/* *+ * Name: * palPrec * Purpose: * Form the matrix of precession between two epochs (IAU 2006) * Language: * Starlink ANSI C * Type of Module: * Library routine * Invocation: * palPrec( double ep0, double ep1, double rmatp[3][3] ) * Arguments: * ep0 = double (Given) * Beginning epoch * ep1 = double (Given) * Ending epoch * rmatp = double[3][3] (Returned) * Precession matrix * Description: * The IAU 2006 precession matrix from ep0 to ep1 is found and * returned. The matrix is in the sense V(EP1) = RMATP * V(EP0). * The epochs are TDB (loosely TT) Julian epochs. * * Though the matrix method itself is rigorous, the precession * angles are expressed through canonical polynomials which are * valid only for a limited time span of a few hundred years around * the current epoch. * Authors: * PTW: Pat Wallace (STFC) * DSB: David Berry (JAC, Hawaii) * {enter_new_authors_here} * History: * 2012-02-10 (DSB): * Initial version with documentation taken from Fortran SLA * {enter_further_changes_here} * Copyright: * Copyright (C) 2012 Science and Technology Facilities Council. * All Rights Reserved. * Licence: * This program is free software; you can redistribute it and/or * modify it under the terms of the GNU General Public License as * published by the Free Software Foundation; either version 3 of * the License, or (at your option) any later version. * * This program is distributed in the hope that it will be * useful, but WITHOUT ANY WARRANTY; without even the implied * warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR * PURPOSE. See the GNU General Public License for more details. * * You should have received a copy of the GNU General Public License * along with this program; if not, write to the Free Software * Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 * USA. * Bugs: * {note_any_bugs_here} *- */ #include "pal.h" #include "sofa.h" #include "sofam.h" void palPrec( double ep0, double ep1, double rmatp[3][3] ){ /* Local Variables: */ double rmatq[3][3]; double ep0_days; double ep1_days; /* Convert supplied dates to days since J2000 */ ep0_days = ( ep0 - 2000.0 )*DJY; ep1_days = ( ep1 - 2000.0 )*DJY; /* If beginning epoch is J2000, just return the rotation matrix from J2000 to EP1. */ if( ep0 == 2000.0 ) { iauPmat06( DJ00, ep1_days, rmatp ); /* If end epoch is J2000, get the rotation matrix from J2000 to EP0 and then transpose it to get the rotation matrix from EP0 to J2000. */ } else if( ep1 == 2000.0 ) { iauPmat06( DJ00, ep0_days, rmatp ); iauTr( rmatp, rmatp ); /* Otherwise. get the two matrices used above and multiply them together. */ } else { iauPmat06( DJ00, ep0_days, rmatp ); iauTr( rmatp, rmatp ); iauPmat06( DJ00, ep1_days, rmatq ); iauRxr( rmatp, rmatq, rmatp ); } }