1 | #include "erfa.h"
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2 |
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3 | int eraPvstar(double pv[2][3], double *ra, double *dec,
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4 | double *pmr, double *pmd, double *px, double *rv)
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5 | /*
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6 | ** - - - - - - - - - -
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7 | ** e r a P v s t a r
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8 | ** - - - - - - - - - -
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9 | **
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10 | ** Convert star position+velocity vector to catalog coordinates.
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11 | **
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12 | ** Given (Note 1):
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13 | ** pv double[2][3] pv-vector (au, au/day)
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14 | **
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15 | ** Returned (Note 2):
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16 | ** ra double right ascension (radians)
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17 | ** dec double declination (radians)
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18 | ** pmr double RA proper motion (radians/year)
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19 | ** pmd double Dec proper motion (radians/year)
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20 | ** px double parallax (arcsec)
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21 | ** rv double radial velocity (km/s, positive = receding)
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22 | **
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23 | ** Returned (function value):
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24 | ** int status:
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25 | ** 0 = OK
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26 | ** -1 = superluminal speed (Note 5)
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27 | ** -2 = null position vector
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28 | **
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29 | ** Notes:
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30 | **
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31 | ** 1) The specified pv-vector is the coordinate direction (and its rate
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32 | ** of change) for the date at which the light leaving the star
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33 | ** reached the solar-system barycenter.
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34 | **
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35 | ** 2) The star data returned by this function are "observables" for an
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36 | ** imaginary observer at the solar-system barycenter. Proper motion
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37 | ** and radial velocity are, strictly, in terms of barycentric
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38 | ** coordinate time, TCB. For most practical applications, it is
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39 | ** permissible to neglect the distinction between TCB and ordinary
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40 | ** "proper" time on Earth (TT/TAI). The result will, as a rule, be
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41 | ** limited by the intrinsic accuracy of the proper-motion and
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42 | ** radial-velocity data; moreover, the supplied pv-vector is likely
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43 | ** to be merely an intermediate result (for example generated by the
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44 | ** function eraStarpv), so that a change of time unit will cancel
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45 | ** out overall.
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46 | **
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47 | ** In accordance with normal star-catalog conventions, the object's
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48 | ** right ascension and declination are freed from the effects of
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49 | ** secular aberration. The frame, which is aligned to the catalog
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50 | ** equator and equinox, is Lorentzian and centered on the SSB.
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51 | **
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52 | ** Summarizing, the specified pv-vector is for most stars almost
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53 | ** identical to the result of applying the standard geometrical
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54 | ** "space motion" transformation to the catalog data. The
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55 | ** differences, which are the subject of the Stumpff paper cited
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56 | ** below, are:
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57 | **
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58 | ** (i) In stars with significant radial velocity and proper motion,
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59 | ** the constantly changing light-time distorts the apparent proper
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60 | ** motion. Note that this is a classical, not a relativistic,
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61 | ** effect.
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62 | **
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63 | ** (ii) The transformation complies with special relativity.
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64 | **
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65 | ** 3) Care is needed with units. The star coordinates are in radians
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66 | ** and the proper motions in radians per Julian year, but the
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67 | ** parallax is in arcseconds; the radial velocity is in km/s, but
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68 | ** the pv-vector result is in au and au/day.
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69 | **
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70 | ** 4) The proper motions are the rate of change of the right ascension
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71 | ** and declination at the catalog epoch and are in radians per Julian
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72 | ** year. The RA proper motion is in terms of coordinate angle, not
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73 | ** true angle, and will thus be numerically larger at high
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74 | ** declinations.
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75 | **
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76 | ** 5) Straight-line motion at constant speed in the inertial frame is
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77 | ** assumed. If the speed is greater than or equal to the speed of
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78 | ** light, the function aborts with an error status.
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79 | **
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80 | ** 6) The inverse transformation is performed by the function eraStarpv.
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81 | **
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82 | ** Called:
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83 | ** eraPn decompose p-vector into modulus and direction
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84 | ** eraPdp scalar product of two p-vectors
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85 | ** eraSxp multiply p-vector by scalar
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86 | ** eraPmp p-vector minus p-vector
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87 | ** eraPm modulus of p-vector
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88 | ** eraPpp p-vector plus p-vector
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89 | ** eraPv2s pv-vector to spherical
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90 | ** eraAnp normalize angle into range 0 to 2pi
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91 | **
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92 | ** Reference:
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93 | **
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94 | ** Stumpff, P., 1985, Astron.Astrophys. 144, 232-240.
