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Index Page illum_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
       illum_c ( Illumination angles )

       void illum_c  ( ConstSpiceChar          * target,
                       SpiceDouble               et,
                       ConstSpiceChar          * abcorr,
                       ConstSpiceChar          * obsrvr,
                       ConstSpiceDouble          spoint [3],
                       SpiceDouble             * phase,
                       SpiceDouble             * solar,
                       SpiceDouble             * emissn     )
#### Abstract
       Deprecated: This routine has been superseded by the CSPICE
       routine ilumin_c. This routine is supported for purposes of
       backward compatibility only.

       Find the illumination angles at a specified surface point of a
       target body.
#### Required_Reading
       KERNEL
       NAIF_IDS
       SPK
       TIME
#### Keywords
       GEOMETRY
#### Brief_I/O
       VARIABLE  I/O  DESCRIPTION
       --------  ---  --------------------------------------------------
       target     I   Name of target body.
       et         I   Epoch in ephemeris seconds past J2000.
       abcorr     I   Desired aberration correction.
       obsrvr     I   Name of observing body.
       spoint     I   Body-fixed coordinates of a target surface point.
       phase      O   Phase angle at the surface point.
       solar      O   Solar incidence angle at the surface point.
       emissn     O   Emission angle at the surface point.
#### Detailed_Input
       target      is the name of the target body.  `target' is
                   case-insensitive, and leading and trailing blanks in
                   `target' are not significant. Optionally, you may
                   supply a string containing the integer ID code for
                   the object. For example both "MOON" and "301" are
                   legitimate strings that indicate the moon is the
                   target body.

       et          is the epoch, specified in ephemeris seconds past
                   J2000, at which the apparent illumination angles at
                   the specified surface point on the target body, as
                   seen from the observing body, are to be computed.

       abcorr      is the aberration correction to be used in
                   computing the location and orientation of the
                   target body and the location of the Sun. Possible
                   values are:

                      "NONE"        No aberration correction.

                      "LT"          Correct the position and
                                    orientation of target body for
                                    light time, and correct the
                                    position of the Sun for light
                                    time.

                      "LT+S"        Correct the observer-target vector
                                    for light time and stellar
                                    aberration, correct the
                                    orientation of the target body
                                    for light time, and correct the
                                    target-Sun vector for light time
                                    and stellar aberration.

                      "CN"          Converged Newtonian light time
                                    correction. In solving the light
                                    time equation, the "CN" correction
                                    iterates until the solution
                                    converges (three iterations on all
                                    supported platforms). Whether the
                                    "CN+S" solution is substantially
                                    more accurate than the "LT" solution
                                    depends on the geometry of the
                                    participating objects and on the
                                    accuracy of the input data. In all
                                    cases this routine will execute more
                                    slowly when a converged solution is
                                    computed. See the -Particulars
                                    section of spkezr_c for a discussion
                                    of precision of light time
                                    corrections.

                                    Both the state and rotation of the
                                    target body are corrected for light
                                    time.

                      "CN+S"        Converged Newtonian light time
                                    correction and stellar aberration
                                    correction.

                                    Both the state and rotation of the
                                    target body are corrected for light
                                    time.

       obsrvr      is the name of the observing body. This is typically
                   a spacecraft, the earth, or a surface point on the
                   earth.  `obsrvr' is case-insensitive, and leading and
                   trailing blanks in `obsrvr' are not significant.
                   Optionally, you may supply a string containing the
                   integer ID code for the object. For example both
                   "EARTH" and "399" are legitimate strings that
                   indicate the earth is the observer.

