/* *+ * Name: * palEcmat * Purpose: * Form the equatorial to ecliptic rotation matrix - IAU 2006 * precession model. * Language: * Starlink ANSI C * Type of Module: * Library routine * Invocation: * palEcmat( double date, double rmat[3][3] ) * Arguments: * date = double (Given) * TT as Modified Julian Date (JD-2400000.5). The difference * between TT and TDB is of the order of a millisecond or two * (i.e. about 0.02 arc-seconds). * rmat = double[3][3] (Returned) * Rotation matrix * Description: * The equatorial to ecliptic rotation matrix is found and returned. * The matrix is in the sense V(ecl) = RMAT * V(equ); the * equator, equinox and ecliptic are mean of date. * 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 * Adapted with permission from the Fortran SLALIB library. * {enter_further_changes_here} * Copyright: * Copyright (C) 1996 Rutherford Appleton Laboratory * 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 Lesser 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 Lesser General Public License for more details. * * You should have received a copy of the GNU Lesser General * License along with this program. If not, see * . * Bugs: * {note_any_bugs_here} *- */ #include "pal.h" #include "palmac.h" #include "pal1sofa.h" void palEcmat( double date, double rmat[3][3] ) { /* Mean obliquity (the angle between the ecliptic and mean equator of date). */ double eps0 = eraObl06( PAL__MJD0, date ); /* Matrix */ palDeuler( "X", eps0, 0.0, 0.0, rmat ); }