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cspice_dazldr

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


Abstract


   CSPICE_DAZLDR computes the Jacobian matrix of the transformation from
   rectangular to azimuth/elevation coordinates.

I/O


   Given:

      x,
      y,
      z        the rectangular coordinates of the point at which the Jacobian
               matrix of the map from rectangular to azimuth/elevation
               coordinates is desired.

               help, x
                  DOUBLE = Scalar
               help, y
                  DOUBLE = Scalar
               help, z
                  DOUBLE = Scalar

      azccw    a flag indicating how the azimuth is measured.

               help, azccw
                  BOOLEAN = Scalar

               If `azccw' is True, the azimuth increases in the
               counterclockwise direction; otherwise it increases
               in the clockwise direction.

      elplsz   a flag indicating how the elevation is measured.

               help, elplsz
                  BOOLEAN = Scalar

               If `elplsz' is True, the elevation increases from the
               XY plane toward +Z; otherwise toward -Z.

   the call:

      cspice_dazldr, x, y, z, azccw, elplsz, jacobi

   returns:

      jacobi   the matrix of partial derivatives of the transformation from
               rectangular to azimuth/elevation coordinates.

               help, jacobi
                  DOUBLE = Array[3,3]

               It has the form

                  .-                            -.
                  |  dr/dx     dr/dy     dr/dz   |
                  |                              |
                  |  daz/dx    daz/dy    daz/dz  |
                  |                              |
                  |  del/dx    del/dy    del/dz  |
                  `-                            -'

                evaluated at the input values of `x', `y', and `z'.

Parameters


   None.

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) Find the azimuth/elevation state of Venus as seen from the
      DSS-14 station at a given epoch. Map this state back to
      rectangular coordinates as a check.

      Task description
      ================

      In this example, we will obtain the apparent state of Venus as
      seen from the DSS-14 station in the DSS-14 topocentric
      reference frame. We will use a station frames kernel and
      transform the resulting rectangular coordinates to azimuth,
      elevation and range and its derivatives using cspice_recazl and
      cspice_dazldr.

      We will map this state back to rectangular coordinates using
      cspice_azlrec and cspice_drdazl.

      In order to introduce the usage of the logical flags `azccw'
      and `elplsz', we will request the azimuth to be measured
      clockwise and the elevation positive towards +Z
      axis of the DSS-14_TOPO reference frame.

      Kernels
      =======

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


         KPL/MK

         File name: dazldr_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
            ---------                        --------
            de430.bsp                        Planetary ephemeris
            naif0011.tls                     Leapseconds
            earth_720101_070426.bpc          Earth historical
                                                binary PCK
            earthstns_itrf93_050714.bsp      DSN station SPK
            earth_topo_050714.tf             DSN station FK

         \begindata

         KERNELS_TO_LOAD = ( 'de430.bsp',
                             'naif0011.tls',
                             'earth_720101_070426.bpc',
                             'earthstns_itrf93_050714.bsp',
                             'earth_topo_050714.tf'         )

         \begintext

         End of meta-kernel.


      Example code begins here.


      PRO dazldr_ex1

         ;;
         ;; Local parameters
         ;;
         FMT1       = '(A,F20.8)'
         META       = 'dazldr_ex1.tm'

         SPICEFALSE = 0B
         SPICETRUE  = 1B

         ;;
         ;; Load SPICE kernels.
         ;;
         cspice_furnsh, META

         ;;
         ;; Convert the observation time to seconds past J2000 TDB.
         ;;
         obstim = '2003 OCT 13 06:00:00.000000 UTC'

         cspice_str2et, obstim, et

         ;;
         ;; Set the target, observer, observer frame, and
         ;; aberration corrections.
         ;;
         target = 'VENUS'
         obs    = 'DSS-14'
         ref    = 'DSS-14_TOPO'
         abcorr = 'CN+S'

         ;;
         ;; Compute the observer-target state.
         ;;
         cspice_spkezr, target, et, ref, abcorr, obs, state, ltime

         ;;
         ;; Convert position to azimuth/elevation coordinates,
         ;; with azimuth increasing clockwise and elevation
         ;; positive towards +Z axis of the DSS-14_TOPO
         ;; reference frame
         ;;
         azccw  = SPICEFALSE
         elplsz = SPICETRUE

         cspice_recazl, state[0:2], azccw, elplsz, r, az, el

         ;;
         ;; Convert velocity to azimuth/elevation coordinates.
         ;;
         cspice_dazldr, state[0], state[1], state[2], azccw, elplsz, jacobi

         cspice_mxv, jacobi, state[3:5], azlvel

         ;;
         ;; As a check, convert the azimuth/elevation state back to
         ;; rectangular coordinates.
         ;;
         cspice_azlrec, r, az, el, azccw, elplsz, rectan

