1 | #include "erfa.h"
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2 |
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3 | double eraS00(double date1, double date2, double x, double y)
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4 | /*
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5 | ** - - - - - - -
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6 | ** e r a S 0 0
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7 | ** - - - - - - -
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8 | **
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9 | ** The CIO locator s, positioning the Celestial Intermediate Origin on
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10 | ** the equator of the Celestial Intermediate Pole, given the CIP's X,Y
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11 | ** coordinates. Compatible with IAU 2000A precession-nutation.
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12 | **
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13 | ** Given:
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14 | ** date1,date2 double TT as a 2-part Julian Date (Note 1)
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15 | ** x,y double CIP coordinates (Note 3)
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16 | **
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17 | ** Returned (function value):
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18 | ** double the CIO locator s in radians (Note 2)
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19 | **
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20 | ** Notes:
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21 | **
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22 | ** 1) The TT date date1+date2 is a Julian Date, apportioned in any
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23 | ** convenient way between the two arguments. For example,
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24 | ** JD(TT)=2450123.7 could be expressed in any of these ways,
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25 | ** among others:
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26 | **
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27 | ** date1 date2
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28 | **
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29 | ** 2450123.7 0.0 (JD method)
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30 | ** 2451545.0 -1421.3 (J2000 method)
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31 | ** 2400000.5 50123.2 (MJD method)
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32 | ** 2450123.5 0.2 (date & time method)
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33 | **
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34 | ** The JD method is the most natural and convenient to use in
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35 | ** cases where the loss of several decimal digits of resolution
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36 | ** is acceptable. The J2000 method is best matched to the way
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37 | ** the argument is handled internally and will deliver the
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38 | ** optimum resolution. The MJD method and the date & time methods
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39 | ** are both good compromises between resolution and convenience.
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40 | **
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41 | ** 2) The CIO locator s is the difference between the right ascensions
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42 | ** of the same point in two systems: the two systems are the GCRS
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43 | ** and the CIP,CIO, and the point is the ascending node of the
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44 | ** CIP equator. The quantity s remains below 0.1 arcsecond
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45 | ** throughout 1900-2100.
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46 | **
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47 | ** 3) The series used to compute s is in fact for s+XY/2, where X and Y
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48 | ** are the x and y components of the CIP unit vector; this series
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49 | ** is more compact than a direct series for s would be. This
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50 | ** function requires X,Y to be supplied by the caller, who is
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51 | ** responsible for providing values that are consistent with the
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52 | ** supplied date.
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53 | **
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54 | ** 4) The model is consistent with the IAU 2000A precession-nutation.
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55 | **
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56 | ** Called:
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57 | ** eraFal03 mean anomaly of the Moon
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58 | ** eraFalp03 mean anomaly of the Sun
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59 | ** eraFaf03 mean argument of the latitude of the Moon
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60 | ** eraFad03 mean elongation of the Moon from the Sun
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61 | ** eraFaom03 mean longitude of the Moon's ascending node
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62 | ** eraFave03 mean longitude of Venus
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63 | ** eraFae03 mean longitude of Earth
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64 | ** eraFapa03 general accumulated precession in longitude
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65 | **
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66 | ** References:
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67 | **
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68 | ** Capitaine, N., Chapront, J., Lambert, S. and Wallace, P.,
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69 | ** "Expressions for the Celestial Intermediate Pole and Celestial
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70 | ** Ephemeris Origin consistent with the IAU 2000A precession-
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71 | ** nutation model", Astron.Astrophys. 400, 1145-1154 (2003)
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72 | **
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73 | ** n.b. The celestial ephemeris origin (CEO) was renamed "celestial
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74 | ** intermediate origin" (CIO) by IAU 2006 Resolution 2.
