void palDeuler( const char *order, double phi, double theta, double psi, double rmat[3][3] ) { int i = 0; double rotations[3]; /* Initialise rmat */ iauIr( rmat ); /* copy the rotations into an array */ rotations[0] = phi; rotations[1] = theta; rotations[2] = psi; /* maximum three rotations */ while (i < 3 && order[i] != '\0') { switch (order[i]) { case 'X': case 'x': case '1': iauRx( rotations[i], rmat ); break; case 'Y': case 'y': case '2': iauRy( rotations[i], rmat ); break; case 'Z': case 'z': case '3': iauRz( rotations[i], rmat ); break; default: /* break out the loop if we do not recognize something */ i = 3; } /* Go to the next position */ i++; } return; }
void iauPmat76(double date1, double date2, double rmatp[3][3]) /* ** - - - - - - - - - - ** i a u P m a t 7 6 ** - - - - - - - - - - ** ** Precession matrix from J2000.0 to a specified date, IAU 1976 model. ** ** This function is part of the International Astronomical Union's ** SOFA (Standards Of Fundamental Astronomy) software collection. ** ** Status: support function. ** ** 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: ** iauPrec76 accumulated precession angles, IAU 1976 ** iauIr initialize r-matrix to identity ** iauRz rotate around Z-axis ** iauRy rotate around Y-axis ** iauCr 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. ** ** This revision: 2013 June 18 ** ** SOFA release 2016-05-03 ** ** Copyright (C) 2016 IAU SOFA Board. See notes at end. */ { double zeta, z, theta, wmat[3][3]; /* Precession Euler angles, J2000.0 to specified date. */ iauPrec76(DJ00, 0.0, date1, date2, &zeta, &z, &theta); /* Form the rotation matrix. */ iauIr( wmat); iauRz( -zeta, wmat); iauRy( theta, wmat); iauRz( -z, wmat); iauCr( wmat, rmatp); return; /*---------------------------------------------------------------------- ** ** Copyright (C) 2016 ** Standards Of Fundamental Astronomy Board ** of the International Astronomical Union. ** ** ===================== ** SOFA Software License ** ===================== ** ** NOTICE TO USER: ** ** BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING SIX 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 names of all routines in your derived work shall not ** include the prefix "iau" or "sofa" or trivial modifications ** thereof such as changes of case. ** ** 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. You shall not cause the SOFA software to be brought into ** disrepute, either by misuse, or use for inappropriate tasks, or ** by inappropriate modification. ** ** 5. 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. In no event will SOFA be ** liable to the user for any consequential, incidental, or special ** damages, including any lost profits or lost savings, even if a ** SOFA representative has been advised of such damages, or for any ** claim by any third party. ** ** 6. The provision of any version of the SOFA software under the terms ** and conditions specified herein does not imply that future ** versions will also be made available under the same terms and ** conditions. * ** In any published work or commercial product which uses the SOFA ** software directly, acknowledgement (see www.iausofa.org) is ** appreciated. ** ** Correspondence concerning SOFA software should be addressed as ** follows: ** ** By email: [email protected] ** By post: IAU SOFA Center ** HM Nautical Almanac Office ** UK Hydrographic Office ** Admiralty Way, Taunton ** Somerset, TA1 2DN ** United Kingdom ** **--------------------------------------------------------------------*/ }
void iauC2ixys(double x, double y, double s, double rc2i[3][3]) /* ** - - - - - - - - - - ** i a u C 2 i x y s ** - - - - - - - - - - ** ** Form the celestial to intermediate-frame-of-date matrix given the CIP ** X,Y and the CIO locator s. ** ** This function is part of the International Astronomical Union's ** SOFA (Standards Of Fundamental Astronomy) software collection. ** ** Status: support function. ** ** Given: ** x,y double Celestial Intermediate Pole (Note 1) ** s double the CIO locator s (Note 2) ** ** Returned: ** rc2i double[3][3] celestial-to-intermediate matrix (Note 3) ** ** Notes: ** ** 1) The Celestial Intermediate Pole coordinates are the x,y ** components