line |
stmt |
bran |
cond |
sub |
pod |
time |
code |
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#include "erfa.h" |
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void eraFk524(double r2000, double d2000, |
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double dr2000, double dd2000, |
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double p2000, double v2000, |
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double *r1950, double *d1950, |
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double *dr1950, double *dd1950, |
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double *p1950, double *v1950) |
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/* |
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** - - - - - - - - - |
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** e r a F k 5 2 4 |
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** - - - - - - - - - |
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** |
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** Convert J2000.0 FK5 star catalog data to B1950.0 FK4. |
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** |
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** Given: (all J2000.0, FK5) |
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** r2000,d2000 double J2000.0 RA,Dec (rad) |
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** dr2000,dd2000 double J2000.0 proper motions (rad/Jul.yr) |
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** p2000 double parallax (arcsec) |
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** v2000 double radial velocity (km/s, +ve = moving away) |
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** |
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** Returned: (all B1950.0, FK4) |
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** r1950,d1950 double B1950.0 RA,Dec (rad) |
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** dr1950,dd1950 double B1950.0 proper motions (rad/trop.yr) |
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** p1950 double parallax (arcsec) |
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** v1950 double radial velocity (km/s, +ve = moving away) |
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** |
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** Notes: |
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** |
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** 1) The proper motions in RA are dRA/dt rather than cos(Dec)*dRA/dt, |
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** and are per year rather than per century. |
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** |
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** 2) The conversion is somewhat complicated, for several reasons: |
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** |
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** . Change of standard epoch from J2000.0 to B1950.0. |
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** |
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** . An intermediate transition date of 1984 January 1.0 TT. |
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** |
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** . A change of precession model. |
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** |
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** . Change of time unit for proper motion (Julian to tropical). |
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** |
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** . FK4 positions include the E-terms of aberration, to simplify |
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** the hand computation of annual aberration. FK5 positions |
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** assume a rigorous aberration computation based on the Earth's |
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** barycentric velocity. |
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** |
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** . The E-terms also affect proper motions, and in particular cause |
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** objects at large distances to exhibit fictitious proper |
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** motions. |
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** |
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** The algorithm is based on Smith et al. (1989) and Yallop et al. |
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** (1989), which presented a matrix method due to Standish (1982) as |
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** developed by Aoki et al. (1983), using Kinoshita's development of |
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** Andoyer's post-Newcomb precession. The numerical constants from |
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** Seidelmann (1992) are used canonically. |
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** |
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** 4) In the FK4 catalog the proper motions of stars within 10 degrees |
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** of the poles do not embody differential E-terms effects and |
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** should, strictly speaking, be handled in a different manner from |
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** stars outside these regions. However, given the general lack of |
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** homogeneity of the star data available for routine astrometry, |
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** the difficulties of handling positions that may have been |
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** determined from astrometric fields spanning the polar and non- |
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** polar regions, the likelihood that the differential E-terms |
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** effect was not taken into account when allowing for proper motion |
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** in past astrometry, and the undesirability of a discontinuity in |
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** the algorithm, the decision has been made in this ERFA algorithm |
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** to include the effects of differential E-terms on the proper |
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** motions for all stars, whether polar or not. At epoch J2000.0, |
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** and measuring "on the sky" rather than in terms of RA change, the |
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** errors resulting from this simplification are less than |
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** 1 milliarcsecond in position and 1 milliarcsecond per century in |
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** proper motion. |
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** |
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** Called: |
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** eraAnp normalize angle into range 0 to 2pi |
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** eraPdp scalar product of two p-vectors |
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** eraPm modulus of p-vector |
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** eraPmp p-vector minus p-vector |
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** eraPpp p-vector pluus p-vector |
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** eraPv2s pv-vector to spherical coordinates |
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** eraS2pv spherical coordinates to pv-vector |
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** eraSxp multiply p-vector by scalar |
