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Required Reading


   CSPICE_CKGP returns pointing (attitude) for a specified 
   spacecraft clock time.

   For important details concerning this module's function, please refer to
   the CSPICE routine ckgp_c.


      inst     the scalar integer NAIF ID for the instrument, spacecraft, 
               or other structure for which pointing is requested, the 
               frame fixed to this object is called the"instrument frame"
               or "instrument-fixed" frame
      sclkdp   the double precision scalar encoded spacecraft clock time
               for which pointing is being requested.  
      tol      the scalar double precision time tolerance in ticks (+/-),
               the units of encoded spacecraft clock time, about 'sclkdp'
                  The C-matrix returned by cspice_ckgp is the one whose
                  time tag is closest to 'sclkdp' and within 'tol' units
                  of 'sclkdp'.
               In general, because using a non-zero tolerance affects 
               selection of the segment from which the data is obtained, 
               users are strongly discouraged from using a non-zero 
               tolerance when reading CKs with continuous data. Using 
               a non-zero tolerance should be reserved exclusively to 
               reading CKs with discrete data because in practice 
               obtaining data from such CKs using a zero tolerance is 
               often not possible due to time round off. 

      ref      the scalar string name of the desired reference 
               frame for the returned pointing

   the call:
      cspice_ckgp, inst, sclkdp, tol, ref, cmat, clkout, found
      cmat     a double precision, 3x3 rotation matrix that transforms 
               the components of a vector expressed in the frame 
               specified by 'ref' to components expressed in the frame 
               tied to the instrument, spacecraft, or other structure 
               at time 'clkout'
      clkout   the scalar double precision encoded spacecraft clock 
               time associated with the returned C-matrix. (this value 
               may differ from the requested time, but never by more 
               than the input tolerance 'tol')
      found    a scalar boolean with value TRUE when requested 
               pointing is found
   If 'vec_ref' is a double-precision 3-vector defined in reference
   frame 'ref', rotate 'vec_ref' into the instrument frame via:
      vec_inst = cmat ## vec_ref              ;; column vector
      vec_inst = transpose(cmat) # vec_ref    ;; row vector
      cspice_mxv, cmat, vec_ref, vec_inst     ;; row vector


   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.

   Retrieve pointing data from a Voyager 2 CK kernel.
      ;; Constants for this program:
      ;; -- The code for the Voyager 2 spacecraft clock is -32
      ;; -- The code for the narrow angle camera on the Voyager 2
      ;;    spacecraft is -32001.
      ;; --  Spacecraft clock times for successive Voyager images always
      ;;     differ by more than 0:0:400.  This is an acceptable
      ;;     tolerance, and must be converted to "ticks" (units of
      ;;     encoded SCLK) for input to ckgp_c .
      ;; -- The reference frame we want is FK4.
      ;; -- The narrow angle camera boresight has direction 
      ;;    ( 0, 0, 1 ) in camera (instrument) frame.
      SC     =  -32
      INST   =  -32001
      REF    = 'FK4'
      TOLVGR = '0:0:400'
      BORE   = [ 0.d, 0.d, 1.d]
      NPICS  = 2
      CK     = '/kernels/voyager2/ck/vg2_jup_qmw_na.bc'
      SCLK   = '/kernels/voyager2/sclk/vg200004.tsc' 
      SCLKCH =  [ '2/18381:54:768' , '4/08970:58:768' ]
      ;; Load the CK pointing file. 
      cspice_furnsh, CK
      ;; Need to load a Voyager 2 SCLK kernel to convert from 
      ;; clock string to ticks.  Although not required for
      ;; the Voyager spacecraft clocks, most modern spacecraft
      ;; clocks require a leapseconds kernel to be loaded in
      ;; addition to an SCLK kernel.
      cspice_furnsh, SCLK
      ;; Convert tolerance from VGR formatted character string 
      ;; SCLK to ticks, which are units of encoded SCLK. 
      cspice_sctiks, SC, TOLVGR, toltik
      for i = 0, (NPICS-1) do begin
         ;; cspice_ckgp requires encoded spacecraft clock time. 
         cspice_scencd, SC, sclkch[i], sclkdp  
         ;; Retrieve the 'REF' reference frame to 'INST' reference frame
         ;; transformation matrix at time sclkdp with a tolerance 
         ;; 'toltik'.
         ;;   [INST] = [cmat][ref]
         cspice_ckgp, INST, sclkdp, toltik, REF, cmat, clkout, found
         ;; Did we find pointing information within (+/-) 'toltik' of the
         ;; requested time.
         if ( found ) then begin
            ;; Transform the 'BORE' vector from 'INST' reference frame to
            ;; 'REF' frame.
            ;;                T
            ;;  [ref] = [cmat] [INST]
            ;; The Icy code to perform the same operation.
            ;;    cspice_mtxv, cmat, BORE, bore_ref
            bore_ref = cmat # BORE
            print, 'At SCLK time        : ', sclkch[i]
            print, 'The boresight vector: ', bore_ref
         endif else begin
            print, 'Pointing not found for SCLK time: ', sclkch[i]
   IDL outputs (for SCLK = 2/18381:54:768):
      At SCLK time        : 2/18381:54:768
      The boresight vector:  -0.089388922  0.94794277  0.30563724
   IDL outputs (for SCLK = 4/08970:58:768):
      Pointing not found for SCLK time: 4/08970:58:768



Required Reading



   -Icy Version 1.0.2, 03-JUN-2010, BVS (JPL)

       Edits to header. Added warning regarding non-zero tolerance.

   -Icy Version 1.0.1, 09-JUN-2006, EDW (JPL)

       Edits to header. Improved argument descriptions.

   -Icy Version 1.0.0, 16-JUN-2003, EDW (JPL)


   get ck pointing 

Wed Apr  5 17:57:59 2017