| 1 | #include "sofa.h"
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| 2 |
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| 3 | void iauApcs(double date1, double date2, double pv[2][3],
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| 4 | double ebpv[2][3], double ehp[3],
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| 5 | iauASTROM *astrom)
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| 6 | /*
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| 7 | ** - - - - - - - -
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| 8 | ** i a u A p c s
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| 9 | ** - - - - - - - -
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| 10 | **
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| 11 | ** For an observer whose geocentric position and velocity are known,
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| 12 | ** prepare star-independent astrometry parameters for transformations
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| 13 | ** between ICRS and GCRS. The Earth ephemeris is supplied by the
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| 14 | ** caller.
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| 15 | **
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| 16 | ** The parameters produced by this function are required in the space
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| 17 | ** motion, parallax, light deflection and aberration parts of the
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| 18 | ** astrometric transformation chain.
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| 19 | **
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| 20 | ** This function is part of the International Astronomical Union's
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| 21 | ** SOFA (Standards of Fundamental Astronomy) software collection.
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| 22 | **
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| 23 | ** Status: support function.
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| 24 | **
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| 25 | ** Given:
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| 26 | ** date1 double TDB as a 2-part...
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| 27 | ** date2 double ...Julian Date (Note 1)
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| 28 | ** pv double[2][3] observer's geocentric pos/vel (m, m/s)
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| 29 | ** ebpv double[2][3] Earth barycentric PV (au, au/day)
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| 30 | ** ehp double[3] Earth heliocentric P (au)
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| 31 | **
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| 32 | ** Returned:
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| 33 | ** astrom iauASTROM* star-independent astrometry parameters:
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| 34 | ** pmt double PM time interval (SSB, Julian years)
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| 35 | ** eb double[3] SSB to observer (vector, au)
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| 36 | ** eh double[3] Sun to observer (unit vector)
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| 37 | ** em double distance from Sun to observer (au)
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| 38 | ** v double[3] barycentric observer velocity (vector, c)
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| 39 | ** bm1 double sqrt(1-|v|^2): reciprocal of Lorenz factor
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| 40 | ** bpn double[3][3] bias-precession-nutation matrix
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| 41 | ** along double unchanged
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| 42 | ** xpl double unchanged
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| 43 | ** ypl double unchanged
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| 44 | ** sphi double unchanged
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| 45 | ** cphi double unchanged
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| 46 | ** diurab double unchanged
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| 47 | ** eral double unchanged
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| 48 | ** refa double unchanged
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| 49 | ** refb double unchanged
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| 50 | **
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| 51 | ** Notes:
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| 52 | **
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| 53 | ** 1) The TDB date date1+date2 is a Julian Date, apportioned in any
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| 54 | ** convenient way between the two arguments. For example,
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| 55 | ** JD(TDB)=2450123.7 could be expressed in any of these ways, among
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| 56 | ** others:
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| 57 | **
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| 58 | ** date1 date2
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| 59 | **
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| 60 | ** 2450123.7 0.0 (JD method)
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| 61 | ** 2451545.0 -1421.3 (J2000 method)
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| 62 | ** 2400000.5 50123.2 (MJD method)
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| 63 | ** 2450123.5 0.2 (date & time method)
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| 64 | **
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| 65 | ** The JD method is the most natural and convenient to use in cases
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| 66 | ** where the loss of several decimal digits of resolution is
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| 67 | ** acceptable. The J2000 method is best matched to the way the
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| 68 | ** argument is handled internally and will deliver the optimum
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| 69 | ** resolution. The MJD method and the date & time methods are both
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| 70 | ** good compromises between resolution and convenience. For most
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| 71 | ** applications of this function the choice will not be at all
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| 72 | ** critical.
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| 73 | **
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| 74 | ** TT can be used instead of TDB without any significant impact on
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| 75 | ** accuracy.
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| 76 | **
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| 77 | ** 2) All the vectors are with respect to BCRS axes.
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| 78 | **
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| 79 | ** 3) Providing separate arguments for (i) the observer's geocentric
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| 80 | ** position and velocity and (ii) the Earth ephemeris is done for
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| 81 | ** convenience in the geocentric, terrestrial and Earth orbit cases.
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| 82 | ** For deep space applications it maybe more convenient to specify
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| 83 | ** zero geocentric position and velocity and to supply the
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| 84 | ** observer's position and velocity information directly instead of
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| 85 | ** with respect to the Earth. However, note the different units:
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| 86 | ** m and m/s for the geocentric vectors, au and au/day for the
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| 87 | ** heliocentric and barycentric vectors.