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** |
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** References: |
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** |
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** Aoki, S. et al., 1983, "Conversion matrix of epoch B1950.0 |
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** FK4-based positions of stars to epoch J2000.0 positions in |
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** accordance with the new IAU resolutions". Astron.Astrophys. |
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** 128, 263-267. |
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** |
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** Seidelmann, P.K. (ed), 1992, "Explanatory Supplement to the |
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** Astronomical Almanac", ISBN 0-935702-68-7. |
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** |
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** Smith, C.A. et al., 1989, "The transformation of astrometric |
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** catalog systems to the equinox J2000.0". Astron.J. 97, 265. |
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** |
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** Standish, E.M., 1982, "Conversion of positions and proper motions |
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** from B1950.0 to the IAU system at J2000.0". Astron.Astrophys., |
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** 115, 1, 20-22. |
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** |
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** Yallop, B.D. et al., 1989, "Transformation of mean star places |
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** from FK4 B1950.0 to FK5 J2000.0 using matrices in 6-space". |
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** Astron.J. 97, 274. |
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** |
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** Copyright (C) 2013-2020, NumFOCUS Foundation. |
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** Derived, with permission, from the SOFA library. See notes at end of file. |
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*/ |
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{ |
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/* Radians per year to arcsec per century */ |
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const double PMF = 100.0*ERFA_DR2AS; |
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/* Small number to avoid arithmetic problems */ |
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const double TINY = 1e-30; |
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/* Miscellaneous */ |
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double r, d, ur, ud, px, rv, pxvf, w, rd; |
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int i, j, k, l; |
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/* Vectors, p and pv */ |
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double r0[2][3], r1[2][3], p1[3], p2[3], pv[2][3]; |
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/* |
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** CANONICAL CONSTANTS (Seidelmann 1992) |
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*/ |
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/* Km per sec to AU per tropical century */ |
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/* = 86400 * 36524.2198782 / 149597870.7 */ |
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const double VF = 21.095; |
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/* Constant pv-vector (cf. Seidelmann 3.591-2, vectors A and Adot) */ |
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static double a[2][3] = { |
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{ -1.62557e-6, -0.31919e-6, -0.13843e-6 }, |
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{ +1.245e-3, -1.580e-3, -0.659e-3 } |
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}; |
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/* 3x2 matrix of pv-vectors (cf. Seidelmann 3.592-1, matrix M^-1) */ |
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static double em[2][3][2][3] = { |
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{ { { +0.9999256795, +0.0111814828, +0.0048590039, }, |
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{ -0.00000242389840, -0.00000002710544, -0.00000001177742 } }, |
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{ { -0.0111814828, +0.9999374849, -0.0000271771, }, |
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{ +0.00000002710544, -0.00000242392702, +0.00000000006585 } }, |
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{ { -0.0048590040, -0.0000271557, +0.9999881946, }, |
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{ +0.00000001177742, +0.00000000006585, -0.00000242404995 } } }, |
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{ { { -0.000551, +0.238509, -0.435614, }, |
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{ +0.99990432, +0.01118145, +0.00485852 } }, |
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{ { -0.238560, -0.002667, +0.012254, }, |
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{ -0.01118145, +0.99991613, -0.00002717 } }, |
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{ { +0.435730, -0.008541, +0.002117, }, |
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{ -0.00485852, -0.00002716, +0.99996684 } } } |
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}; |
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/*- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - */ |
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/* The FK5 data (units radians and arcsec per Julian century). */ |
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r = r2000; |
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d = d2000; |
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ur = dr2000*PMF; |
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ud = dd2000*PMF; |
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px = p2000; |
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rv = v2000; |
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/* Express as a pv-vector. */ |
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pxvf = px * VF; |
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w = rv * pxvf; |
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eraS2pv(r, d, 1.0, ur, ud, w, r0); |
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/* Convert pv-vector to Bessel-Newcomb system (cf. Seidelmann 3.592-1). */ |
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for ( i = 0; i < 2; i++ ) { |
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for ( j = 0; j < 3; j++ ) { |
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w = 0.0; |
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for ( k = 0; k < 2; k++ ) { |
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for ( l = 0; l < 3; l++ ) { |
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w += em[i][j][k][l] * r0[k][l]; |
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} |
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} |
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r1[i][j] = w; |
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} |
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} |
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/* Apply E-terms (equivalent to Seidelmann 3.592-3, one iteration). */ |
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/* Direction. */ |
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w = eraPm(r1[0]); |
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eraSxp(eraPdp(r1[0],a[0]), r1[0], p1); |
