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cspice_spkw09

Table of contents
Abstract
I/O
Parameters
Examples
Particulars
Exceptions
Files
Restrictions
Required_Reading
Literature_References
Author_and_Institution
Version
Index_Entries

Abstract


   CSPICE_SPKW09 writes a type 9 segment to an SPK file.

I/O


   Given:

      handle   the file handle of an SPK file that has been opened for
               writing.

               [1,1] = size(handle); int32 = class(handle)

      body     the NAIF integer code for an ephemeris object whose state
               relative to another body is described by the segment to be
               created.

               [1,1] = size(body); int32 = class(body)

      center   the NAIF integer code for the center of motion of the object
               identified by body.

               [1,1] = size(center); int32 = class(center)

      frame    the NAIF name for a reference frame relative to which the
               state information for body is specified.

               [1,c1] = size(frame); char = class(frame)

                  or

               [1,1] = size(frame); cell = class(frame)

      first,
      last     are, respectively, the start and stop times of the time
               interval over which the segment defines the state of body.

               [1,1] = size(last); double = class(last)

      segid    the segment identifier.

               [1,c2] = size(segid); char = class(segid)

                  or

               [1,1] = size(segid); cell = class(segid)

               An SPK segment identifier may contain up to 40 characters.

      degree   the degree of the Lagrange polynomials used to interpolate
               the states.

               [1,1] = size(degree); int32 = class(degree)

               All components of the state vectors are interpolated by
               polynomials of fixed degree.

      states   contains a time-ordered array of geometric states (x, y, z,
               dx/dt, dy/dt, dz/dt, in kilometers and kilometers per second)
               of body relative to center, specified relative to frame.

               [6,n] = size(states); double = class(states)

      epochs   an array of epochs corresponding to the members of the state
               array.

               [1,n] = size(epochs); double = class(epochs)

               The epochs are specified as seconds past J2000, TDB.

   the call:

      cspice_spkw09( handle, body,   center, frame,  first,  last, ...
                     segid,  degree, states, epochs  )

   returns:

      None.

      See -Particulars for a description of the effect of this routine.

Parameters


   MAXDEG      is the maximum allowed degree of the interpolating
               polynomial.

               The current value of MAXDEG is 15.

Examples


   Any numerical results shown for this example may differ between
   platforms as the results depend on the SPICE kernels used as input
   and the machine specific arithmetic implementation.

   1) Suppose that you have a time-ordered array of geometric states
      of a new object that follows Phobos, with a delay of 1 hour,
      in its orbit around Mars and are prepared to produce a segment
      of type 09 in an SPK file. Create a new SPK file with this
      segment. Use an existing SPK to create the input data for the
      SPK segment.

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


         KPL/MK

         File: spkw09_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
            ---------                        --------
            mar097.bsp                       Mars satellite ephemeris
            naif0012.tls                     Leapseconds

         \begindata

            KERNELS_TO_LOAD = ( 'mar097.bsp',
                                'naif0012.tls' )

         \begintext

         End of meta-kernel


      Example code begins here.


      function spkw09_ex1()

         %
         % Local parameters.
         %
         SPKNAM = 'spkw09_ex1.bsp';
         DEGREE = 3;
         MARS   = 499;
         NEPOCS = 800;
         NOBJ   = 403;

         %
         % Local variables.
         %
         epochs = zeros(NEPOCS,1);
         states = zeros(6,NEPOCS);

         %
         % Load the input SPK file.
         %
         cspice_furnsh( 'spkw09_ex1.tm' );

         %
         % Convert the input UTC to ephemeris time
         %
         [et] = cspice_str2et( '2018 Apr 03 08:35' );

         %
         % Create the time-ordered array of geometric states,
         % at unequal time steps.
         %
         time  = et;
         step  = 60.0;
         delta = 10.0;

         for i=1:NEPOCS

            [states(:,i), lt] = cspice_spkezr( 'PHOBOS', time,  'J2000', ...
                                               'NONE',   'MARS'          );

            epochs(i) = time + 3600.0;
            time      =   time + step                             ...
                        + sin( cspice_halfpi * i / 2.0 ) * delta;

         end

         %
         % Open a new SPK file, with 5000 characters reserved
         % for comments.
         %
         ifname   = 'Test SPK type 9 internal filename.';
         [handle] = cspice_spkopn( SPKNAM, ifname, 5000 );

         %
         % Create a segment identifier.
         %
         segid = 'MY_SAMPLE_SPK_TYPE_9_SEGMENT';

         %
         % Write the segment.
         %
         cspice_spkw09( handle,    NOBJ,           MARS,  'J2000', ...
                        epochs(1), epochs(NEPOCS), segid, DEGREE,  ...
                        states,    epochs                          );

         %
         % Close the new SPK file.
         %
         cspice_spkcls( handle );