                   `obsrvr' may be not be identical to `target'.

       spoint      is a surface point on the target body, expressed
                   in rectangular body-fixed (body equator and prime
                   meridian) coordinates.  `spoint' need not be visible
                   from the observer's location at time `et'.
#### Detailed_Output
       phase       is the phase angle at `spoint', as seen from `obsrvr'
                   at time `et'. This is the angle between the
                   spoint-obsrvr vector and the spoint-sun vector.
                   Units are radians. The range of `phase' is [0, pi].
                   See -Particulars below for a detailed discussion of
                   the definition.

       solar       is the solar incidence angle at `spoint', as seen
                   from `obsrvr' at time `et'. This is the angle
                   between the surface normal vector at `spoint' and the
                   spoint-sun vector. Units are radians. The range
                   of `solar' is [0, pi]. See -Particulars below for a
                   detailed discussion of the definition.

       emissn      is the emission angle at `spoint', as seen from
                   `obsrvr' at time `et'. This is the angle between the
                   surface normal vector at `spoint' and the
                   spoint-observer vector. Units are radians. The
                   range of `emissn' is [0, pi]. See -Particulars below
                   for a detailed discussion of the definition.
#### Parameters
       None.
#### Exceptions
       1)  If `target' and `obsrvr' are not distinct, the error
           SPICE(BODIESNOTDISTINCT) is signaled by a routine in the call
           tree of this routine.

       2)  If no SPK (ephemeris) data are available for the observer,
           target, and Sun at the time specified by `et', an error is
           signaled by a routine in the call tree of this routine. If
           light time corrections are used, SPK data for the target body
           must be available at the time et - lt, where `lt' is the one-way
           light time from the target to the observer at `et'.
           Additionally, SPK data must be available for the Sun at the
           time et - lt - lt2, where `lt2' is the light time from the Sun
           to the target body at time et - lt.

       3)  If PCK data defining the orientation or shape of the target
           body are unavailable, an error is signaled by a routine in the
           call tree of this routine.

       4)  If no body-fixed frame is associated with the target body, the
           error SPICE(NOFRAME) is signaled by a routine in the call tree
           of this routine.

       5)  If name of target or observer cannot be translated to its NAIF
           ID code, the error SPICE(IDCODENOTFOUND) is signaled by a
           routine in the call tree of this routine.

       6)  If radii for `target' are not found in the kernel pool, an error
           is signaled by a routine in the call tree of this routine.

       7)  If the size of the `target' body radii kernel variable is not
           three, an error is signaled by a routine in the call tree of
           this routine.

       8)  If any of the three `target' body radii is less-than or equal to
           zero, an error is signaled by a routine in the call tree of
           this routine.

       9)  If any of the `target', `abcorr' or `obsrvr' input string
           pointers is null, the error SPICE(NULLPOINTER) is signaled.

       10) If any of the `target', `abcorr' or `obsrvr' input strings has
           zero length, the error SPICE(EMPTYSTRING) is signaled.
#### Files
       No files are input to this routine. However, illum_c expects
       that the appropriate SPK and PCK files have been loaded via
       furnsh_c.
#### Particulars
       The term "illumination angles" refers to following set of
       angles:

          solar incidence angle    Angle between the surface normal at the
                                   specified surface point and the vector
                                   from the surface point to the Sun.

          emission angle           Angle between the surface normal at the
                                   specified surface point and the vector
                                   from the surface point to the observer.

          phase angle              Angle between the vectors from the
                                   surface point to the observing body and
                                   from the surface point to the Sun.

       The diagram below illustrates the geometric relationships defining
       these angles. The labels for the solar incidence, emission, and
       phase angles are "s.i.", "e.", and "phase".

                                                        *
                                                       Sun

                      surface normal vector
                                ._                 _.
                                |\                 /|  Sun vector
                                  \    phase      /
                                   \   .    .    /
                                   .            .
                                     \   ___   /
                                .     \/     \/
                                      _\ s.i./
                               .    /   \   /
                               .   |  e. \ /
           *             <--------------- *  surface point on
        viewing            vector            target body
        location           to viewing
        (observer)         location

       Note that if the target-observer vector, the target normal vector
       at the surface point, and the target-sun vector are coplanar, then
       phase is the sum of incidence and emission. This is rarely true;
       usually

          phase angle  <  solar incidence angle + emission angle

       All of the above angles can be computed using light time
       corrections, light time and stellar aberration corrections, or
       no aberration corrections. The way aberration corrections
       are used is described below.