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75 | **
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76 | ** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
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77 | ** IERS Technical Note No. 32, BKG (2004)
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78 | **
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79 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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80 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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81 | */
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82 | {
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83 | /* Time since J2000.0, in Julian centuries */
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84 | double t;
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85 |
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86 | /* Miscellaneous */
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87 | int i, j;
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88 | double a, w0, w1, w2, w3, w4, w5;
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89 |
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90 | /* Fundamental arguments */
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91 | double fa[8];
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92 |
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93 | /* Returned value */
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94 | double s;
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95 |
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96 | /* --------------------- */
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97 | /* The series for s+XY/2 */
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98 | /* --------------------- */
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99 |
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100 | typedef struct {
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101 | int nfa[8]; /* coefficients of l,l',F,D,Om,LVe,LE,pA */
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102 | double s, c; /* sine and cosine coefficients */
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103 | } TERM;
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104 |
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105 | /* Polynomial coefficients */
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106 | static const double sp[] = {
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107 |
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108 | /* 1-6 */
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109 | 94.00e-6,
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110 | 3808.35e-6,
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111 | -119.94e-6,
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112 | -72574.09e-6,
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113 | 27.70e-6,
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114 | 15.61e-6
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115 | };
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116 |
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117 | /* Terms of order t^0 */
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118 | static const TERM s0[] = {
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119 |
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120 | /* 1-10 */
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121 | {{ 0, 0, 0, 0, 1, 0, 0, 0}, -2640.73e-6, 0.39e-6 },
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122 | {{ 0, 0, 0, 0, 2, 0, 0, 0}, -63.53e-6, 0.02e-6 },
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123 | {{ 0, 0, 2, -2, 3, 0, 0, 0}, -11.75e-6, -0.01e-6 },
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124 | {{ 0, 0, 2, -2, 1, 0, 0, 0}, -11.21e-6, -0.01e-6 },
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125 | {{ 0, 0, 2, -2, 2, 0, 0, 0}, 4.57e-6, 0.00e-6 },
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126 | {{ 0, 0, 2, 0, 3, 0, 0, 0}, -2.02e-6, 0.00e-6 },
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127 | {{ 0, 0, 2, 0, 1, 0, 0, 0}, -1.98e-6, 0.00e-6 },
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128 | {{ 0, 0, 0, 0, 3, 0, 0, 0}, 1.72e-6, 0.00e-6 },
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129 | {{ 0, 1, 0, 0, 1, 0, 0, 0}, 1.41e-6, 0.01e-6 },
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130 | {{ 0, 1, 0, 0, -1, 0, 0, 0}, 1.26e-6, 0.01e-6 },
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131 |
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132 | /* 11-20 */
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133 | {{ 1, 0, 0, 0, -1, 0, 0, 0}, 0.63e-6, 0.00e-6 },
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134 | {{ 1, 0, 0, 0, 1, 0, 0, 0}, 0.63e-6, 0.00e-6 },
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135 | {{ 0, 1, 2, -2, 3, 0, 0, 0}, -0.46e-6, 0.00e-6 },
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136 | {{ 0, 1, 2, -2, 1, 0, 0, 0}, -0.45e-6, 0.00e-6 },
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137 | {{ 0, 0, 4, -4, 4, 0, 0, 0}, -0.36e-6, 0.00e-6 },
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138 | {{ 0, 0, 1, -1, 1, -8, 12, 0}, 0.24e-6, 0.12e-6 },
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139 | {{ 0, 0, 2, 0, 0, 0, 0, 0}, -0.32e-6, 0.00e-6 },
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140 | {{ 0, 0, 2, 0, 2, 0, 0, 0}, -0.28e-6, 0.00e-6 },
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141 | {{ 1, 0, 2, 0, 3, 0, 0, 0}, -0.27e-6, 0.00e-6 },
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142 | {{ 1, 0, 2, 0, 1, 0, 0, 0}, -0.26e-6, 0.00e-6 },
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143 |
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144 | /* 21-30 */
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145 | {{ 0, 0, 2, -2, 0, 0, 0, 0}, 0.21e-6, 0.00e-6 },
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146 | {{ 0, 1, -2, 2, -3, 0, 0, 0}, -0.19e-6, 0.00e-6 },
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147 | {{ 0, 1, -2, 2, -1, 0, 0, 0}, -0.18e-6, 0.00e-6 },
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148 | {{ 0, 0, 0, 0, 0, 8,-13, -1}, 0.10e-6, -0.05e-6 },
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149 | {{ 0, 0, 0, 2, 0, 0, 0, 0}, -0.15e-6, 0.00e-6 },
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150 | {{ 2, 0, -2, 0, -1, 0, 0, 0}, 0.14e-6, 0.00e-6 },
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151 | {{ 0, 1, 2, -2, 2, 0, 0, 0}, 0.14e-6, 0.00e-6 },
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152 | {{ 1, 0, 0, -2, 1, 0, 0, 0}, -0.14e-6, 0.00e-6 },
