SUBROUTINE iau_PN00 ( DATE1, DATE2, DPSI, DEPS, : EPSA, RB, RP, RBP, RN, RBPN ) *+ * - - - - - - - - - * i a u _ P N 0 0 * - - - - - - - - - * * Precession-nutation, IAU 2000 model: a multi-purpose routine, * supporting classical (equinox-based) use directly and CIO-based * use indirectly. * * This routine is part of the International Astronomical Union's * SOFA (Standards of Fundamental Astronomy) software collection. * * Status: support routine. * * Given: * DATE1,DATE2 d TT as a 2-part Julian Date (Note 1) * DPSI,DEPS d nutation (Note 2) * * Returned: * EPSA d mean obliquity (Note 3) * RB d(3,3) frame bias matrix (Note 4) * RP d(3,3) precession matrix (Note 5) * RBP d(3,3) bias-precession matrix (Note 6) * RN d(3,3) nutation matrix (Note 7) * RBPN d(3,3) GCRS-to-true matrix (Note 8) * * 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 * * 2450123.7D0 0D0 (JD method) * 2451545D0 -1421.3D0 (J2000 method) * 2400000.5D0 50123.2D0 (MJD method) * 2450123.5D0 0.2D0 (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 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 returned mean obliquity is consistent with the IAU 2000 * precession-nutation models. * * 4) The matrix RB transforms vectors from GCRS to J2000.0 mean equator * and equinox by applying frame bias. * * 5) The matrix RP transforms vectors from J2000.0 mean equator and * equinox to mean equator and equinox of date by applying * precession. * * 6) The matrix RBP transforms vectors from GCRS to mean equator and * equinox of date by applying frame bias then precession. It is the * product RP x RB. * * 7) The matrix RN transforms vectors from mean equator and equinox of * date to true equator and equinox of date by applying the nutation * (luni-solar + planetary). * * 8) The matrix RBPN transforms vectors from GCRS to true equator and * equinox of date. It is the product RN x RBP, applying frame bias, * precession and nutation in that order. * * Called: * iau_PR00 IAU 2000 precession adjustments * iau_OBL80 mean obliquity, IAU 1980 * iau_BP00 frame bias and precession matrices, IAU 2000 * iau_NUMAT form nutation matrix * iau_RXR product of two r-matrices * * Reference: * * Capitaine, N., Chapront, J., Lambert, S. and Wallace, P., * "Expressions for the Celestial Intermediate Pole and Celestial * Ephemeris Origin consistent with the IAU 2000A precession-nutation * model", Astron.Astrophys. 400, 1145-1154 (2003) * * n.b. The celestial ephemeris origin (CEO) was renamed "celestial * intermediate origin" (CIO) by IAU 2006 Resolution 2. * * This revision: 2010 January 18 * * SOFA release 2010-12-01 * * Copyright (C) 2010 IAU SOFA Board. See notes at end. * *----------------------------------------------------------------------- IMPLICIT NONE DOUBLE PRECISION DATE1, DATE2, DPSI, DEPS, : EPSA, RB(3,3), RP(3,3), RBP(3,3), : RN(3,3), RBPN(3,3) DOUBLE PRECISION DPSIPR, DEPSPR DOUBLE PRECISION iau_OBL80 * - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - * IAU 2000 precession-rate adjustments. CALL iau_PR00 ( DATE1, DATE2, DPSIPR, DEPSPR ) * Mean obliquity, consistent with IAU 2000 precession-nutation. EPSA = iau_OBL80 ( DATE1, DATE2 ) + DEPSPR * Frame bias and precession matrices and their product. CALL iau_BP00 ( DATE1, DATE2, RB, RP, RBP ) * Nutation matrix. CALL iau_NUMAT ( EPSA, DPSI, DEPS, RN ) * Bias-precession-nutation matrix (classical). CALL iau_RXR ( RN, RBP, RBPN ) * Finished. *+---------------------------------------------------------------------- * * Copyright (C) 2010 * Standards Of Fundamental Astronomy Board * of the International Astronomical Union. * * ===================== * SOFA Software License * ===================== * * NOTICE TO USER: * * BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING TERMS AND CONDITIONS * WHICH APPLY TO ITS USE. * * 1. The Software is owned by the IAU SOFA Board ("SOFA"). * * 2. Permission is granted to anyone to use the SOFA software for any * purpose, including commercial applications, free of charge and * without payment of royalties, subject to the conditions and * restrictions listed below. * * 3. You (the user) may copy and distribute SOFA source code to others, * and use and adapt its code and algorithms in your own software, * on a world-wide, royalty-free basis. That portion of your * distribution that does not consist of intact and unchanged copies * of SOFA source code files is a "derived work" that must comply * with the following requirements: * * a) Your work shall be marked or carry a statement that it * (i) uses routines and computations derived by you from * software provided by SOFA under license to you; and * (ii) does not itself constitute software provided by and/or * endorsed by SOFA. * * b) The source code of your derived work must contain descriptions * of how the derived work is based upon, contains and/or differs * from the original SOFA software. * * c) The name(s) of all routine(s) in your derived work shall not * include the prefix "iau". * * d) The origin of the SOFA components of your derived work must * not be misrepresented; you must not claim that you wrote the * original software, nor file a patent application for SOFA * software or algorithms embedded in the SOFA software. * * e) These requirements must be reproduced intact in any source * distribution and shall apply to anyone to whom you have * granted a further right to modify the source code of your * derived work. * * Note that, as originally distributed, the SOFA software is * intended to be a definitive implementation of the IAU standards, * and consequently third-party modifications are discouraged. All * variations, no matter how minor, must be explicitly marked as * such, as explained above. * * 4. In any published work or commercial products which includes * results achieved by using the SOFA software, you shall * acknowledge that the SOFA software was used in obtaining those * results. * * 5. You shall not cause the SOFA software to be brought into * disrepute, either by misuse, or use for inappropriate tasks, or * by inappropriate modification. * * 6. The SOFA software is provided "as is" and SOFA makes no warranty * as to its use or performance. SOFA does not and cannot warrant * the performance or results which the user may obtain by using the * SOFA software. SOFA makes no warranties, express or implied, as * to non-infringement of third party rights, merchantability, or * fitness for any particular purpose. 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