         %
         % Compute the state of Phobos as seen from Mars,
         % 12 hours after the input UTC time.
         %
         et = et + 43200.0;
         [state, lt] = cspice_spkezr( 'PHOBOS', et,    'J2000', ...
                                      'NONE',   'MARS'          );

         fprintf( 'Phobos as seen from Mars at t0:\n' )
         fprintf( '   Epoch       (s): %19.5f\n', et )
         fprintf( '   Position   (km): %13.5f %13.5f %13.5f\n', ...
                                   state(1), state(2), state(3) )
         fprintf( '   Velocity (km/s): %13.5f %13.5f %13.5f\n', ...
                                   state(4), state(5), state(6) )
         fprintf( '\n' )

         %
         % Load the newly created kernel, and compute the state
         % of the new object as seen from Mars, 13 hours after
         % the input UTC time.
         %
         cspice_furnsh( SPKNAM );
         et = et + 3600.0;

         [state, lt] = cspice_spkezr( '403', et, 'J2000', 'NONE', 'MARS' );

         fprintf( 'Object 403 as seen from Mars at t0 + 1h:\n' )
         fprintf( '   Epoch       (s): %19.5f\n', et )
         fprintf( '   Position   (km): %13.5f %13.5f %13.5f\n', ...
                                   state(1), state(2), state(3) )
         fprintf( '   Velocity (km/s): %13.5f %13.5f %13.5f\n', ...
                                   state(4), state(5), state(6) )

         %
         % It's always good form to unload kernels after use,
         % particularly in Matlab due to data persistence.
         %
         cspice_kclear


      When this program was executed on a Mac/Intel/Octave6.x/64-bit
      platform, the output was:


      Phobos as seen from Mars at t0:
         Epoch       (s):     576059769.18566
         Position   (km):   -7327.26277    2414.32655    5207.10638
         Velocity (km/s):      -0.94289      -1.89473      -0.39671

      Object 403 as seen from Mars at t0 + 1h:
         Epoch       (s):     576063369.18566
         Position   (km):   -7327.26277    2414.32655    5207.10638
         Velocity (km/s):      -0.94289      -1.89473      -0.39671


      Note that after run completion, a new SPK file exists in
      the output directory.

Particulars


   This routine writes an SPK type 09 data segment to the open SPK
   file according to the format described in the type 09 section of
   the SPK Required Reading. The SPK file must have been opened with
   write access.

Exceptions


   If any of the following exceptions occur, this routine will return
   without creating a new segment.

   1)  If `frame' is not a recognized name, the error
       SPICE(INVALIDREFFRAME) is signaled by a routine in the call
       tree of this routine.

   2)  If the last non-blank character of `segid' occurs past index 40,
       the error SPICE(SEGIDTOOLONG) is signaled by a routine in the
       call tree of this routine.

   3)  If `segid' contains any nonprintable characters, the error
       SPICE(NONPRINTABLECHARS) is signaled by a routine in the call
       tree of this routine.

   4)  If `degree' is not at least 1 or is greater than MAXDEG, the
       error SPICE(INVALIDDEGREE) is signaled by a routine in the
       call tree of this routine.

   5)  If the number of states `n' is not at least degree+1, the
       error SPICE(TOOFEWSTATES) is signaled by a routine in the call
       tree of this routine.

   6)  If `first' is greater than or equal to `last', the error
       SPICE(BADDESCRTIMES) is signaled by a routine in the call tree
       of this routine.

   7)  If the elements of the array `epochs' are not in strictly
       increasing order, the error SPICE(TIMESOUTOFORDER) is
       signaled by a routine in the call tree of this routine.

   8)  If the first epoch, epochs(1), is greater than `first', the
       error SPICE(BADDESCRTIMES) is signaled by a routine in the
       call tree of this routine.

   9)  If the last epoch, epochs(n), where `n' is the number of
       states, is less than `last', the error SPICE(BADDESCRTIMES) is
       signaled by a routine in the call tree of this routine.

   10) If any of the input arguments, `handle', `body', `center',
       `frame', `first', `last', `segid', `degree', `states' or
       `epochs', is undefined, an error is signaled by the Matlab
       error handling system.

   11) If any of the input arguments, `handle', `body', `center',
       `frame', `first', `last', `segid', `degree', `states' or
       `epochs', is not of the expected type, or it does not have the
       expected dimensions and size, an error is signaled by the Mice
       interface.

   12) If the input vector arguments `states' and `epochs' do not
       have the same dimension (n), an error is signaled by the Mice
       interface.

Files


   A new type 9 SPK segment is written to the SPK file attached
   to `handle'.

Restrictions


   None.

Required_Reading


   MICE.REQ
   NAIF_IDS.REQ
   SPC.REQ
   SPK.REQ
   TIME.REQ

Literature_References


   None.

Author_and_Institution


   J. Diaz del Rio     (ODC Space)

Version


   -Mice Version 1.0.0, 26-NOV-2021 (JDR)

Index_Entries


   write SPK type_9 ephemeris data segment


Fri Dec 31 18:44:27 2021