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153 | {{ 1, 0, 0, -2, -1, 0, 0, 0}, -0.14e-6, 0.00e-6 },
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154 | {{ 0, 0, 4, -2, 4, 0, 0, 0}, -0.13e-6, 0.00e-6 },
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155 |
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156 | /* 31-33 */
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157 | {{ 0, 0, 2, -2, 4, 0, 0, 0}, 0.11e-6, 0.00e-6 },
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158 | {{ 1, 0, -2, 0, -3, 0, 0, 0}, -0.11e-6, 0.00e-6 },
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159 | {{ 1, 0, -2, 0, -1, 0, 0, 0}, -0.11e-6, 0.00e-6 }
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160 | };
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161 |
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162 | /* Terms of order t^1 */
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163 | static const TERM s1[] ={
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164 |
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165 | /* 1-3 */
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166 | {{ 0, 0, 0, 0, 2, 0, 0, 0}, -0.07e-6, 3.57e-6 },
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167 | {{ 0, 0, 0, 0, 1, 0, 0, 0}, 1.71e-6, -0.03e-6 },
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168 | {{ 0, 0, 2, -2, 3, 0, 0, 0}, 0.00e-6, 0.48e-6 }
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169 | };
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170 |
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171 | /* Terms of order t^2 */
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172 | static const TERM s2[] ={
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173 |
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174 | /* 1-10 */
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175 | {{ 0, 0, 0, 0, 1, 0, 0, 0}, 743.53e-6, -0.17e-6 },
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176 | {{ 0, 0, 2, -2, 2, 0, 0, 0}, 56.91e-6, 0.06e-6 },
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177 | {{ 0, 0, 2, 0, 2, 0, 0, 0}, 9.84e-6, -0.01e-6 },
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178 | {{ 0, 0, 0, 0, 2, 0, 0, 0}, -8.85e-6, 0.01e-6 },
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179 | {{ 0, 1, 0, 0, 0, 0, 0, 0}, -6.38e-6, -0.05e-6 },
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180 | {{ 1, 0, 0, 0, 0, 0, 0, 0}, -3.07e-6, 0.00e-6 },
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181 | {{ 0, 1, 2, -2, 2, 0, 0, 0}, 2.23e-6, 0.00e-6 },
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182 | {{ 0, 0, 2, 0, 1, 0, 0, 0}, 1.67e-6, 0.00e-6 },
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183 | {{ 1, 0, 2, 0, 2, 0, 0, 0}, 1.30e-6, 0.00e-6 },
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184 | {{ 0, 1, -2, 2, -2, 0, 0, 0}, 0.93e-6, 0.00e-6 },
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185 |
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186 | /* 11-20 */
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187 | {{ 1, 0, 0, -2, 0, 0, 0, 0}, 0.68e-6, 0.00e-6 },
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188 | {{ 0, 0, 2, -2, 1, 0, 0, 0}, -0.55e-6, 0.00e-6 },
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189 | {{ 1, 0, -2, 0, -2, 0, 0, 0}, 0.53e-6, 0.00e-6 },
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190 | {{ 0, 0, 0, 2, 0, 0, 0, 0}, -0.27e-6, 0.00e-6 },
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191 | {{ 1, 0, 0, 0, 1, 0, 0, 0}, -0.27e-6, 0.00e-6 },
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192 | {{ 1, 0, -2, -2, -2, 0, 0, 0}, -0.26e-6, 0.00e-6 },
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193 | {{ 1, 0, 0, 0, -1, 0, 0, 0}, -0.25e-6, 0.00e-6 },
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194 | {{ 1, 0, 2, 0, 1, 0, 0, 0}, 0.22e-6, 0.00e-6 },
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195 | {{ 2, 0, 0, -2, 0, 0, 0, 0}, -0.21e-6, 0.00e-6 },
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196 | {{ 2, 0, -2, 0, -1, 0, 0, 0}, 0.20e-6, 0.00e-6 },
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197 |
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198 | /* 21-25 */
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199 | {{ 0, 0, 2, 2, 2, 0, 0, 0}, 0.17e-6, 0.00e-6 },
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200 | {{ 2, 0, 2, 0, 2, 0, 0, 0}, 0.13e-6, 0.00e-6 },
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201 | {{ 2, 0, 0, 0, 0, 0, 0, 0}, -0.13e-6, 0.00e-6 },
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202 | {{ 1, 0, 2, -2, 2, 0, 0, 0}, -0.12e-6, 0.00e-6 },
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203 | {{ 0, 0, 2, 0, 0, 0, 0, 0}, -0.11e-6, 0.00e-6 }
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204 | };
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205 |
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206 | /* Terms of order t^3 */
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207 | static const TERM s3[] ={
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208 |
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209 | /* 1-4 */
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210 | {{ 0, 0, 0, 0, 1, 0, 0, 0}, 0.30e-6, -23.51e-6 },
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211 | {{ 0, 0, 2, -2, 2, 0, 0, 0}, -0.03e-6, -1.39e-6 },
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212 | {{ 0, 0, 2, 0, 2, 0, 0, 0}, -0.01e-6, -0.24e-6 },
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213 | {{ 0, 0, 0, 0, 2, 0, 0, 0}, 0.00e-6, 0.22e-6 }
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214 | };
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215 |
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216 | /* Terms of order t^4 */
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217 | static const TERM s4[] ={
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218 |
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219 | /* 1-1 */
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220 | {{ 0, 0, 0, 0, 1, 0, 0, 0}, -0.26e-6, -0.01e-6 }
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221 | };
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222 |
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223 | /* Number of terms in the series */
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224 | const int NS0 = (int) (sizeof s0 / sizeof (TERM));
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225 | const int NS1 = (int) (sizeof s1 / sizeof (TERM));
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226 | const int NS2 = (int) (sizeof s2 / sizeof (TERM));
