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authorWilliam Joye <wjoye@cfa.harvard.edu>2018-01-09 19:26:44 (GMT)
committerWilliam Joye <wjoye@cfa.harvard.edu>2018-01-09 19:26:44 (GMT)
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update ast 8.6.2
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diff --git a/ast/erfa/pmat76.c b/ast/erfa/pmat76.c
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-#include "erfa.h"
-
-void eraPmat76(double date1, double date2, double rmatp[3][3])
-/*
-** - - - - - - - - - -
-** e r a P m a t 7 6
-** - - - - - - - - - -
-**
-** Precession matrix from J2000.0 to a specified date, IAU 1976 model.
-**
-** Given:
-** date1,date2 double ending date, TT (Note 1)
-**
-** Returned:
-** rmatp double[3][3] precession matrix, J2000.0 -> date1+date2
-**
-** Notes:
-**
-** 1) The TT date date1+date2 is a Julian Date, apportioned in any
-** convenient way between the two arguments. For example,
-** JD(TT)=2450123.7 could be expressed in any of these ways,
-** among others:
-**
-** date1 date2
-**
-** 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 method is best matched to the way
-** the argument is handled internally and will deliver the
-** optimum resolution. The MJD method and the date & time methods
-** are both good compromises between resolution and convenience.
-**
-** 2) The matrix operates in the sense V(date) = RMATP * V(J2000),
-** where the p-vector V(J2000) is with respect to the mean
-** equatorial triad of epoch J2000.0 and the p-vector V(date)
-** is with respect to the mean equatorial triad of the given
-** date.
-**
-** 3) Though the matrix method itself is rigorous, the precession
-** angles are expressed through canonical polynomials which are
-** valid only for a limited time span. In addition, the IAU 1976
-** precession rate is known to be imperfect. The absolute accuracy
-** of the present formulation is better than 0.1 arcsec from
-** 1960AD to 2040AD, better than 1 arcsec from 1640AD to 2360AD,
-** and remains below 3 arcsec for the whole of the period
-** 500BC to 3000AD. The errors exceed 10 arcsec outside the
-** range 1200BC to 3900AD, exceed 100 arcsec outside 4200BC to
-** 5600AD and exceed 1000 arcsec outside 6800BC to 8200AD.
-**
-** Called:
-** eraPrec76 accumulated precession angles, IAU 1976
-** eraIr initialize r-matrix to identity
-** eraRz rotate around Z-axis
-** eraRy rotate around Y-axis
-** eraCr copy r-matrix
-**
-** References:
-**
-** Lieske, J.H., 1979, Astron.Astrophys. 73, 282.
-** equations (6) & (7), p283.
-**
-** Kaplan,G.H., 1981. USNO circular no. 163, pA2.
-**
-** Copyright (C) 2013-2016, NumFOCUS Foundation.
-** Derived, with permission, from the SOFA library. See notes at end of file.
-*/
-{
- double zeta, z, theta, wmat[3][3];
-
-
-/* Precession Euler angles, J2000.0 to specified date. */
- eraPrec76(ERFA_DJ00, 0.0, date1, date2, &zeta, &z, &theta);
-
-/* Form the rotation matrix. */
- eraIr( wmat);
- eraRz( -zeta, wmat);
- eraRy( theta, wmat);
- eraRz( -z, wmat);
- eraCr( wmat, rmatp);
-
- 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.
-**
-*/