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sxform

Table of contents
Procedure
Abstract
Required_Reading
Keywords
Declarations
Brief_I/O
Detailed_Input
Detailed_Output
Parameters
Exceptions
Files
Particulars
Examples
Restrictions
Literature_References
Author_and_Institution
Version

Procedure

     SXFORM ( State Transformation Matrix )

     SUBROUTINE SXFORM ( FROM, TO, ET, XFORM )

Abstract

     Return the state transformation matrix from one frame to
     another at a specified epoch.

Required_Reading

     FRAMES

Keywords

     FRAMES

Declarations

     IMPLICIT NONE

     INCLUDE               'zzctr.inc'

     CHARACTER*(*)         FROM
     CHARACTER*(*)         TO
     DOUBLE PRECISION      ET
     DOUBLE PRECISION      XFORM  ( 6, 6 )

Brief_I/O

     VARIABLE  I/O  DESCRIPTION
     --------  ---  --------------------------------------------------
     FROM       I   Name of the frame to transform from.
     TO         I   Name of the frame to transform to.
     ET         I   Epoch of the state transformation matrix.
     XFORM      O   A state transformation matrix.

Detailed_Input

     FROM     is the name of a reference frame in which a state is
              known.

     TO       is the name of a reference frame in which it is
              desired to represent the state.

     ET       is the epoch in ephemeris seconds past the epoch of
              J2000 (TDB) at which the state transformation matrix
              should be evaluated.

Detailed_Output

     XFORM    is the state transformation matrix that transforms
              states from the reference frame FROM to the frame TO
              at epoch ET. If (x, y, z, dx, dy, dz) is a state
              relative to the frame FROM then the vector ( x', y',
              z', dx', dy', dz' ) is the same state relative to the
              frame TO at epoch ET. Here the vector ( x', y', z',
              dx', dy', dz' ) is defined by the equation:

                 .-   -.     .-          -.   .-  -.
                 | x'  |     |            |   | x  |
                 | y'  |     |            |   | y  |
                 | z'  |  =  |   XFORM    |   | z  |
                 | dx' |     |            |   | dx |
                 | dy' |     |            |   | dy |
                 | dz' |     |            |   | dz |
                 `-   -'     `-          -'   `-  -'

Parameters

     None.

Exceptions

     1)  If sufficient information has not been supplied via loaded
         SPICE kernels to compute the transformation between the two
         frames, an error is signaled by a routine in the call tree of
         this routine.

     2)  If either frame FROM or TO is not recognized, the error
         SPICE(UNKNOWNFRAME) is signaled.

Files

     None.

Particulars

     This routine provides the user level interface to computing state
     transformations from one reference frame to another.

     Note that the reference frames may be inertial or non-inertial.
     However, the user must take care that sufficient SPICE kernel
     information is loaded to provide a complete state transformation
     path from the FROM frame to the TO frame.

Examples

     Suppose that you have geodetic coordinates of a station on
     the surface of the earth and that you need the inertial
     (J2000) state of this station. The following code fragment
     illustrates how to transform the position of the station to
     a J2000 state.

        CALL BODVRD ( 'EARTH', RADII, 3, N, ABC  )

        EQUATR   =  ABC(1)
        POLAR    =  ABC(3)
        F        = (EQUATR - POLAR) / EQUATR

        CALL GEOREC ( LONG, LAT, 0.0D0,  EQUATR, F,  ESTATE )

        ESTATE(4) = 0.0D0
        ESTATE(5) = 0.0D0
        ESTATE(6) = 0.0D0

        CALL SXFORM ( 'IAU_EARTH', 'J2000',   ET, XFORM  )
        CALL MXVG   (  XFORM,       ESTATE, 6, 6, JSTATE )

     The state JSTATE is the desired J2000 state of the station.

Restrictions

     None.

Literature_References

     None.

Author_and_Institution

     C.H. Acton         (JPL)
     N.J. Bachman       (JPL)
     J. Diaz del Rio    (ODC Space)
     B.V. Semenov       (JPL)
     W.L. Taber         (JPL)

Version

    SPICELIB Version 1.1.1, 05-JUL-2021 (JDR)

        Edited the header to comply with NAIF standard.

    SPICELIB Version 1.1.0, 23-SEP-2013 (BVS)

        Updated to save the input frame names and POOL state counters
        and to do frame name-ID conversions only if the counters have
        changed.

    SPICELIB Version 1.0.3, 27-FEB-2008 (BVS)

        Added FRAMES to the $Required_Reading section.

    SPICELIB Version 1.0.2, 23-OCT-2005 (NJB)

        Header example had invalid flattening factor computation;
        this was corrected. Reference to BODVAR in header was
        replaced with reference to BODVRD.

    SPICELIB Version 1.0.1, 29-JUL-2003 (NJB) (CHA)

        Minor header changes were made to improve clarity.

    SPICELIB Version 1.0.0, 19-SEP-1995 (WLT)
Fri Dec 31 18:36:58 2021