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227 | const int NS3 = (int) (sizeof s3 / sizeof (TERM));
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228 | const int NS4 = (int) (sizeof s4 / sizeof (TERM));
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229 |
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230 | /*--------------------------------------------------------------------*/
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231 |
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232 | /* Interval between fundamental epoch J2000.0 and current date (JC). */
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233 | t = ((date1 - ERFA_DJ00) + date2) / ERFA_DJC;
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234 |
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235 | /* Fundamental Arguments (from IERS Conventions 2003) */
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236 |
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237 | /* Mean anomaly of the Moon. */
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238 | fa[0] = eraFal03(t);
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239 |
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240 | /* Mean anomaly of the Sun. */
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241 | fa[1] = eraFalp03(t);
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242 |
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243 | /* Mean longitude of the Moon minus that of the ascending node. */
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244 | fa[2] = eraFaf03(t);
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245 |
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246 | /* Mean elongation of the Moon from the Sun. */
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247 | fa[3] = eraFad03(t);
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248 |
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249 | /* Mean longitude of the ascending node of the Moon. */
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250 | fa[4] = eraFaom03(t);
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251 |
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252 | /* Mean longitude of Venus. */
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253 | fa[5] = eraFave03(t);
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254 |
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255 | /* Mean longitude of Earth. */
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256 | fa[6] = eraFae03(t);
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257 |
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258 | /* General precession in longitude. */
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259 | fa[7] = eraFapa03(t);
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260 |
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261 | /* Evaluate s. */
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262 | w0 = sp[0];
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263 | w1 = sp[1];
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264 | w2 = sp[2];
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265 | w3 = sp[3];
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266 | w4 = sp[4];
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267 | w5 = sp[5];
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268 |
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269 | for (i = NS0-1; i >= 0; i--) {
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270 | a = 0.0;
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271 | for (j = 0; j < 8; j++) {
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272 | a += (double)s0[i].nfa[j] * fa[j];
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273 | }
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274 | w0 += s0[i].s * sin(a) + s0[i].c * cos(a);
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275 | }
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276 |
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277 | for (i = NS1-1; i >= 0; i--) {
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278 | a = 0.0;
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279 | for (j = 0; j < 8; j++) {
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280 | a += (double)s1[i].nfa[j] * fa[j];
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281 | }
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282 | w1 += s1[i].s * sin(a) + s1[i].c * cos(a);
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283 | }
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284 |
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285 | for (i = NS2-1; i >= 0; i--) {
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286 | a = 0.0;
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287 | for (j = 0; j < 8; j++) {
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288 | a += (double)s2[i].nfa[j] * fa[j];
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289 | }
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290 | w2 += s2[i].s * sin(a) + s2[i].c * cos(a);
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291 | }
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292 |
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293 | for (i = NS3-1; i >= 0; i--) {
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294 | a = 0.0;
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295 | for (j = 0; j < 8; j++) {
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296 | a += (double)s3[i].nfa[j] * fa[j];
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297 | }
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298 | w3 += s3[i].s * sin(a) + s3[i].c * cos(a);
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299 | }
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300 |
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301 | for (i = NS4-1; i >= 0; i--) {
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302 | a = 0.0;
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303 | for (j = 0; j < 8; j++) {
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304 | a += (double)s4[i].nfa[j] * fa[j];
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305 | }
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306 | w4 += s4[i].s * sin(a) + s4[i].c * cos(a);
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307 | }
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308 |
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309 | s = (w0 +
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310 | (w1 +
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311 | (w2 +
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312 | (w3 +