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| 88 | **
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| 89 | ** 4) In cases where the caller does not wish to provide the Earth
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| 90 | ** ephemeris, the function iauApcs13 can be used instead of the
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| 91 | ** present function. This computes the Earth ephemeris using the
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| 92 | ** SOFA function iauEpv00.
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| 93 | **
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| 94 | ** 5) This is one of several functions that inserts into the astrom
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| 95 | ** structure star-independent parameters needed for the chain of
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| 96 | ** astrometric transformations ICRS <-> GCRS <-> CIRS <-> observed.
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| 97 | **
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| 98 | ** The various functions support different classes of observer and
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| 99 | ** portions of the transformation chain:
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| 100 | **
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| 101 | ** functions observer transformation
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| 102 | **
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| 103 | ** iauApcg iauApcg13 geocentric ICRS <-> GCRS
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| 104 | ** iauApci iauApci13 terrestrial ICRS <-> CIRS
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| 105 | ** iauApco iauApco13 terrestrial ICRS <-> observed
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| 106 | ** iauApcs iauApcs13 space ICRS <-> GCRS
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| 107 | ** iauAper iauAper13 terrestrial update Earth rotation
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| 108 | ** iauApio iauApio13 terrestrial CIRS <-> observed
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| 109 | **
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| 110 | ** Those with names ending in "13" use contemporary SOFA models to
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| 111 | ** compute the various ephemerides. The others accept ephemerides
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| 112 | ** supplied by the caller.
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| 113 | **
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| 114 | ** The transformation from ICRS to GCRS covers space motion,
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| 115 | ** parallax, light deflection, and aberration. From GCRS to CIRS
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| 116 | ** comprises frame bias and precession-nutation. From CIRS to
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| 117 | ** observed takes account of Earth rotation, polar motion, diurnal
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| 118 | ** aberration and parallax (unless subsumed into the ICRS <-> GCRS
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| 119 | ** transformation), and atmospheric refraction.
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| 120 | **
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| 121 | ** 6) The context structure astrom produced by this function is used by
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| 122 | ** iauAtciq* and iauAticq*.
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| 123 | **
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| 124 | ** Called:
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| 125 | ** iauCp copy p-vector
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| 126 | ** iauPm modulus of p-vector
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| 127 | ** iauPn decompose p-vector into modulus and direction
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| 128 | ** iauIr initialize r-matrix to identity
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| 129 | **
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| 130 | ** This revision: 2013 October 9
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| 131 | **
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| 132 | ** SOFA release 2015-02-09
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| 133 | **
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| 134 | ** Copyright (C) 2015 IAU SOFA Board. See notes at end.
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| 135 | */
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| 136 | {
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| 137 | /* au/d to m/s */
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| 138 | const double AUDMS = DAU/DAYSEC;
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| 139 |
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| 140 | /* Light time for 1 AU (day) */
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| 141 | const double CR = AULT/DAYSEC;
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| 142 |
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| 143 | int i;
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| 144 | double dp, dv, pb[3], vb[3], ph[3], v2, w;
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| 145 |
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| 146 | /* Time since reference epoch, years (for proper motion calculation). */
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| 147 | astrom->pmt = ( (date1 - DJ00) + date2 ) / DJY;
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| 148 |
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| 149 | /* Adjust Earth ephemeris to observer. */
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| 150 | for (i = 0; i < 3; i++) {
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| 151 | dp = pv[0][i] / DAU;
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| 152 | dv = pv[1][i] / AUDMS;
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| 153 | pb[i] = ebpv[0][i] + dp;
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| 154 | vb[i] = ebpv[1][i] + dv;
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| 155 | ph[i] = ehp[i] + dp;
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| 156 | }
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| 157 |
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| 158 | /* Barycentric position of observer (au). */
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| 159 | iauCp(pb, astrom->eb);
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| 160 |
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| 161 | /* Heliocentric direction and distance (unit vector and au). */
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| 162 | iauPn(ph, &astrom->em, astrom->eh);
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| 163 |
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| 164 | /* Barycentric vel. in units of c, and reciprocal of Lorenz factor. */
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| 165 | v2 = 0.0;
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| 166 | for (i = 0; i < 3; i++) {
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| 167 | w = vb[i] * CR;
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| 168 | astrom->v[i] = w;
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| 169 | v2 += w*w;
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| 170 | }
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| 171 | astrom->bm1 = sqrt(1.0 - v2);
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| 172 |
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| 173 | /* Reset the NPB matrix. */
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| 174 | iauIr(astrom->bpn);
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| 175 |
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| 176 | /* Finished. */
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| 177 |
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| 178 | /*----------------------------------------------------------------------
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| 179 | **
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| 180 | ** Copyright (C) 2015
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| 181 | ** Standards Of Fundamental Astronomy Board
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| 182 | ** of the International Astronomical Union.
