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
cspice_psv2pl

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

Abstract


   CSPICE_PSV2PL returns a SPICE plane given a point and two
   spanning vectors.

I/O


   Given:

      point,
      span1,
      span2    respectively, a point and two spanning vectors
               that define a geometric plane in three-dimensional
               space.

               [3,1] = size(point); double = class(point)
               [3,1] = size(span1); double = class(span1)
               [3,1] = size(span2); double = class(span2)

               The plane is the set of vectors

                  point   +   s * span1   +   t * span2

               where `s' and `t' are real numbers. The spanning
               vectors `span1' and `span2' must be linearly
               independent, but they need not be orthogonal or
               unitized.

   the call:

      [plane] = cspice_psv2pl( point, span1, span2 )

   returns:

      plane    a structure describing a SPICE plane defined
               by `point', `span1', and `span2'.

               [1,1] = size(plane); struct = class(plane)

               The structure has the fields:

                  normal:   [3,1] = size(normal);   double = class(normal)
                  constant: [1,1] = size(constant); double = class(constant)

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) Calculate the inclination of the Moon's orbit plane about
      the Earth to the orbit plane of the Earth around the sun.

      Perform geometric analysis, so use no aberration correction
      for the calculation. Use the Ecliptic J2000 frame
      as a conceptual convenience, however the result is invariant
      with respect to an inertial frame.

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


         KPL/MK

         File name: psv2pl_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
            naif0012.tls                  Leapseconds

         \begindata

            KERNELS_TO_LOAD = ( 'de421.bsp',
                                'naif0012.tls'  )

         \begintext

         End of meta-kernel


      Example code begins here.


      function psv2pl_ex1()

         %
         % Local variables.
         %
         epoch = 'Jan 1 2005';
         frame = 'ECLIPJ2000';
         corr  = 'NONE';

         %
         % Load the kernels we need to retrieve state data.
         %
         cspice_furnsh( 'psv2pl_ex1.tm' )

         %
         % Convert the time string to  ephemeris time
         %
         et = cspice_str2et( epoch );

         %
         % Calculate the orbit plane of the Earth about
         % the solar system barycenter at epoch.
         %
         [state, lt] = cspice_spkezr( 'EARTH', et, frame, corr, ...
                                      'Solar System Barycenter' );

         es_plane            = cspice_psv2pl( state(1:3), ...
                                              state(1:3), ...
                                              state(4:6) );
         [es_norm, es_const] = cspice_pl2nvc( es_plane );

         %
         % Calculate the orbit plane of the Moon with respect to
         % the Earth-Moon barycenter at epoch.
         %
         [state, lt] = cspice_spkezr( 'MOON', et, frame, corr, ...
                                       'EARTH BARYCENTER' );

         em_plane            = cspice_psv2pl( state(1:3), ...
                                              state(1:3), ...
                                              state(4:6) );
         [em_norm, em_const] = cspice_pl2nvc( em_plane );

         %
         % Calculate the inclination equals (output in degrees).
         % Depending on the orientation of the plane normals, the
         % cspice_vsep result may exceed 90 degrees. If, so subtract
         % the value off 180 degrees.
         %
         loc_inc = cspice_vsep( es_norm, em_norm );

         if ( loc_inc > cspice_halfpi )
            loc_inc = cspice_pi - loc_inc;
         end

         fprintf( 'Moon-Earth orbit plane inclination (deg): %f\n', ...
                  loc_inc * cspice_dpr )

         %
         % 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:


      Moon-Earth orbit plane inclination (deg): 5.042494


Particulars


   Mice geometry routines that deal with planes use the `plane'
   data type to represent input and output planes. This data type
   makes the subroutine interfaces simpler and more uniform.

   The Mice routines that produce SPICE planes from data that
   define a plane are:

      cspice_nvc2pl ( Normal vector and constant to plane )
      cspice_nvp2pl ( Normal vector and point to plane    )
      cspice_psv2pl ( Point and spanning vectors to plane )

   The Mice routines that convert SPICE planes to data that
   define a plane are:

      cspice_pl2nvc ( Plane to normal vector and constant )
      cspice_pl2nvp ( Plane to normal vector and point    )
      cspice_pl2psv ( Plane to point and spanning vectors )

   Any of these last three routines may be used to convert this
   routine's output, 'plane', to another representation of a
   geometric plane.

Exceptions


   1)  If `span1' and `span2' are linearly dependent, i.e. the vectors
       `point', `span1', and `span2' do not define a plane, the error
       SPICE(DEGENERATECASE) is signaled by a routine in the call
       tree of this routine.

   2)  If any of the input arguments, `point', `span1' or `span2', is
       undefined, an error is signaled by the Matlab error handling
       system.

   3)  If any of the input arguments, `point', `span1' or `span2', is
       not of the expected type, or it does not have the expected
       dimensions and size, an error is signaled by the Mice
       interface.

Files


   None.

Restrictions


   None.

Required_Reading


   MICE.REQ
   PLANES.REQ

Literature_References


   [1]  G. Thomas and R. Finney, "Calculus and Analytic Geometry,"
        7th Edition, Addison Wesley, 1988.

Author_and_Institution


   J. Diaz del Rio     (ODC Space)
   E.D. Wright         (JPL)

Version


   -Mice Version 1.1.0, 10-AUG-2021 (EDW) (JDR)

       Edited the -Examples section to comply with NAIF standard. Added
       example's problem statement and meta-kernel. Added a call to
       cspice_kclear to code example.

       Added -Parameters, -Exceptions, -Files, -Restrictions,
       -Literature_References and -Author_and_Institution sections.

       Eliminated use of "lasterror" in rethrow.

       Removed reference to the function's corresponding CSPICE header from
       -Required_Reading section.

   -Mice Version 1.0.0, 27-AUG-2012 (EDW)

Index_Entries


   plane to point and spanning vectors


Fri Dec 31 18:44:26 2021