void iauC2ixy(double date1, double date2, double x, double y,
              double rc2i[3][3])
/*
**  - - - - - - - - -
**   i a u C 2 i x y
**  - - - - - - - - -
**
**  Form the celestial to intermediate-frame-of-date matrix for a given
**  date when the CIP X,Y coordinates are known.  IAU 2000.
**
**  This function is part of the International Astronomical Union's
**  SOFA (Standards Of Fundamental Astronomy) software collection.
**
**  Status:  support function.
**
**  Given:
**     date1,date2 double       TT as a 2-part Julian Date (Note 1)
**     x,y         double       Celestial Intermediate Pole (Note 2)
**
**  Returned:
**     rc2i        double[3][3] celestial-to-intermediate matrix (Note 3)
**
**  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 Celestial Intermediate Pole coordinates are the x,y components
**     of the unit vector in the Geocentric Celestial Reference System.
**
**  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.
**
**  4) Although its name does not include "00", This function is in fact
**     specific to the IAU 2000 models.
**
**  Called:
**     iauC2ixys    celestial-to-intermediate matrix, given X,Y and s
**     iauS00       the CIO locator s, given X,Y, IAU 2000A
**
**  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.
*/

{
    /* Compute s and then the matrix. */
    iauC2ixys(x, y, iauS00(date1, date2, x, y), 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
    **
    **--------------------------------------------------------------------*/
}
예제 #2
0
파일: s00a.c 프로젝트: DominicDirkx/sofa
double iauS00a(double date1, double date2)
/*
**  - - - - - - - -
**   i a u S 0 0 a
**  - - - - - - - -
**
**  The CIO locator s, positioning the Celestial Intermediate Origin on
**  the equator of the Celestial Intermediate Pole, using the IAU 2000A
**  precession-nutation 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    TT as a 2-part Julian Date (Note 1)
**
**  Returned (function value):
**                  double    the CIO locator s in radians (Note 2)
**
**  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 CIO locator s is the difference between the right ascensions
**     of the same point in two systems.  The two systems are the GCRS
**     and the CIP,CIO, and the point is the ascending node of the
**     CIP equator.  The CIO locator s remains a small fraction of
**     1 arcsecond throughout 1900-2100.
**
**  3) The series used to compute s is in fact for s+XY/2, where X and Y
**     are the x and y components of the CIP unit vector;  this series
**     is more compact than a direct series for s would be.  The present
**     function uses the full IAU 2000A nutation model when predicting
**     the CIP position.  Faster results, with no significant loss of
**     accuracy, can be obtained via the function iauS00b, which uses
**     instead the IAU 2000B truncated model.
**
**  Called:
**     iauPnm00a    classical NPB matrix, IAU 2000A
**     iauBnp2xy    extract CIP X,Y from the BPN matrix
**     iauS00       the CIO locator s, given X,Y, IAU 2000A
**
**  References:
**
**     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.
**
**     McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
**     IERS Technical Note No. 32, BKG (2004)
**
**  This revision:  2013 June 18
**
**  SOFA release 2015-02-09
**
**  Copyright (C) 2015 IAU SOFA Board.  See notes at end.
*/
{
   double rbpn[3][3], x, y, s;

/* Bias-precession-nutation-matrix, IAU 2000A. */
   iauPnm00a(date1, date2, rbpn);

/* Extract the CIP coordinates. */
   iauBpn2xy(rbpn, &x, &y);

/* Compute the CIO locator s, given the CIP coordinates. */
   s = iauS00(date1, date2, x, y);

   return s;

/*----------------------------------------------------------------------
**
**  Copyright (C) 2015
**  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
**
**--------------------------------------------------------------------*/
}
예제 #3
0
파일: s00b.c 프로젝트: tohka/celes
double iauS00b(double date1, double date2)
/*
**  - - - - - - - -
**   i a u S 0 0 b
**  - - - - - - - -
**
**  The CIO locator s, positioning the Celestial Intermediate Origin on
**  the equator of the Celestial Intermediate Pole, using the IAU 2000B
**  precession-nutation model.
**
**  Status:  support function.
**
**  Given:
**     date1,date2  double    TT as a 2-part Julian Date (Note 1)
**
**  Returned (function value):
**                  double    the CIO locator s in radians (Note 2)
**
**  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 CIO locator s is the difference between the right ascensions
**     of the same point in two systems.  The two systems are the GCRS
**     and the CIP,CIO, and the point is the ascending node of the
**     CIP equator.  The CIO locator s remains a small fraction of
**     1 arcsecond throughout 1900-2100.
**
**  3) The series used to compute s is in fact for s+XY/2, where X and Y
**     are the x and y components of the CIP unit vector;  this series
**     is more compact than a direct series for s would be.  The present
**     function uses the IAU 2000B truncated nutation model when
**     predicting the CIP position.  The function iauS00a uses instead
**     the full IAU 2000A model, but with no significant increase in
**     accuracy and at some cost in speed.
**
**  Called:
**     iauPnm00b     classical NPB matrix, IAU 2000B
**     iauBnp2xy     extract CIP X,Y from the BPN matrix
**     iauS00        the CIO locator s, given X,Y, IAU 2000A
**
**  References:
**
**     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.
**
**     McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
**     IERS Technical Note No. 32, BKG (2004)
**
**  This revision:  2010 January 18
**
**  Original version 2012-03-01
**
**  Copyright (C) 2013 Naoki Arita.  See notes at end.
*/
{
   double rbpn[3][3], x, y, s;


/* Bias-precession-nutation-matrix, IAU 2000B. */
   iauPnm00b(date1, date2, rbpn);

/* Extract the CIP coordinates. */
   iauBpn2xy(rbpn, &x, &y);

/* Compute the CIO locator s, given the CIP coordinates. */
   s = iauS00(date1, date2, x, y);

   return s;

/*----------------------------------------------------------------------
**
**  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.
**
**--------------------------------------------------------------------*/
}