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95 | **
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96 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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97 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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98 | */
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99 | {
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100 | double r, x[3], vr, ur[3], vt, ut[3], bett, betr, d, w, del,
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101 | usr[3], ust[3], a, rad, decd, rd;
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102 |
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103 |
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104 | /* Isolate the radial component of the velocity (au/day, inertial). */
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105 | eraPn(pv[0], &r, x);
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106 | vr = eraPdp(x, pv[1]);
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107 | eraSxp(vr, x, ur);
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108 |
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109 | /* Isolate the transverse component of the velocity (au/day, inertial). */
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110 | eraPmp(pv[1], ur, ut);
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111 | vt = eraPm(ut);
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112 |
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113 | /* Special-relativity dimensionless parameters. */
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114 | bett = vt / ERFA_DC;
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115 | betr = vr / ERFA_DC;
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116 |
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117 | /* The inertial-to-observed correction terms. */
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118 | d = 1.0 + betr;
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119 | w = betr*betr + bett*bett;
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120 | if (d == 0.0 || w > 1.0) return -1;
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121 | del = - w / (sqrt(1.0-w) + 1.0);
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122 |
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123 | /* Apply relativistic correction factor to radial velocity component. */
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124 | w = (betr != 0) ? (betr - del) / (betr * d) : 1.0;
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125 | eraSxp(w, ur, usr);
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126 |
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127 | /* Apply relativistic correction factor to tangential velocity */
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128 | /* component. */
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129 | eraSxp(1.0/d, ut, ust);
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130 |
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131 | /* Combine the two to obtain the observed velocity vector (au/day). */
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132 | eraPpp(usr, ust, pv[1]);
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133 |
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134 | /* Cartesian to spherical. */
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135 | eraPv2s(pv, &a, dec, &r, &rad, &decd, &rd);
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136 | if (r == 0.0) return -2;
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137 |
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138 | /* Return RA in range 0 to 2pi. */
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139 | *ra = eraAnp(a);
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140 |
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141 | /* Return proper motions in radians per year. */
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142 | *pmr = rad * ERFA_DJY;
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143 | *pmd = decd * ERFA_DJY;
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144 |
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145 | /* Return parallax in arcsec. */
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146 | *px = ERFA_DR2AS / r;
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147 |
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148 | /* Return radial velocity in km/s. */
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149 | *rv = 1e-3 * rd * ERFA_DAU / ERFA_DAYSEC;
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150 |
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151 | /* OK status. */
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152 | return 0;
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153 |
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154 | }
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155 | /*----------------------------------------------------------------------
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156 | **
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157 | **
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158 | ** Copyright (C) 2013-2017, NumFOCUS Foundation.
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159 | ** All rights reserved.
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160 | **
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161 | ** This library is derived, with permission, from the International
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162 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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163 | ** available from http://www.iausofa.org.
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164 | **
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165 | ** The ERFA version is intended to retain identical functionality to
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166 | ** the SOFA library, but made distinct through different function and
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167 | ** file names, as set out in the SOFA license conditions. The SOFA
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168 | ** original has a role as a reference standard for the IAU and IERS,
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169 | ** and consequently redistribution is permitted only in its unaltered
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170 | ** state. The ERFA version is not subject to this restriction and
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171 | ** therefore can be included in distributions which do not support the
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172 | ** concept of "read only" software.
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173 | **
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174 | ** Although the intent is to replicate the SOFA API (other than
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175 | ** replacement of prefix names) and results (with the exception of
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176 | ** bugs; any that are discovered will be fixed), SOFA is not
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177 | ** responsible for any errors found in this version of the library.
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178 | **
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179 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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180 | ** that you are using a library derived from SOFA, rather than SOFA
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181 | ** itself.
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182 | **
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183 | **
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184 | ** TERMS AND CONDITIONS
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185 | **
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186 | ** Redistribution and use in source and binary forms, with or without
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187 | ** modification, are permitted provided that the following conditions
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188 | ** are met:
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189 | **
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190 | ** 1 Redistributions of source code must retain the above copyright
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191 | ** notice, this list of conditions and the following disclaimer.
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192 | **
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193 | ** 2 Redistributions in binary form must reproduce the above copyright
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194 | ** notice, this list of conditions and the following disclaimer in
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195 | ** the documentation and/or other materials provided with the
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196 | ** distribution.
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197 | **
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198 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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199 | ** the International Astronomical Union nor the names of its
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200 | ** contributors may be used to endorse or promote products derived
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201 | ** from this software without specific prior written permission.
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202 | **
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203 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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204 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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205 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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206 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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207 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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208 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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209 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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210 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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211 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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212 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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213 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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214 | ** POSSIBILITY OF SUCH DAMAGE.
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215 | **
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216 | */
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