Index of Functions: A B C D E F G H I J K L M N O P Q R S T U V W X
Index Page spkpvn_c
Table of contents
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
       spkpvn_c ( S/P Kernel, position and velocity in native frame )

       void spkpvn_c ( SpiceInt             handle,
                       ConstSpiceDouble     descr [5],
                       SpiceDouble          et,
                       SpiceInt           * ref,
                       SpiceDouble          state [6],
                       SpiceInt           * center    )
#### Abstract
       Return, for a specified SPK segment and time, the state (position
       and velocity) of the segment's target body relative to its center
       of motion.
#### Required_Reading
       SPK
#### Keywords
       EPHEMERIS
#### Brief_I/O
       VARIABLE  I/O  DESCRIPTION
       --------  ---  --------------------------------------------------
       handle     I   File handle.
       descr      I   Segment descriptor.
       et         I   Evaluation epoch.
       ref        O   Segment reference frame ID code.
       state      O   Output state vector.
       center     O   Center of state.
#### Detailed_Input
       handle,
       descr       are, respectively, the file handle assigned to a SPK
                   file and the descriptor for a segment within the file.
                   Together they determine the ephemeris data from which
                   the state of the body is to be computed.

       et          is the epoch (ephemeris time) at which the state
                   is to be computed. `et' is expressed as seconds
                   past J2000 TDB.
#### Detailed_Output
       ref         is the ID code of the reference frame relative to which
                   the state returned by the routine is expressed.

       state       contains the position and velocity, at epoch `et',
                   for the body covered by the specified segment.
                   `state' has six elements: the first three contain the
                   body's position; the last three contain the body's
                   velocity. These vectors are expressed into the
                   specified  reference frame. Units are always km and
                   km/sec.

       center      is the integer ID code of the center of motion for
                   the state.
#### Parameters
       None.
#### Exceptions
       1)  If the segment type is not supported by the current
           version of spkpvn_c, the error SPICE(SPKTYPENOTSUPP)
           is signaled by a routine in the call tree of this routine.
#### Files
       See argument `handle'.
#### Particulars
       For most user applications, the high-level SPK APIs

          spkezr_c
          spkez_c
          spkpos_c
          spkezp_c

       should be used instead of this routine.

       The f2c'd routine spkpvn_ called by spkpvn_c is the most basic of
       the SPK readers, the reader upon which spkezr_c and spkgeo_c, etc.
       are built. spkpvn_c normally should not be called directly except in
       cases where some optimization is required. (That is, where the
       calling program has prior knowledge of the center-barycenter shifts
       to be performed, or a non-standard method of determining the files
       and segments to be used when computing states.)

       This is the only reader that makes distinctions between the
       various segment types in the SPK format. The complete list
       of types currently supported is shown below.

          Type   Description
          ----   -------------------------
             1   Modified Difference Array
             2   Chebyshev (P)
             3   Chebyshev (P,V)
             5   Two body propagation between discrete states
             8   Lagrange interpolation, equally spaced discrete states
             9   Lagrange interpolation, unequally spaced discrete states
            12   Hermite interpolation, equally spaced discrete states
            13   Hermite interpolation, unequally spaced discrete states
            14   Chebyshev Unequally spaced
            15   Precessing Ellipse
            17   Equinoctial Elements
            18   ESOC/DDID Hermite/Lagrange Interpolation
            19   ESOC/DDID Piecewise Interpolation
            21   Extended Modified Difference Array

          The maximum record lengths for each data type currently
          supported are as follows:

                    Data type       Maximum record length
                    ---------       ---------------------
                        1                    71
                        2                    87
                        3                   171
                        5                    15
                        8                   171
                        9                   197
                       12                    87
                       13                    99
                       14                 Variable
                       15                    16
                       17                    12
                       18                   198
                       19                   198
                       21                    96
#### Examples
       The numerical results shown for this example may differ across
       platforms. The results depend on the SPICE kernels used as
       input, the compiler and supporting libraries, and the machine
       specific arithmetic implementation.

       1) In the following code example, an SPK file is searched for
          a segment containing ephemeris data for the Jupiter system
          barycenter at a particular epoch. Using this segment,
          states of the Jupiter system barycenter relative to the
          solar system barycenter are evaluated at a sequence of times.

          This method of state computation minimizes the number of
          segment searches required to obtain requested data, but
          it bypasses the SPK subsystem's state chaining mechanism.

          Use the meta-kernel shown below to load the required SPICE
          kernels.

             KPL/MK

             File name: spkpvn_ex1.tm

             This meta-kernel is intended to support operation of SPICE
             example programs. The kernels shown here should not be
             assumed to contain adequate or correct versions of data
             required by SPICE-based user applications.

             In order for an application to use this meta-kernel, the
             kernels referenced here must be present in the user's
             current working directory.

             The names and contents of the kernels referenced
             by this meta-kernel are as follows:

                File name                     Contents
                ---------                     --------
                de421.bsp                     Planetary ephemeris
                naif0010.tls                  Leapseconds

             \begindata

                KERNELS_TO_LOAD = ( 'de421.bsp',
                                    'naif0010.tls'  )

             \begintext

             End of meta-kernel

          Example code begins here.