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313 | (w4 +
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314 | w5 * t) * t) * t) * t) * t) * ERFA_DAS2R - x*y/2.0;
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315 |
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316 | return s;
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317 |
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318 | }
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319 | /*----------------------------------------------------------------------
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320 | **
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321 | **
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322 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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323 | ** All rights reserved.
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324 | **
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325 | ** This library is derived, with permission, from the International
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326 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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327 | ** available from http://www.iausofa.org.
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328 | **
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329 | ** The ERFA version is intended to retain identical functionality to
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330 | ** the SOFA library, but made distinct through different function and
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331 | ** file names, as set out in the SOFA license conditions. The SOFA
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332 | ** original has a role as a reference standard for the IAU and IERS,
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333 | ** and consequently redistribution is permitted only in its unaltered
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334 | ** state. The ERFA version is not subject to this restriction and
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335 | ** therefore can be included in distributions which do not support the
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336 | ** concept of "read only" software.
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337 | **
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338 | ** Although the intent is to replicate the SOFA API (other than
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339 | ** replacement of prefix names) and results (with the exception of
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340 | ** bugs; any that are discovered will be fixed), SOFA is not
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341 | ** responsible for any errors found in this version of the library.
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342 | **
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343 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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344 | ** that you are using a library derived from SOFA, rather than SOFA
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345 | ** itself.
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346 | **
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347 | **
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348 | ** TERMS AND CONDITIONS
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349 | **
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350 | ** Redistribution and use in source and binary forms, with or without
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351 | ** modification, are permitted provided that the following conditions
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352 | ** are met:
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353 | **
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354 | ** 1 Redistributions of source code must retain the above copyright
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355 | ** notice, this list of conditions and the following disclaimer.
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356 | **
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357 | ** 2 Redistributions in binary form must reproduce the above copyright
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358 | ** notice, this list of conditions and the following disclaimer in
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359 | ** the documentation and/or other materials provided with the
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360 | ** distribution.
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361 | **
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362 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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363 | ** the International Astronomical Union nor the names of its
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364 | ** contributors may be used to endorse or promote products derived
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365 | ** from this software without specific prior written permission.
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366 | **
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367 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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368 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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369 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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370 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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371 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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372 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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373 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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374 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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375 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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376 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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377 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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378 | ** POSSIBILITY OF SUCH DAMAGE.
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379 | **
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380 | */
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