsec (optical or radio) at 85 degrees and better
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| 59 | ** than 20 arcmin (optical) or 30 arcmin (radio) at the horizon.
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| 60 | **
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| 61 | ** Without refraction, the complementary functions eraAtioq and
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| 62 | ** eraAtoiq are self-consistent to better than 1 microarcsecond all
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| 63 | ** over the celestial sphere. With refraction included, consistency
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| 64 | ** falls off at high zenith distances, but is still better than
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| 65 | ** 0.05 arcsec at 85 degrees.
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| 66 | **
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| 67 | ** 3) It is advisable to take great care with units, as even unlikely
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| 68 | ** values of the input parameters are accepted and processed in
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| 69 | ** accordance with the models used.
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| 70 | **
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| 71 | ** 4) The CIRS RA,Dec is obtained from a star catalog mean place by
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| 72 | ** allowing for space motion, parallax, the Sun's gravitational lens
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| 73 | ** effect, annual aberration and precession-nutation. For star
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| 74 | ** positions in the ICRS, these effects can be applied by means of
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| 75 | ** the eraAtci13 (etc.) functions. Starting from classical "mean
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| 76 | ** place" systems, additional transformations will be needed first.
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| 77 | **
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| 78 | ** 5) "Observed" Az,El means the position that would be seen by a
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| 79 | ** perfect geodetically aligned theodolite. This is obtained from
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| 80 | ** the CIRS RA,Dec by allowing for Earth orientation and diurnal
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| 81 | ** aberration, rotating from equator to horizon coordinates, and
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| 82 | ** then adjusting for refraction. The HA,Dec is obtained by
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| 83 | ** rotating back into equatorial coordinates, and is the position
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| 84 | ** that would be seen by a perfect equatorial with its polar axis
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| 85 | ** aligned to the Earth's axis of rotation. Finally, the RA is
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| 86 | ** obtained by subtracting the HA from the local ERA.
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| 87 | **
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| 88 | ** 6) The star-independent CIRS-to-observed-place parameters in ASTROM
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| 89 | ** may be computed with eraApio[13] or eraApco[13]. If nothing has
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| 90 | ** changed significantly except the time, eraAper[13] may be used to
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| 91 | ** perform the requisite adjustment to the astrom structure.
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| 92 | **
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| 93 | ** Called:
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| 94 | ** eraS2c spherical coordinates to unit vector
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| 95 | ** eraC2s p-vector to spherical
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| 96 | ** eraAnp normalize angle into range 0 to 2pi
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| 97 | **
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| 98 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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| 99 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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| 100 | */
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| 101 | {
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| 102 | /* Minimum cos(alt) and sin(alt) for refraction purposes */
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| 103 | const double CELMIN = 1e-6;
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| 104 | const double SELMIN = 0.05;
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| 105 |
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| 106 | double v[3], x, y, z, xhd, yhd, zhd, f, xhdt, yhdt, zhdt,
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| 107 | xaet, yaet, zaet, azobs, r, tz, w, del, cosdel,
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| 108 | xaeo, yaeo, zaeo, zdobs, hmobs, dcobs, raobs;
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| 109 |
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| 110 |
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| 111 | /* CIRS RA,Dec to Cartesian -HA,Dec. */
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| 112 | eraS2c(ri-astrom->eral, di, v);
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| 113 | x = v[0];
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| 114 | y = v[1];
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| 115 | z = v[2];
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| 116 |
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| 117 | /* Polar motion. */
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| 118 | xhd = x + astrom->xpl*z;
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| 119 | yhd = y - astrom->ypl*z;
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| 120 | zhd = z - astrom->xpl*x + astrom->ypl*y;
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| 121 |
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| 122 | /* Diurnal aberration. */
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| 123 | f = ( 1.0 - astrom->diurab*yhd );
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| 124 | xhdt = f * xhd;
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| 125 | yhdt = f * ( yhd + astrom->diurab );
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| 126 | zhdt = f * zhd;
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| 127 |
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| 128 | /* Cartesian -HA,Dec to Cartesian Az,El (S=0,E=90). */
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| 129 | xaet = astrom->sphi*xhdt - astrom->cphi*zhdt;
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| 130 | yaet = yhdt;
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| 131 | zaet = astrom->cphi*xhdt + astrom->sphi*zhdt;
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| 132 |
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| 133 | /* Azimuth (N=0,E=90). */
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| 134 | azobs = ( xaet != 0.0 || yaet != 0.0 ) ? atan2(yaet,-xaet) : 0.0;
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| 135 |
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| 136 | /* ---------- */
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| 137 | /* Refraction */
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| 138 | /* ---------- */
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| 139 |
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| 140 | /* Cosine and sine of altitude, with precautions. */
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| 141 | r = sqrt(xaet*xaet + yaet*yaet);
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| 142 | r = r > CELMIN ? r : CELMIN;
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| 143 | z = zaet > SELMIN ? zaet : SELMIN;
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| 144 |
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| 145 | /* A*tan(z)+B*tan^3(z) model, with Newton-Raphson correction. */
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| 146 | tz = r/z;
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| 147 | w = astrom->refb*tz*tz;
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| 148 | del = ( astrom->refa + w ) * tz /
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| 149 | ( 1.0 + ( astrom->refa + 3.0*w ) / ( z*z ) );
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| 150 |
