1 | #include "slalib.h"
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2 | #include "slamac.h"
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3 | void slaHfk5z ( double rh, double dh, double epoch,
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4 | double *r5, double *d5, double *dr5, double *dd5 )
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5 | /*
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6 | ** - - - - - - - - -
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7 | ** s l a H f k 5 z
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8 | ** - - - - - - - - -
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9 | **
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10 | ** Transform a Hipparcos star position into FK5 J2000, assuming
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11 | ** zero Hipparcos proper motion.
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12 | **
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13 | ** (double precision)
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14 | **
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15 | ** Given:
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16 | ** rh double Hipparcos RA (radians)
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17 | ** dh double Hipparcos Dec (radians)
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18 | ** epoch double Julian epoch (TDB)
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19 | **
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20 | ** Returned (all FK5, equinox J2000, epoch EPOCH):
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21 | ** r5 double RA (radians)
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22 | ** d5 double Dec (radians)
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23 | **
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24 | ** Called: slaDcs2c, slaDav2m, slaDmxv, slaDav2m, slaDmxm,
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25 | ** slaDimxv, slaDvxv, slaDc62s, slaDranrm
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26 | **
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27 | ** Notes:
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28 | **
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29 | ** 1) The proper motion in RA is dRA/dt rather than cos(Dec)*dRA/dt.
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30 | **
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31 | ** 2) The FK5 to Hipparcos transformation consists of a pure
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32 | ** rotation and spin; zonal errors in the FK5 catalogue are
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33 | ** not taken into account.
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34 | **
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35 | ** 3) The published orientation and spin components are interpreted
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36 | ** as "axial vectors". An axial vector points at the pole of the
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37 | ** rotation and its length is the amount of rotation in radians.
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38 | **
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39 | ** 4) It was the intention that Hipparcos should be a close
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40 | ** approximation to an inertial frame, so that distant objects
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41 | ** have zero proper motion; such objects have (in general)
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42 | ** non-zero proper motion in FK5, and this routine returns those
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43 | ** fictitious proper motions.
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44 | **
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45 | ** 5) The position returned by this routine is in the FK5 J2000
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46 | ** reference frame but at the specified epoch.
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47 | **
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48 | ** 6) See also slaFk52h, slaH2fk5, slaFk5zhz.
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49 | **
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50 | ** Reference:
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51 | **
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52 | ** M.Feissel & F.Mignard, Astron. Astrophys. 331, L33-L36 (1998).
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53 | **
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54 | ** Last revision: 30 December 1999
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55 | **
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56 | ** Copyright P.T.Wallace. All rights reserved.
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57 | */
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58 |
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59 | #define AS2R 0.484813681109535994e-5 /* arcseconds to radians */
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60 |
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61 | {
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62 | /* FK5 to Hipparcos orientation and spin (radians, radians/year) */
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63 | static double ortn[3] = { -19.9e-3 * AS2R,
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64 | -9.1e-3 * AS2R,
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65 | 22.9e-3 * AS2R },
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66 | s5[3] = { -0.30e-3 * AS2R,
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67 | 0.60e-3 * AS2R,
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68 | 0.70e-3 * AS2R };
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69 |
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70 | double ph[3], r5h[3][3], sh[3], t, vst[3], rst[3][3], r5ht[3][3],
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71 | pv5e[6], vv[3], w, r, v;
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72 | int i;
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73 |
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74 |
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75 | /* Hipparcos barycentric position vector (normalized). */
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76 | slaDcs2c ( rh, dh, ph );
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77 |
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78 | /* FK5 to Hipparcos orientation matrix. */
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79 | slaDav2m ( ortn, r5h );
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80 |
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81 | /* Rotate the spin vector into the Hipparcos frame. */
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82 | slaDmxv ( r5h, s5, sh );
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83 |
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84 | /* Time interval from J2000 to epoch. */
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85 | t = epoch - 2000.0;
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86 |
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87 | /* Axial vector: accumulated Hipparcos wrt FK5 spin over that interval. */
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88 | for ( i = 0; i < 3; i++ ) {
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89 | vst [ i ] = s5 [ i ] * t;
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90 | }
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91 |
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92 | /* Express the accumulated spin as a rotation matrix. */
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93 | slaDav2m ( vst, rst );
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94 |
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95 | /* Rotation matrix: accumulated spin, then FK5 to Hipparcos. */
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96 | slaDmxm ( r5h, rst, r5ht );
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97 |
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98 | /* De-orient & de-spin the vector into FK5 J2000 at epoch. */
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99 | slaDimxv ( r5ht, ph, pv5e );
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100 | slaDvxv ( sh, ph, vv );
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101 | slaDimxv ( r5ht, vv, pv5e + 3 );
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102 |
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103 | /* FK5 position/velocity 6-vector to spherical. */
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104 | slaDc62s( pv5e, &w, d5, &r, dr5, dd5, &v );
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105 | *r5 = slaDranrm ( w );
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106 | }
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