of the unit vector in the Geocentric Celestial ** Reference System. ** ** 2) The CIO locator s (in radians) positions the Celestial ** Intermediate Origin on the equator of the CIP. ** ** 3) The matrix rc2i is the first stage in the transformation from ** celestial to terrestrial coordinates: ** ** [TRS] = RPOM * R_3(ERA) * rc2i * [CRS] ** ** = RC2T * [CRS] ** ** where [CRS] is a vector in the Geocentric Celestial Reference ** System and [TRS] is a vector in the International Terrestrial ** Reference System (see IERS Conventions 2003), ERA is the Earth ** Rotation Angle and RPOM is the polar motion matrix. ** ** Called: ** iauIr initialize r-matrix to identity ** iauRz rotate around Z-axis ** iauRy rotate around Y-axis ** ** Reference: ** ** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003), ** IERS Technical Note No. 32, BKG (2004) ** ** This revision: 2014 November 7 ** ** SOFA release 2016-05-03 ** ** Copyright (C) 2016 IAU SOFA Board. See notes at end. */ { double r2, e, d; /* Obtain the spherical angles E and d. */ r2 = x*x + y*y; e = (r2 > 0.0) ? atan2(y, x) : 0.0; d = atan(sqrt(r2 / (1.0 - r2))); /* Form the matrix. */ iauIr(rc2i); iauRz(e, rc2i); iauRy(d, rc2i); iauRz(-(e+s), rc2i); return; /*---------------------------------------------------------------------- ** ** Copyright (C) 2016 ** Standards Of Fundamental Astronomy Board ** of the International Astronomical Union. ** ** ===================== ** SOFA Software License ** ===================== ** ** NOTICE TO USER: ** ** BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING SIX 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 names of all routines in your derived work shall not ** include the prefix "iau" or "sofa" or trivial modifications ** thereof such as changes of case. ** ** 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. You shall not cause the SOFA software to be brought into ** disrepute, either by misuse, or use for inappropriate tasks, or ** by inappropriate modification. ** ** 5. 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. In no event will SOFA be ** liable to the user for any consequential, incidental, or special ** damages, including any lost profits or lost savings, even if a ** SOFA representative has been advised of such damages, or for any ** claim by any third party. ** ** 6. The provision of any version of the SOFA software under the terms ** and conditions specified herein does not imply that future ** versions will also be made available under the same terms and ** conditions. * ** In any published work or commercial product which uses the SOFA ** software directly, acknowledgement (see www.iausofa.org) is ** appreciated. ** ** Correspondence concerning SOFA software should be addressed as ** follows: ** ** By email: [email protected] ** By post: IAU SOFA Center ** HM Nautical Almanac Office ** UK Hydrographic Office ** Admiralty Way, Taunton ** Somerset, TA1 2DN ** United Kingdom ** **--------------------------------------------------------------------*/ }
void iauBp00(double date1, double date2, double rb[3][3], double rp[3][3], double rbp[3][3]) /* ** - - - - - - - - ** i a u B p 0 0 ** - - - - - - - - ** ** Frame bias and precession, IAU 2000. ** ** Status: canonical model. ** ** Given: ** date1,date2 double TT as a 2-part Julian Date (Note 1) ** ** Returned: ** rb double[3][3] frame bias matrix (Note 2) ** rp double[3][3] precession matrix (Note 3) ** rbp double[3][3] bias-precession matrix (Note 4) ** ** 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 rb transforms vectors from GCRS to mean J2000.0 by ** applying frame bias. ** ** 3) The matrix rp transforms vectors from J2000.0 mean equator and ** equinox to mean equator and equinox of date by applying ** precession. ** ** 4) 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. ** ** 5) It is permissible to re-use the same array in the returned ** arguments. The arrays are filled in the order given. ** ** Called: ** iauBi00 frame bias components, IAU 2000 ** iauPr00 IAU 2000 precession adjustments ** iauIr initialize r-matrix to identity ** iauRx rotate around X-axis ** iauRy rotate around Y-axis ** iauRz rotate around Z-axis ** iauCr copy r-matrix ** iauRxr