#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) 2013-2017, 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) 2013-2017, 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. ** */