         cspice_drdazl, r, az, el, azccw, elplsz, jacobi

         cspice_mxv, jacobi, azlvel, drectn

         print
         print, format='(A)', 'AZ/EL coordinates:'
         print
         print, format=FMT1, '   Range      (km)        = ', r
         print, format=FMT1, '   Azimuth    (deg)       = ',                 $
                             az * cspice_dpr()
         print, format=FMT1, '   Elevation  (deg)       = ',                 $
                             el * cspice_dpr()
         print
         print, format='(A)', 'AZ/EL velocity:'
         print
         print, format=FMT1, '   d Range/dt     (km/s)  = ', azlvel[0]
         print, format=FMT1, '   d Azimuth/dt   (deg/s) = ',                 $
                             azlvel[1] * cspice_dpr()
         print, format=FMT1, '   d Elevation/dt (deg/s) = ',                 $
                             azlvel[2] * cspice_dpr()
         print
         print, format='(A)', 'Rectangular coordinates:'
         print
         print, format=FMT1, '   X (km)                 = ', state[0]
         print, format=FMT1, '   Y (km)                 = ', state[1]
         print, format=FMT1, '   Z (km)                 = ', state[2]
         print
         print, format='(A)', 'Rectangular velocity:'
         print
         print, format=FMT1, '   dX/dt (km/s)           = ', state[3]
         print, format=FMT1, '   dY/dt (km/s)           = ', state[4]
         print, format=FMT1, '   dZ/dt (km/s)           = ', state[5]
         print
         print, format='(A)', 'Rectangular coordinates from inverse mapping:'
         print
         print, format=FMT1, '   X (km)                 = ', rectan[0]
         print, format=FMT1, '   Y (km)                 = ', rectan[1]
         print, format=FMT1, '   Z (km)                 = ', rectan[2]
         print
         print, format='(A)', 'Rectangular velocity from inverse mapping:'
         print
         print, format=FMT1, '   dX/dt (km/s)           = ', drectn[0]
         print, format=FMT1, '   dY/dt (km/s)           = ', drectn[1]
         print, format=FMT1, '   dZ/dt (km/s)           = ', drectn[2]
         print

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

      END


      When this program was executed on a Mac/Intel/IDL8.x/64-bit
      platform, the output was:


      AZ/EL coordinates:

         Range      (km)        =   245721478.99272084
         Azimuth    (deg)       =         294.48543372
         Elevation  (deg)       =         -48.94609726

      AZ/EL velocity:

         d Range/dt     (km/s)  =          -4.68189834
         d Azimuth/dt   (deg/s) =           0.00402256
         d Elevation/dt (deg/s) =          -0.00309156

      Rectangular coordinates:

         X (km)                 =    66886767.37916667
         Y (km)                 =   146868551.77222887
         Z (km)                 =  -185296611.10841590

      Rectangular velocity:

         dX/dt (km/s)           =        6166.04150307
         dY/dt (km/s)           =      -13797.77164550
         dZ/dt (km/s)           =       -8704.32385654

      Rectangular coordinates from inverse mapping:

         X (km)                 =    66886767.37916658
         Y (km)                 =   146868551.77222890
         Z (km)                 =  -185296611.10841590

      Rectangular velocity from inverse mapping:

         dX/dt (km/s)           =        6166.04150307
         dY/dt (km/s)           =      -13797.77164550
         dZ/dt (km/s)           =       -8704.32385654


Particulars


   When performing vector calculations with velocities it is
   usually most convenient to work in rectangular coordinates.
   However, once the vector manipulations have been performed
   it is often desirable to convert the rectangular representations
   into azimuth/elevation coordinates to gain insights about
   phenomena in this coordinate system.

   To transform rectangular velocities to derivatives of coordinates
   in an azimuth/elevation coordinate system, one uses the Jacobian
   matrix of the transformation between the two systems.

   Given a state in rectangular coordinates

      ( x, y, z, dx, dy, dz )

   the corresponding azimuth/elevation coordinate derivatives are
   given by the matrix equation:

                    t          |                      t
      (dr, daz, del)   = jacobi|        * (dx, dy, dz)
                               |(x,y,z)

   This routine computes the matrix

            |
      jacobi|
            |(x, y, z)

   In the azimuth/elevation coordinate system, several conventions
   exist on how azimuth and elevation are measured. Using the `azccw'
   and `elplsz' flags, users indicate which conventions shall be used.
   See the descriptions of these input arguments for details.

Exceptions


   1)  If the input point is on the Z-axis ( x = 0 and y = 0 ), the
       Jacobian matrix is undefined and therefore, the error
       SPICE(POINTONZAXIS) is signaled by a routine in the call tree
       of this routine.

   2)  If any of the input arguments, `x', `y', `z', `azccw' or
       `elplsz', is undefined, an error is signaled by the IDL error
       handling system.

   3)  If any of the input arguments, `x', `y', `z', `azccw' or
       `elplsz', is not of the expected type, or it does not have the
       expected dimensions and size, an error is signaled by the Icy
       interface.

   4)  If the output argument `jacobi' is not a named variable, an
       error is signaled by the Icy interface.

Files


   None.

Restrictions


   None.

Required_Reading


   ICY.REQ

Literature_References


   None.

Author_and_Institution


   J. Diaz del Rio     (ODC Space)

Version


   -Icy Version 1.0.0, 17-JUN-2021 (JDR)

Index_Entries


   Jacobian matrix of AZ/EL w.r.t. rectangular coordinates
   Rectangular to range, azimuth and elevation derivative
   Rectangular to range, AZ and EL velocity conversion



Fri Dec 31 18:43:03 2021