1 | #include "erfa.h"
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2 |
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3 | void eraC2txy(double tta, double ttb, double uta, double utb,
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4 | double x, double y, double xp, double yp,
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5 | double rc2t[3][3])
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6 | /*
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7 | ** - - - - - - - - -
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8 | ** e r a C 2 t x y
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9 | ** - - - - - - - - -
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10 | **
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11 | ** Form the celestial to terrestrial matrix given the date, the UT1,
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12 | ** the CIP coordinates and the polar motion. IAU 2000.
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13 | **
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14 | ** Given:
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15 | ** tta,ttb double TT as a 2-part Julian Date (Note 1)
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16 | ** uta,utb double UT1 as a 2-part Julian Date (Note 1)
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17 | ** x,y double Celestial Intermediate Pole (Note 2)
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18 | ** xp,yp double coordinates of the pole (radians, Note 3)
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19 | **
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20 | ** Returned:
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21 | ** rc2t double[3][3] celestial-to-terrestrial matrix (Note 4)
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22 | **
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23 | ** Notes:
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24 | **
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25 | ** 1) The TT and UT1 dates tta+ttb and uta+utb are Julian Dates,
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26 | ** apportioned in any convenient way between the arguments uta and
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27 | ** utb. For example, JD(UT1)=2450123.7 could be expressed in any o
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28 | ** these ways, among others:
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29 | **
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30 | ** uta utb
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31 | **
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32 | ** 2450123.7 0.0 (JD method)
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33 | ** 2451545.0 -1421.3 (J2000 method)
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34 | ** 2400000.5 50123.2 (MJD method)
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35 | ** 2450123.5 0.2 (date & time method)
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36 | **
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37 | ** The JD method is the most natural and convenient to use in
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38 | ** cases where the loss of several decimal digits of resolution is
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39 | ** acceptable. The J2000 and MJD methods are good compromises
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40 | ** between resolution and convenience. In the case of uta,utb, the
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41 | ** date & time method is best matched to the Earth rotation angle
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42 | ** algorithm used: maximum precision is delivered when the uta
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43 | ** argument is for 0hrs UT1 on the day in question and the utb
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44 | ** argument lies in the range 0 to 1, or vice versa.
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45 | **
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46 | ** 2) The Celestial Intermediate Pole coordinates are the x,y
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47 | ** components of the unit vector in the Geocentric Celestial
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48 | ** Reference System.
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49 | **
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50 | ** 3) The arguments xp and yp are the coordinates (in radians) of the
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51 | ** Celestial Intermediate Pole with respect to the International
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52 | ** Terrestrial Reference System (see IERS Conventions 2003),
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53 | ** measured along the meridians to 0 and 90 deg west respectively.
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54 | **
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55 | ** 4) The matrix rc2t transforms from celestial to terrestrial
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56 | ** coordinates:
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57 | **
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58 | ** [TRS] = RPOM * R_3(ERA) * RC2I * [CRS]
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59 | **
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60 | ** = rc2t * [CRS]
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61 | **
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62 | ** where [CRS] is a vector in the Geocentric Celestial Reference
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63 | ** System and [TRS] is a vector in the International Terrestrial
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64 | ** Reference System (see IERS Conventions 2003), ERA is the Earth
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65 | ** Rotation Angle and RPOM is the polar motion matrix.
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66 | **
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67 | ** 5) Although its name does not include "00", This function is in fact
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68 | ** specific to the IAU 2000 models.
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69 | **
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70 | ** Called:
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71 | ** eraC2ixy celestial-to-intermediate matrix, given X,Y
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72 | ** eraEra00 Earth rotation angle, IAU 2000
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73 | ** eraSp00 the TIO locator s', IERS 2000
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74 | ** eraPom00 polar motion matrix
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75 | ** eraC2tcio form CIO-based celestial-to-terrestrial matrix
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76 | **
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77 | ** Reference:
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78 | **
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79 | ** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
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80 | ** IERS Technical Note No. 32, BKG (2004)
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81 | **
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82 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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83 | ** Derived, with permission, from the SOFA library. See notes at end of file.
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84 | */
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85 | {
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86 | double rc2i[3][3], era, sp, rpom[3][3];
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87 |
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88 |
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89 | /* Form the celestial-to-intermediate matrix for this TT. */
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90 | eraC2ixy(tta, ttb, x, y, rc2i);
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91 |
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92 | /* Predict the Earth rotation angle for this UT1. */
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93 | era = eraEra00(uta, utb);
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94 |
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95 | /* Estimate s'. */
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96 | sp = eraSp00(tta, ttb);
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97 |
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98 | /* Form the polar motion matrix. */
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99 | eraPom00(xp, yp, sp, rpom);
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100 |
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101 | /* Combine to form the celestial-to-terrestrial matrix. */
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102 | eraC2tcio(rc2i, era, rpom, rc2t);
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103 |
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104 | return;
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105 |
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106 | }
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107 | /*----------------------------------------------------------------------
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108 | **
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109 | **
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110 | ** Copyright (C) 2013-2016, NumFOCUS Foundation.
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111 | ** All rights reserved.
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112 | **
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113 | ** This library is derived, with permission, from the International
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114 | ** Astronomical Union's "Standards of Fundamental Astronomy" library,
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115 | ** available from http://www.iausofa.org.
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116 | **
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117 | ** The ERFA version is intended to retain identical functionality to
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118 | ** the SOFA library, but made distinct through different function and
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119 | ** file names, as set out in the SOFA license conditions. The SOFA
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120 | ** original has a role as a reference standard for the IAU and IERS,
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121 | ** and consequently redistribution is permitted only in its unaltered
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122 | ** state. The ERFA version is not subject to this restriction and
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123 | ** therefore can be included in distributions which do not support the
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124 | ** concept of "read only" software.
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125 | **
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126 | ** Although the intent is to replicate the SOFA API (other than
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127 | ** replacement of prefix names) and results (with the exception of
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128 | ** bugs; any that are discovered will be fixed), SOFA is not
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129 | ** responsible for any errors found in this version of the library.
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130 | **
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131 | ** If you wish to acknowledge the SOFA heritage, please acknowledge
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132 | ** that you are using a library derived from SOFA, rather than SOFA
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133 | ** itself.
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134 | **
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135 | **
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136 | ** TERMS AND CONDITIONS
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137 | **
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138 | ** Redistribution and use in source and binary forms, with or without
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139 | ** modification, are permitted provided that the following conditions
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140 | ** are met:
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141 | **
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142 | ** 1 Redistributions of source code must retain the above copyright
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143 | ** notice, this list of conditions and the following disclaimer.
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144 | **
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145 | ** 2 Redistributions in binary form must reproduce the above copyright
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146 | ** notice, this list of conditions and the following disclaimer in
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147 | ** the documentation and/or other materials provided with the
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148 | ** distribution.
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149 | **
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150 | ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
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151 | ** the International Astronomical Union nor the names of its
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152 | ** contributors may be used to endorse or promote products derived
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153 | ** from this software without specific prior written permission.
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154 | **
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155 | ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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156 | ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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157 | ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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158 | ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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159 | ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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160 | ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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161 | ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
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162 | ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
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163 | ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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164 | ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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165 | ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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166 | ** POSSIBILITY OF SUCH DAMAGE.
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167 | **
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168 | */
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