product of two r-matrices ** ** Reference: ** "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 ** ** Original version 2012-03-01 ** ** Copyright (C) 2013 Naoki Arita. See notes at end. */ { /* J2000.0 obliquity (Lieske et al. 1977) */ const double EPS0 = 84381.448 * DAS2R; double t, dpsibi, depsbi; double dra0, psia77, oma77, chia, dpsipr, depspr, psia, oma, rbw[3][3]; /* Interval between fundamental epoch J2000.0 and current date (JC). */ t = ((date1 - DJ00) + date2) / DJC; /* Frame bias. */ iauBi00(&dpsibi, &depsbi, &dra0); /* Precession angles (Lieske et al. 1977) */ psia77 = (5038.7784 + (-1.07259 + (-0.001147) * t) * t) * t * DAS2R; oma77 = EPS0 + ((0.05127 + (-0.007726) * t) * t) * t * DAS2R; chia = ( 10.5526 + (-2.38064 + (-0.001125) * t) * t) * t * DAS2R; /* Apply IAU 2000 precession corrections. */ iauPr00(date1, date2, &dpsipr, &depspr); psia = psia77 + dpsipr; oma = oma77 + depspr; /* Frame bias matrix: GCRS to J2000.0. */ iauIr(rbw); iauRz(dra0, rbw); iauRy(dpsibi * sin(EPS0), rbw); iauRx(-depsbi, rbw); iauCr(rbw, rb); /* Precession matrix: J2000.0 to mean of date. */ iauIr(rp); iauRx(EPS0, rp); iauRz(-psia, rp); iauRx(-oma, rp); iauRz(chia, rp); /* Bias-precession matrix: GCRS to mean of date. */ iauRxr(rp, rbw, rbp); return; /*---------------------------------------------------------------------- ** ** Celes is a wrapper of the SOFA Library for Ruby. ** ** This file is redistributed and relicensed in accordance with ** the SOFA Software License (http://www.iausofa.org/tandc.html). ** ** The original library is available from IAU Standards of ** Fundamental Astronomy (http://www.iausofa.org/). ** ** ** ** ** ** Copyright (C) 2013, Naoki Arita ** All rights reserved. ** ** 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. ** **--------------------------------------------------------------------*/ }
void iauBp00(double date1, double date2, double rb[3][3], double rp[3][3], double rbp[3][3]) /* ** - - - - - - - - ** i a u B p 0 0 ** - - - - - - - - ** ** Frame bias and precession, IAU 2000. ** ** This function is part of the International Astronomical Union's ** SOFA (Standards Of Fundamental Astronomy) software collection. ** ** Status: canonical model. ** ** Given: ** date1,date2 double TT as a 2-part Julian Date (Note 1) ** ** Returned: ** rb double[3][3] frame bias matrix (Note 2) ** rp double[3][3] precession matrix (Note 3) ** rbp double[3][3] bias-precession matrix (Note 4) ** ** 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 rb transforms vectors from GCRS to mean J2000.0 by ** applying frame bias. ** ** 3) The matrix rp transforms vectors from J2000.0 mean equator and ** equinox to mean equator and equinox of date by applying ** precession. ** ** 4) 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. ** ** 5) It is permissible to re-use the same array in the returned ** arguments. The arrays are filled in the order given. ** ** Called: ** iauBi00 frame bias components, IAU 2000 ** iauPr00 IAU 2000 precession adjustments ** iauIr initialize r-matrix to identity ** iauRx rotate around X-axis ** iauRy rotate around Y-axis ** iauRz rotate around Z-axis ** iauCr copy r-matrix ** iauRxr product of two r-matrices ** ** Reference: ** "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. */ { /* J2000.0 obliquity (Lieske et al. 1977) */ const double EPS0 = 84381.448 * DAS2R; double t, dpsibi, depsbi; double dra0, psia77, oma77, chia, dpsipr, depspr, psia, oma, rbw[3][3]; /* Interval between fundamental epoch J2000.0 and current date (JC). */ t = ((date1 - DJ00) + date2) / DJC; /* Frame bias. */ iauBi00(&dpsibi, &depsbi, &dra0); /* Precession angles (Lieske et al. 1977) */ psia77 = (5038.7784 + (-1.07259 + (-0.001147) * t) * t) * t * DAS2R; oma77 = EPS0 + ((0.05127 + (-0.007726) * t) * t) * t * DAS2R; chia = ( 10.5526 + (-2.38064 + (-0.001125) * t) * t) * t * DAS2R; /* Apply IAU 2000 precession corrections. */ iauPr00(date1, date2, &dpsipr, &depspr); psia = psia77 + dpsipr; oma = oma77 + depspr; /* Frame bias matrix: GCRS to J2000.0. */ iauIr(rbw); iauRz(dra0, rbw); iauRy(dpsibi * sin(EPS0), rbw); iauRx(-depsbi, rbw); iauCr(rbw, rb); /* Precession matrix: J2000.0 to mean of date. */ iauIr(rp); iauRx(EPS0, rp); iauRz(-psia, rp); iauRx(-oma, rp); iauRz(chia, rp); /* Bias-precession matrix: GCRS to mean of date. */ iauRxr(rp, rbw, rbp); return; /*---------------------------------------------------------------------- ** ** 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. In no event will SOFA be ** liable to the user for any consequential, incidental, or special ** damages, including any lost profits or lost savings, even if a ** SOFA representative has been advised of such damages, or for any ** claim by any third party. ** ** 7. The provision of any version of the SOFA software under the terms ** and conditions specified herein does not imply that future ** versions will also be made available under the same terms and ** conditions. ** ** Correspondence concerning SOFA software should be addressed as ** follows: ** ** By email: [email protected] ** By post: IAU SOFA Center ** HM Nautical Almanac Office ** UK Hydrographic Office ** Admiralty Way, Taunton ** Somerset, TA1 2DN ** United Kingdom ** **--------------------------------------------------------------------*/ }
void iauPom00(double xp, double yp, double sp, double rpom[3][3]) /* ** - - - - - - - - - - ** i a u P o m 0 0 ** - - - - - - - - - - ** ** Form the matrix of polar motion for a given date, IAU 2000. ** ** This function is part of the International Astronomical Union's ** SOFA (Standards Of Fundamental Astronomy) software collection. ** ** Status: support function. ** ** Given: ** xp,yp double coordinates of the pole (radians, Note 1) ** sp double the TIO locator s' (radians, Note 2) ** ** Returned: ** rpom double[3][3] polar-motion matrix (Note 3) ** ** Notes: ** ** 1) The arguments xp and yp are the coordinates (in radians) of the ** Celestial Intermediate Pole with respect to the International ** Terrestrial Reference System (see IERS Conventions 2003), ** measured along the meridians to 0 and 90 deg west respectively. ** ** 2) The argument sp is the TIO locator s', in radians, which ** positions the Terrestrial Intermediate Origin on the equator. It ** is obtained from polar motion observations by numerical ** integration, and so is in essence unpredictable. However, it is ** dominated by a secular drift of about 47 microarcseconds per ** century, and so can be taken into account by using s' = -47*t, ** where t is centuries since J2000.0. The function iauSp00 ** implements this approximation. ** ** 3) The matrix operates in the sense V(TRS) = rpom * V(CIP), meaning ** that it is the final rotation when computing the pointing ** direction to a celestial source. ** ** Called: ** iauIr initialize r-matrix to identity ** iauRz rotate around Z-axis ** iauRy rotate around Y-axis ** iauRx rotate around X-axis ** ** Reference: ** ** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003), ** IERS Technical Note No. 32, BKG (2004) ** ** This revision: 2013 June 18 ** ** SOFA release 2016-05-03 ** ** Copyright (C) 2016 IAU SOFA Board. See notes at end. */ { /* Construct the matrix. */ iauIr(rpom); iauRz(sp, rpom); iauRy(-xp, rpom); iauRx(-yp, rpom); return; /*---------------------------------------------------------------------- ** ** Copyright (C) 2016 ** Standards Of Fundamental Astronomy Board ** of the International Astronomical Union. ** ** ===================== ** SOFA Software License ** ===================== ** ** NOTICE TO USER: ** ** BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING SIX 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. 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The provision of any version of the SOFA software under the terms ** and conditions specified herein does not imply that future ** versions will also be made available under the same terms and ** conditions. * ** In any published work or commercial product which uses the SOFA ** software directly, acknowledgement (see www.iausofa.org) is ** appreciated. ** ** Correspondence concerning SOFA software should be addressed as ** follows: ** ** By email: [email protected] ** By post: IAU SOFA Center ** HM Nautical Almanac Office ** UK Hydrographic Office ** Admiralty Way, Taunton ** Somerset, TA1 2DN ** United Kingdom ** **--------------------------------------------------------------------*/ }