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eraSxp(w, a[0], p2); |
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eraPmp(p2, p1, p1); |
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eraPpp(r1[0], p1, p1); |
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/* Recompute length. */ |
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w = eraPm(p1); |
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/* Direction. */ |
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0
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eraSxp(eraPdp(r1[0],a[0]), r1[0], p1); |
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eraSxp(w, a[0], p2); |
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eraPmp(p2, p1, p1); |
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eraPpp(r1[0], p1, pv[0]); |
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/* Derivative. */ |
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eraSxp(eraPdp(r1[0],a[1]), pv[0], p1); |
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eraSxp(w, a[1], p2); |
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eraPmp(p2, p1, p1); |
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eraPpp(r1[1], p1, pv[1]); |
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/* Revert to catalog form. */ |
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eraPv2s(pv, &r, &d, &w, &ur, &ud, &rd); |
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if ( px > TINY ) { |
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rv = rd/pxvf; |
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px = px/w; |
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} |
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/* Return the results. */ |
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*r1950 = eraAnp(r); |
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*d1950 = d; |
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*dr1950 = ur/PMF; |
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*dd1950 = ud/PMF; |
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*p1950 = px; |
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*v1950 = rv; |
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/* Finished. */ |
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0
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} |
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/*---------------------------------------------------------------------- |
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** |
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** |
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** Copyright (C) 2013-2020, NumFOCUS Foundation. |
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** All rights reserved. |
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** |
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** This library is derived, with permission, from the International |
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** Astronomical Union's "Standards of Fundamental Astronomy" library, |
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** available from http://www.iausofa.org. |
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** |
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** The ERFA version is intended to retain identical functionality to |
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** the SOFA library, but made distinct through different function and |
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** file names, as set out in the SOFA license conditions. The SOFA |
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** original has a role as a reference standard for the IAU and IERS, |
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** and consequently redistribution is permitted only in its unaltered |
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** state. The ERFA version is not subject to this restriction and |
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** therefore can be included in distributions which do not support the |
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** concept of "read only" software. |
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** |
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** Although the intent is to replicate the SOFA API (other than |
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** replacement of prefix names) and results (with the exception of |
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** bugs; any that are discovered will be fixed), SOFA is not |
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** responsible for any errors found in this version of the library. |
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** |
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** If you wish to acknowledge the SOFA heritage, please acknowledge |
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** that you are using a library derived from SOFA, rather than SOFA |
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** itself. |
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** |
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** |
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** TERMS AND CONDITIONS |
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** |
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** Redistribution and use in source and binary forms, with or without |
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** modification, are permitted provided that the following conditions |
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** are met: |
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** |
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** 1 Redistributions of source code must retain the above copyright |
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** notice, this list of conditions and the following disclaimer. |
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** |
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** 2 Redistributions in binary form must reproduce the above copyright |
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** notice, this list of conditions and the following disclaimer in |
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** the documentation and/or other materials provided with the |
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** distribution. |
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** |
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** 3 Neither the name of the Standards Of Fundamental Astronomy Board, |
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** the International Astronomical Union nor the names of its |
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** contributors may be used to endorse or promote products derived |
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** from this software without specific prior written permission. |
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** |
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** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; |
286
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** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER |
287
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** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
288
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|
|
** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
289
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|
** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
290
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** POSSIBILITY OF SUCH DAMAGE. |
291
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** |
292
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*/ |