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| 183 | **
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| 184 | ** =====================
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| 185 | ** SOFA Software License
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| 186 | ** =====================
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| 187 | **
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| 188 | ** NOTICE TO USER:
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| 189 | **
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| 190 | ** BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING SIX TERMS AND
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| 191 | ** CONDITIONS WHICH APPLY TO ITS USE.
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| 192 | **
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| 193 | ** 1. The Software is owned by the IAU SOFA Board ("SOFA").
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| 194 | **
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| 195 | ** 2. Permission is granted to anyone to use the SOFA software for any
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| 196 | ** purpose, including commercial applications, free of charge and
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| 197 | ** without payment of royalties, subject to the conditions and
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| 198 | ** restrictions listed below.
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| 199 | **
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| 200 | ** 3. You (the user) may copy and distribute SOFA source code to others,
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| 201 | ** and use and adapt its code and algorithms in your own software,
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| 202 | ** on a world-wide, royalty-free basis. That portion of your
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| 203 | ** distribution that does not consist of intact and unchanged copies
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| 204 | ** of SOFA source code files is a "derived work" that must comply
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| 205 | ** with the following requirements:
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| 206 | **
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| 207 | ** a) Your work shall be marked or carry a statement that it
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| 208 | ** (i) uses routines and computations derived by you from
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| 209 | ** software provided by SOFA under license to you; and
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| 210 | ** (ii) does not itself constitute software provided by and/or
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| 211 | ** endorsed by SOFA.
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| 212 | **
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| 213 | ** b) The source code of your derived work must contain descriptions
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| 214 | ** of how the derived work is based upon, contains and/or differs
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| 215 | ** from the original SOFA software.
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| 216 | **
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| 217 | ** c) The names of all routines in your derived work shall not
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| 218 | ** include the prefix "iau" or "sofa" or trivial modifications
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| 219 | ** thereof such as changes of case.
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| 220 | **
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| 221 | ** d) The origin of the SOFA components of your derived work must
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| 222 | ** not be misrepresented; you must not claim that you wrote the
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| 223 | ** original software, nor file a patent application for SOFA
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| 224 | ** software or algorithms embedded in the SOFA software.
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| 225 | **
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| 226 | ** e) These requirements must be reproduced intact in any source
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| 227 | ** distribution and shall apply to anyone to whom you have
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| 228 | ** granted a further right to modify the source code of your
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| 229 | ** derived work.
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| 230 | **
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| 231 | ** Note that, as originally distributed, the SOFA software is
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| 232 | ** intended to be a definitive implementation of the IAU standards,
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| 233 | ** and consequently third-party modifications are discouraged. All
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| 234 | ** variations, no matter how minor, must be explicitly marked as
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| 235 | ** such, as explained above.
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| 236 | **
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| 237 | ** 4. You shall not cause the SOFA software to be brought into
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| 238 | ** disrepute, either by misuse, or use for inappropriate tasks, or
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| 239 | ** by inappropriate modification.
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| 240 | **
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| 241 | ** 5. The SOFA software is provided "as is" and SOFA makes no warranty
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| 242 | ** as to its use or performance. SOFA does not and cannot warrant
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| 243 | ** the performance or results which the user may obtain by using the
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| 244 | ** SOFA software. SOFA makes no warranties, express or implied, as
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| 245 | ** to non-infringement of third party rights, merchantability, or
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| 246 | ** fitness for any particular purpose. In no event will SOFA be
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| 247 | ** liable to the user for any consequential, incidental, or special
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| 248 | ** damages, including any lost profits or lost savings, even if a
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| 249 | ** SOFA representative has been advised of such damages, or for any
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| 250 | ** claim by any third party.
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| 251 | **
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| 252 | ** 6. The provision of any version of the SOFA software under the terms
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| 253 | ** and conditions specified herein does not imply that future
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| 254 | ** versions will also be made available under the same terms and
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| 255 | ** conditions.
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| 256 | *
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| 257 | ** In any published work or commercial product which uses the SOFA
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| 258 | ** software directly, acknowledgement (see www.iausofa.org) is
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| 259 | ** appreciated.
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| 260 | **
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| 261 | ** Correspondence concerning SOFA software should be addressed as
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| 262 | ** follows:
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| 263 | **
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| 264 | ** By email: sofa@ukho.gov.uk
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| 265 | ** By post: IAU SOFA Center
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| 266 | ** HM Nautical Almanac Office
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| 267 | ** UK Hydrographic Office
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| 268 | ** Admiralty Way, Taunton
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| 269 | ** Somerset, TA1 2DN
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| 270 | ** United Kingdom
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| 271 | **
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| 272 | **--------------------------------------------------------------------*/
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| 273 |
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| 274 | }
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