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authorWilliam Joye <wjoye@cfa.harvard.edu>2018-01-09 19:06:55 (GMT)
committerWilliam Joye <wjoye@cfa.harvard.edu>2018-01-09 19:06:55 (GMT)
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update ast 8.6.2
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+#include "erfa.h"
+
+void eraC2tpe(double tta, double ttb, double uta, double utb,
+ double dpsi, double deps, double xp, double yp,
+ double rc2t[3][3])
+/*
+** - - - - - - - - -
+** e r a C 2 t p e
+** - - - - - - - - -
+**
+** Form the celestial to terrestrial matrix given the date, the UT1,
+** the nutation and the polar motion. IAU 2000.
+**
+** Given:
+** tta,ttb double TT as a 2-part Julian Date (Note 1)
+** uta,utb double UT1 as a 2-part Julian Date (Note 1)
+** dpsi,deps double nutation (Note 2)
+** xp,yp double coordinates of the pole (radians, Note 3)
+**
+** Returned:
+** rc2t double[3][3] celestial-to-terrestrial matrix (Note 4)
+**
+** Notes:
+**
+** 1) The TT and UT1 dates tta+ttb and uta+utb are Julian Dates,
+** apportioned in any convenient way between the arguments uta and
+** utb. For example, JD(UT1)=2450123.7 could be expressed in any of
+** these ways, among others:
+**
+** uta utb
+**
+** 2450123.7 0.0 (JD method)
+** 2451545.0 -1421.3 (J2000 method)
+** 2400000.5 50123.2 (MJD method)
+** 2450123.5 0.2 (date & time method)
+**
+** The JD method is the most natural and convenient to use in
+** cases where the loss of several decimal digits of resolution is
+** acceptable. The J2000 and MJD methods are good compromises
+** between resolution and convenience. In the case of uta,utb, the
+** date & time method is best matched to the Earth rotation angle
+** algorithm used: maximum precision is delivered when the uta
+** argument is for 0hrs UT1 on the day in question and the utb
+** argument lies in the range 0 to 1, or vice versa.
+**
+** 2) The caller is responsible for providing the nutation components;
+** they are in longitude and obliquity, in radians and are with
+** respect to the equinox and ecliptic of date. For high-accuracy
+** applications, free core nutation should be included as well as
+** any other relevant corrections to the position of the CIP.
+**
+** 3) The arguments xp and yp are the coordinates (in radians) of the
+** Celestial Intermediate Pole with respect to the International
+** Terrestrial Reference System (see IERS Conventions 2003),
+** measured along the meridians to 0 and 90 deg west respectively.
+**
+** 4) The matrix rc2t transforms from celestial to terrestrial
+** coordinates:
+**
+** [TRS] = RPOM * R_3(GST) * RBPN * [CRS]
+**
+** = rc2t * [CRS]
+**
+** where [CRS] is a vector in the Geocentric Celestial Reference
+** System and [TRS] is a vector in the International Terrestrial
+** Reference System (see IERS Conventions 2003), RBPN is the
+** bias-precession-nutation matrix, GST is the Greenwich (apparent)
+** Sidereal Time and RPOM is the polar motion matrix.
+**
+** 5) Although its name does not include "00", This function is in fact
+** specific to the IAU 2000 models.
+**
+** Called:
+** eraPn00 bias/precession/nutation results, IAU 2000
+** eraGmst00 Greenwich mean sidereal time, IAU 2000
+** eraSp00 the TIO locator s', IERS 2000
+** eraEe00 equation of the equinoxes, IAU 2000
+** eraPom00 polar motion matrix
+** eraC2teqx form equinox-based celestial-to-terrestrial matrix
+**
+** Reference:
+**
+** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
+** IERS Technical Note No. 32, BKG (2004)
+**
+** Copyright (C) 2013-2016, NumFOCUS Foundation.
+** Derived, with permission, from the SOFA library. See notes at end of file.
+*/
+{
+ double epsa, rb[3][3], rp[3][3], rbp[3][3], rn[3][3],
+ rbpn[3][3], gmst, ee, sp, rpom[3][3];
+
+
+/* Form the celestial-to-true matrix for this TT. */
+ eraPn00(tta, ttb, dpsi, deps, &epsa, rb, rp, rbp, rn, rbpn);
+
+/* Predict the Greenwich Mean Sidereal Time for this UT1 and TT. */
+ gmst = eraGmst00(uta, utb, tta, ttb);
+
+/* Predict the equation of the equinoxes given TT and nutation. */
+ ee = eraEe00(tta, ttb, epsa, dpsi);
+
+/* Estimate s'. */
+ sp = eraSp00(tta, ttb);
+
+/* Form the polar motion matrix. */
+ eraPom00(xp, yp, sp, rpom);
+
+/* Combine to form the celestial-to-terrestrial matrix. */
+ eraC2teqx(rbpn, gmst + ee, rpom, rc2t);
+
+ return;
+
+}
+/*----------------------------------------------------------------------
+**
+**
+** Copyright (C) 2013-2016, NumFOCUS Foundation.
+** All rights reserved.
+**
+** This library is derived, with permission, from the International
+** Astronomical Union's "Standards of Fundamental Astronomy" library,
+** available from http://www.iausofa.org.
+**
+** The ERFA version is intended to retain identical functionality to
+** the SOFA library, but made distinct through different function and
+** file names, as set out in the SOFA license conditions. The SOFA
+** original has a role as a reference standard for the IAU and IERS,
+** and consequently redistribution is permitted only in its unaltered
+** state. The ERFA version is not subject to this restriction and
+** therefore can be included in distributions which do not support the
+** concept of "read only" software.
+**
+** Although the intent is to replicate the SOFA API (other than
+** replacement of prefix names) and results (with the exception of
+** bugs; any that are discovered will be fixed), SOFA is not
+** responsible for any errors found in this version of the library.
+**
+** If you wish to acknowledge the SOFA heritage, please acknowledge
+** that you are using a library derived from SOFA, rather than SOFA
+** itself.
+**
+**
+** TERMS AND CONDITIONS
+**
+** Redistribution and use in source and binary forms, with or without
+** modification, are permitted provided that the following conditions
+** are met:
+**
+** 1 Redistributions of source code must retain the above copyright
+** notice, this list of conditions and the following disclaimer.
+**
+** 2 Redistributions in binary form must reproduce the above copyright
+** notice, this list of conditions and the following disclaimer in
+** the documentation and/or other materials provided with the
+** distribution.
+**
+** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
+** the International Astronomical Union nor the names of its
+** contributors may be used to endorse or promote products derived
+** from this software without specific prior written permission.
+**
+** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
+** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
+** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
+** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
+** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
+** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
+** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
+** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
+** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
+** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
+** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
+** POSSIBILITY OF SUCH DAMAGE.
+**
+*/