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| 151 | /* Apply the change, giving observed vector. */
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| 152 | cosdel = 1.0 - del*del/2.0;
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| 153 | f = cosdel - del*z/r;
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| 154 | xaeo = xaet*f;
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| 155 | yaeo = yaet*f;
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| 156 | zaeo = cosdel*zaet + del*r;
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| 157 |
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| 158 | /* Observed ZD. */
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| 159 | zdobs = atan2(sqrt(xaeo*xaeo+yaeo*yaeo), zaeo);
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| 160 |
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| 161 | /* Az/El vector to HA,Dec vector (both right-handed). */
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| 162 | v[0] = astrom->sphi*xaeo + astrom->cphi*zaeo;
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| 163 | v[1] = yaeo;
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| 164 | v[2] = - astrom->cphi*xaeo + astrom->sphi*zaeo;
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| 165 |
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| 166 | /* To spherical -HA,Dec. */
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| 167 | eraC2s ( v, &hmobs, &dcobs );
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| 168 |
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| 169 | /* Right ascension (with respect to CIO). */
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| 170 | raobs = astrom->eral + hmobs;
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| 171 |
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| 172 | /* Return the results. */
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| 173 | *aob = eraAnp(azobs);
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| 174 | *zob = zdobs;
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| 175 | *hob = -hmobs;
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| 176 | *dob = dcobs;
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| 177 | *rob = eraAnp(raobs);
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| 178 |
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| 179 | /* Finished. */
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| 180 |
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| 181 | }
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| 182 | /*----------------------------------------------------------------------
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| 183 | **
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| 184 | **
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| 185 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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| 186 | ** All rights reserved.
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| 187 | **
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| 188 | ** This library is derived, with permission, from the International
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| 189 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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| 190 | ** available from http://www.iausofa.org.
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| 191 | **
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| 192 | ** The ERFA version is intended to retain identical functionality to
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| 193 | ** the SOFA library, but made distinct through different function and
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| 194 | ** file names, as set out in the SOFA license conditions. The SOFA
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| 195 | ** original has a role as a reference standard for the IAU and IERS,
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| 196 | ** and consequently redistribution is permitted only in its unaltered
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| 197 | ** state. The ERFA version is not subject to this restriction and
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| 198 | ** therefore can be included in distributions which do not support the
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| 199 | ** concept of "read only" software.
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| 200 | **
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| 201 | ** Although the intent is to replicate the SOFA API (other than
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| 202 | ** replacement of prefix names) and results (with the exception of
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| 203 | ** bugs; any that are discovered will be fixed), SOFA is not
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| 204 | ** responsible for any errors found in this version of the library.
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| 205 | **
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| 206 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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| 207 | ** that you are using a library derived from SOFA, rather than SOFA
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| 208 | ** itself.
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| 209 | **
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| 210 | **
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| 211 | ** TERMS AND CONDITIONS
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| 212 | **
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| 213 | ** Redistribution and use in source and binary forms, with or without
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| 214 | ** modification, are permitted provided that the following conditions
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| 215 | ** are met:
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| 216 | **
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| 217 | ** 1 Redistributions of source code must retain the above copyright
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| 218 | ** notice, this list of conditions and the following disclaimer.
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| 219 | **
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| 220 | ** 2 Redistributions in binary form must reproduce the above copyright
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| 221 | ** notice, this list of conditions and the following disclaimer in
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| 222 | ** the documentation and/or other materials provided with the
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| 223 | ** distribution.
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| 224 | **
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| 225 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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| 226 | ** the International Astronomical Union nor the names of its
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| 227 | ** contributors may be used to endorse or promote products derived
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| 228 | ** from this software without specific prior written permission.
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| 229 | **
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| 230 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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| 231 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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| 232 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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| 233 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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| 234 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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| 235 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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| 236 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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| 237 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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| 238 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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| 239 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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| 240 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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| 241 | ** POSSIBILITY OF SUCH DAMAGE.
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| 242 | **
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| 243 | */
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