Index Page scs2e_c
A B C D E F G H I J K L M N O P Q R S T U V W X
Procedure Abstract Required_Reading Keywords Brief_I/O Detailed_Input | Detailed_Output Parameters Exceptions Files Particulars Examples | Restrictions Literature_References Author_and_Institution Version Index_Entries
#### Procedure
       void scs2e_c ( SpiceInt          sc,
                      ConstSpiceChar  * sclkch,
                      SpiceDouble     * et      )
#### Abstract
       Convert a spacecraft clock string to ephemeris seconds past
       J2000 (ET).
#### Required_Reading
       SCLK
       TIME
#### Keywords
       CONVERSION
       TIME
#### Brief_I/O
       Variable  I/O  Description
       --------  ---  --------------------------------------------------
       sc         I   NAIF integer code for a spacecraft.
       sclkch     I   An SCLK string.
       et         O   Ephemeris time, seconds past J2000.
#### Detailed_Input
       sc             is a NAIF ID code for a spacecraft, one of whose
                      clock values is represented by sclkch.  The set of
                      supported spacecraft clocks is listed in the SCLK
                      Required Reading.

       sclkch         is a character string representation of the
                      spacecraft clock value that corresponds to ET, for
                      the spacecraft specified by the input argument sc.
                      sclkch is an absolute spacecraft clock time, so
                      partition information should be included in this
                      string.  The precise format of sclkch is specified
                      in the SCLK Required Reading.
#### Detailed_Output
       et             is the epoch, specified as ephemeris seconds past
                      J2000, that corresponds to sclkch.
#### Parameters
       None.
#### Exceptions
       1)  This routine assumes that that an SCLK kernel appropriate
           to the spacecraft clock identified by the input argument SC
           has been loaded.  If an SCLK kernel has not been loaded,
           does not contain all of the required data, or contains
           invalid data, error diagnoses will be performed by routines
           called by this routine.  The output argument et will not
           be modified.

       2)  When using SCLK kernels that map SCLK to a time system other
           than ET (also called barycentric dynamical time---`TDB'), it
           is necessary to have a leapseconds kernel loaded at the time
           this routine is called.  If a leapseconds kernel is required
           for conversion between SCLK and ET but is not loaded, the
           error will be diagnosed by routines called by this routine.
           The output argument et will not be modified.

           The time system that an SCLK kernel maps SCLK to is indicated
           by the variable SCLK_TIME_SYSTEM_nn in the kernel, where nn
           is the negative of the NAIF integer code for the spacecraft.
           The time system used in a kernel is TDB if and only if the
           variable is assigned the value 1.

       3)  Invalid values of sclkch will be diagnosed by routines called
           by this routine.  The output argument et will not be modified.
#### Files
       None.
#### Particulars
       This routine is provided as a convenience; it is simply shorthand
       for the code fragment

          scencd_c ( sc, sclkch, &sclkdp );
          sct2e_c  ( sc, sclkdp, &et     );
#### Examples
       1)  Find the state (position and velocity) of Jupiter, as seen
           from the Galileo spacecraft, at the epoch corresponding to
           the SCLK value

              2 / 3110578:89:09

           The digit "2", followed by the forward slash, indicates that
           the time value is in the second mission partition.

           During program initialization, load the leapseconds and
           SCLK kernels.  We will pretend that these files are named
           "leapseconds.ker" and "gllsclk.ker".  To use this code
           fragment, you must substitute the actual names of these
           kernel files for the names used here.

              /.
              Load leapseconds and SCLK kernels:
              ./
              furnsh_c ( "leapseconds.ker" );
              furnsh_c ( "gllsclk.ker"     );

              /.
              Load an SPK file (again, a fictitious file)
              containing an ephemeris for Jupiter and the
              GLL orbiter's trajectory.
              ./
              spklef_c ( "gllspk.ker", &handle );

              /.
              The Galileo spacecraft ID is -77.  Convert our SCLK
              string to ephemeris seconds past J2000, which is the
              time representation expected by spkez_c.
              ./
              scs2e_c ( -77, "2 / 3110578:89:09", &et );

              /.
              Find the state of Jupiter (body 599) as seen from Galileo
              at time et.  To use spkez_c, you must first load an SPK
              kernel, using the routine spklef_c.
              ./
              spkez_c ( 599, et, refsys, corr, -77, state, &lt );

       2)  Convert a Voyager 2 SCLK value to UTC, using calendar format,
           with 3 digits of precision in the seconds component.

           Again, your initialization code must load the leapseconds
           and SCLK kernels:

              /.
              Load leapseconds and SCLK kernels:
              ./
              furnsh_c ( "leapseconds.ker" );
              furnsh_c ( "vgr2sclk.ker"    );

           To find the UTC value corresponding to Voyager 2 SCLK
           string

              11389.20.768

           you can use the code fragment

              scs2e_c  ( -32,  "11389.29.768",          &et  );
              et2utc_c (  et,  "c",      3,    UTCLEN,  utc  );

           where UTCLEN is a constant indicating the available
           room in the string utc.  A value of 25 characters suffices.
#### Restrictions
       1)  An SCLK kernel appropriate to the spacecraft clock identified
           by SC must be loaded at the time this routine is called.

       2)  If the SCLK kernel used with this routine does not map SCLK
           directly to barycentric dynamical time, a leapseconds kernel
           must be loaded at the time this routine is called.
#### Literature_References
       [1]   SPK Required Reading
#### Author_and_Institution
       N.J. Bachman   (JPL)
#### Version
       -CSPICE Version 1.1.1, 14-AUG-2006   (EDW)

          Replace mention of ldpool_c with furnsh_c.

       -CSPICE Version 1.1.0, 08-FEB-1998 (NJB)

           References to C2F_CreateStr_Sig were removed; code was
           cleaned up accordingly.  String checks are now done using
           the macro CHKFSTR.

       -CSPICE Version 1.0.0, 25-OCT-1997 (NJB)

          Based on SPICELIB Version 1.0.2, 10-APR-1992 (NJB) (WLT)
#### Index_Entries
       spacecraft_clock string to ephemeris time
#### Link to routine scs2e_c source file scs2e_c.c

    Wed Apr  5 17:54:42 2017