SUBROUTINE iau_HFK5Z ( RH, DH, DATE1, DATE2, R5, D5, DR5, DD5 )
*+
*  - - - - - - - - - -
*   i a u _ H F K 5 Z
*  - - - - - - - - - -
*
*  Transform a Hipparcos star position into FK5 J2000, assuming
*  zero Hipparcos proper motion.
*
*  This routine is part of the International Astronomical Union's
*  SOFA (Standards of Fundamental Astronomy) software collection.
*
*  Status:  support routine.
*
*  Given:
*     RH              d      Hipparcos RA (radians)
*     DH              d      Hipparcos Dec (radians)
*     DATE1,DATE2     d      TDB date (Note 1)
*
*  Returned (all FK5, equinox J2000, date DATE1+DATE2):
*     R5              d      RA (radians)
*     D5              d      Dec (radians)
*     DR5             d      FK5 RA proper motion (rad/year, Note 4)
*     DD5             d      Dec proper motion (rad/year, Note 4)
*
*  Notes:
*
*  1) The date DATE1+DATE2 is a Julian Date, apportioned in any
*     convenient way between the two arguments.  For example,
*     JD(TDB)=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 proper motion in RA is dRA/dt rather than cos(Dec)*dRA/dt.
*
*  3) The FK5 to Hipparcos transformation is modeled as a pure
*     rotation and spin;  zonal errors in the FK5 catalogue are
*     not taken into account.
*
*  4) It was the intention that Hipparcos should be a close
*     approximation to an inertial frame, so that distant objects
*     have zero proper motion;  such objects have (in general)
*     non-zero proper motion in FK5, and this routine returns those
*     fictitious proper motions.
*
*  5) The position returned by this routine is in the FK5 J2000
*     reference system but at date DATE1+DATE2.
*
*  6) See also iau_FK52H, iau_H2FK5, iau_FK5ZHZ.
*
*  Called:
*     iau_S2C      spherical coordinates to unit vector
*     iau_FK5HIP   FK5 to Hipparcos rotation and spin
*     iau_RXP      product of r-matrix and p-vector
*     iau_SXP      multiply p-vector by scalar
*     iau_RXR      product of two r-matrices
*     iau_TRXP     product of transpose of r-matrix and p-vector
*     iau_PXP      vector product of two p-vectors
*     iau_PV2S     pv-vector to spherical
*     iau_ANP      normalize angle into range 0 to 2pi
*
*  Reference:
*
*     F.Mignard & M.Froeschle, Astron. Astrophys. 354, 732-739 (2000).
*
*  This revision:  2008 May 24
*
*  Copyright (C) 2008 IAU SOFA Review Board.  See notes at end.
*
*-----------------------------------------------------------------------

      IMPLICIT NONE

      DOUBLE PRECISION RH, DH, DATE1, DATE2, R5, D5, DR5, DD5

*  Reference epoch (J2000), JD
      DOUBLE PRECISION DJ00
      PARAMETER ( DJ00 = 2451545D0 )

*  Days per Julian year
      DOUBLE PRECISION DJY
      PARAMETER ( DJY = 365.25D0 )

      DOUBLE PRECISION T, PH(3), R5H(3,3), S5H(3), SH(3), VST(3),
     :                 RST(3,3), R5HT(3,3), PV5E(3,2), VV(3),
     :                 W, R, V

      DOUBLE PRECISION iau_ANP

* - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

*  Time interval from fundamental epoch J2000.0 to given date (JY).
      T = ( ( DATE1-DJ00 ) + DATE2 ) / DJY

*  Hipparcos barycentric position vector (normalized).
      CALL iau_S2C ( RH, DH, PH )

*  FK5 to Hipparcos orientation matrix and spin vector.
      CALL iau_FK5HIP ( R5H, S5H )

*  Rotate the spin into the Hipparcos system.
      CALL iau_RXP ( R5H, S5H, SH )

*  Accumulated Hipparcos wrt FK5 spin over that interval.
      CALL iau_SXP ( T, S5H, VST )

*  Express the accumulated spin as a rotation matrix.
      CALL iau_RV2M ( VST, RST )

*  Rotation matrix:  accumulated spin, then FK5 to Hipparcos.
      CALL iau_RXR ( R5H, RST, R5HT )

*  De-orient & de-spin the Hipparcos position into FK5 J2000.
      CALL iau_TRXP ( R5HT, PH, PV5E )

*  Apply spin to the position giving a space motion.
      CALL iau_PXP ( SH, PH, VV )

*  De-orient & de-spin the Hipparcos space motion into FK5 J2000.
      CALL iau_TRXP ( R5HT, VV, PV5E(1,2) )

*  FK5 position/velocity pv-vector to spherical.
      CALL iau_PV2S ( PV5E, W, D5, R, DR5, DD5, V )
      R5 = iau_ANP ( W )

*  Finished.

*+-----------------------------------------------------------------------
*
*  Copyright (C) 2008
*  Standards Of Fundamental Astronomy Review 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.
*
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*
*  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 
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*
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*
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*-----------------------------------------------------------------------

      END