          /.
             Program spkpvn_ex1
          ./
          #include <stdio.h>
          #include <stdlib.h>
          #include "SpiceUsr.h"

          int main()
          {
             /.
             Local constants
             ./
             #define FRNMLN   33
             #define META     "spkpvn_ex1.tm"
             #define DSCSIZ   5
             #define ND       2
             #define NI       6
             #define SIDLEN   41
             #define TIMFMT   "YYYY MON DD HR:MN:SC.######::TDB TDB"
             #define TIMLEN   41

             /.
             Local variables
             ./
             SpiceBoolean            found;

             SpiceChar               frname [ FRNMLN ];
             SpiceChar               segid  [ SIDLEN ];
             SpiceChar             * timstr;
             SpiceChar               outstr [ TIMLEN ];

             SpiceDouble             dc     [ ND ] ;
             SpiceDouble             descr  [ DSCSIZ ];
             SpiceDouble             et;
             SpiceDouble             et0;
             SpiceDouble             state  [ 6 ];

             SpiceInt                body;
             SpiceInt                center;
             SpiceInt                handle;
             SpiceInt                i;
             SpiceInt                ic     [ NI ];
             SpiceInt                refID;

             /.
             Load meta-kernel.
             ./
             furnsh_c ( META );

             /.
             Convert starting time to seconds past J2000 TDB.
             ./
             timstr = "2012 APR 27 00:00:00.000 TDB";

             str2et_c ( timstr, &et0 );

             /.
             Find a loaded segment for the Jupiter barycenter
             that covers `et0'.
             ./
             body = 5;
             spksfs_c ( body,    et0,   SIDLEN,
                        &handle, descr, segid,  &found );

             if ( !found )
             {
                setmsg_c ( "No SPK segment available for body # at "
                           "time #."                                );
                errint_c ( "#",  body                               );
                errch_c  ( "#",  timstr                             );
                sigerr_c ( "SPICE(NOSEGMENT)"                       );
             }

             /.
             Unpack the descriptor of the current segment.
             ./
             dafus_c ( descr, 2, 6, dc, ic );

             frmnam_c ( ic[2], FRNMLN, frname );

             printf ( "\n"
                      " Body       = %d\n"
                      " Center     = %d\n"
                      " Frame      = %s\n"
                      " Data type  = %d\n"
                      " Start ET   = %24.17e\n"
                      " Stop ET    = %24.17e\n"
                      " Segment ID = %s\n",
                      (int)ic[0],
                      (int)ic[1],
                      frname,
                      (int)ic[3],
                      dc[0],
                      dc[1],
                      segid                 );

             /.
             Evaluate states at 10-second steps, starting at `et0'
             and continuing for 20 seconds.
             ./

             for ( i = 0;  i < 3;  i++ )
             {
                et = et0 + ( 10.0 * i );

                /.
                Convert `et' to a string for display.
                ./
                timout_c ( et, TIMFMT, TIMLEN, outstr );

                /.
                Attempt to compute a state only if the segment's
                coverage interval contains `et'.
                ./
                if ( et <= dc[1] )
                {
                   /.
                   This segment has data at `et'. Evaluate the
                   state of the target relative to its center
                   of motion.
                   ./
                   spkpvn_c ( handle, descr, et, &refID, state, &center );

                   /.
                   Display the time and state.
                   ./
                   printf ( "\n"
                            " %s\n"
                            "   Position X (km):   %24.17e\n"
                            "   Position Y (km):   %24.17e\n"
                            "   Position Z (km):   %24.17e\n"
                            "   Velocity X (km/s): %24.17e\n"
                            "   Velocity Y (km/s): %24.17e\n"
                            "   Velocity Z (km/s): %24.17e\n",
                            outstr,
                            state[0], state[1], state[2],
                            state[3], state[4], state[5]     );
                }
                else
                {
                   printf ( "\nNo data for body %d found at %s.\n",
                            (int)body,
                            outstr                                 );
                   exit(0);
                }
             }
             return ( 0 );
          }

          When this program was executed on a Mac/Intel/cc/64-bit
          platform, the output was:

           Body       = 5
           Center     = 0
           Frame      = J2000
           Data type  = 2
           Start ET   = -3.16919520000000000e+09
           Stop ET    =  1.69685280000000000e+09
           Segment ID = DE-0421LE-0421

           2012 APR 27 00:00:00.000000 TDB
             Position X (km):    4.64528993982164860e+08
             Position Y (km):    5.41513126156852007e+08
             Position Z (km):    2.20785135624629408e+08
             Velocity X (km/s): -1.03868564830765493e+01
             Velocity Y (km/s):  7.95324700713742416e+00
             Velocity Z (km/s):  3.66185835431306517e+00

           2012 APR 27 00:00:10.000000 TDB
             Position X (km):    4.64528890113592625e+08
             Position Y (km):    5.41513205689313412e+08
             Position Z (km):    2.20785172243209451e+08
             Velocity X (km/s): -1.03868579616041927e+01
             Velocity Y (km/s):  7.95324528430304944e+00
             Velocity Z (km/s):  3.66185765185608103e+00

           2012 APR 27 00:00:20.000000 TDB
             Position X (km):    4.64528786245005608e+08
             Position Y (km):    5.41513285221757650e+08
             Position Z (km):    2.20785208861782461e+08
             Velocity X (km/s): -1.03868594401314791e+01
             Velocity Y (km/s):  7.95324356146845002e+00
             Velocity Z (km/s):  3.66185694939899253e+00
#### Restrictions
       None.
#### Literature_References
       None.
#### Author_and_Institution
       N.J. Bachman        (JPL)
       J. Diaz del Rio     (ODC Space)
       W.L. Taber          (JPL)
       E.D. Wright         (JPL)
#### Version
       -CSPICE Version 1.0.2, 27-AUG-2021 (JDR)

           Edited the header to comply with NAIF standard.

       -CSPICE Version 1.0.1, 12-JUL-2016 (EDW)

           Edit to example program to use "%d" with explicit casts
           to int for printing SpiceInts with printf.

       -CSPICE Version 1.0.0, 05-OCT-2012 (NJB) (WLT)
#### Index_Entries
       position and velocity from ephemeris
       SPK file position and velocity
#### Link to routine spkpvn_c source file spkpvn_c.c

    Fri Dec 31 18:41:12 2021