       Care must be used in computing light time corrections. The
       guiding principle used here is "describe what appears in
       an image." We ignore differential light time; the light times
       from all points on the target to the observer are presumed to be
       equal.

          Observer-target body vector
          ---------------------------

          Let `et' be the epoch at which an observation or remote
          sensing measurement is made, and let et - lt ("lt" stands
          for "light time") be the epoch at which the photons received
          at `et' were emitted from the body (we use the term "emitted"
          loosely here).

          The correct observer-target vector points from the observer's
          location at `et' to the target body's location at et - lt.
          The target-observer vector points in the opposite direction.

          Since light time corrections are not symmetric, the correct
          target-observer vector CANNOT be found by computing the light
          time corrected position of the observer as seen from the
          target body.

          Target body's orientation
          -------------------------

          Using the definitions of `et' and `lt' above, the target
          body's orientation at et - lt is used. The surface
          normal is dependent on the target body's orientation, so
          the body's orientation model must be evaluated for the correct
          epoch.

          Target body -- Sun vector
          -------------------------

          All surface features on the target body will appear in
          a measurement made at `et' as they were at et-lt. In
          particular, lighting on the target body is dependent on
          the apparent location of the Sun as seen from the target
          body at et-lt. So, a second light time correction is used
          in finding the apparent location of the Sun.

       Stellar aberration corrections, when used, are applied as follows:

          Observer-target body vector
          ---------------------------

          In addition to light time correction, stellar aberration is
          used in computing the apparent target body position as seen
          from the observer's location at time `et'. This apparent
          position defines the observer-target body vector.

          Target body-Sun vector
          ----------------------

          The target body-Sun vector is the apparent position of the Sun,
          corrected for light time and stellar aberration, as seen from
          the target body at time et-lt. Note that the target body's
          position is not affected by the stellar aberration correction
          applied in finding its apparent position as seen by the
          observer.

       Once all of the vectors, as well as the target body's
       orientation, have been computed with the proper aberration
       corrections, the element of time is eliminated from the
       computation. The problem becomes a purely geometric one,
       and is described by the diagram above.
#### 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) Find the phase, solar incidence, and emission angles at the
          sub-solar and sub-spacecraft points on Mars as seen from the Mars
          Global Surveyor spacecraft at a user-specified UTC time. Use light
          time and stellar aberration corrections.

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

             KPL/MK

             File: illum_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
                pck00010.tpc                     Planet orientation and
                                                 radii
                naif0011.tls                     Leapseconds
                mgs_ext12_ipng_mgs95j.bsp        MGS ephemeris

             \begindata

                KERNELS_TO_LOAD = ( 'mar097.bsp',
                                    'pck00010.tpc',
                                    'naif0011.tls',
                                    'mgs_ext12_ipng_mgs95j.bsp' )
             \begintext

             End of meta-kernel

          Example code begins here.

          /.
             Program illum_ex1
          ./
          #include <string.h>
          #include <stdio.h>
          #include "SpiceUsr.h"

          int main()
          {
             /.
             Local variables
             ./
             SpiceChar             * obsrvr;
             SpiceChar             * target;
             SpiceChar             * utc;

             SpiceDouble             alt;
             SpiceDouble             et;
             SpiceDouble             sscemi;
             SpiceDouble             sscphs;
             SpiceDouble             sscsol;
             SpiceDouble             sslphs;
             SpiceDouble             sslsol;
             SpiceDouble             sslemi;
             SpiceDouble             ssolpt  [3];
             SpiceDouble             sscpt   [3];

             /.
             Load kernels.
             ./
             furnsh_c ( "illum_ex1.tm" );

             /.
             Convert the UTC request time to ET (seconds past J2000 TDB).
             ./
             utc = "2003 AUG 1 12:00:00";

             str2et_c ( utc, &et );

             /.
             Assign observer and target names.  The acronym MGS
             indicates Mars Global Surveyor. See NAIF_IDS for a list
             of names recognized by SPICE.
             ./
             target = "Mars";
             obsrvr = "MGS";

             /.
             Find the sub-solar point on the Earth as seen from
             the MGS spacecraft at et.  Use the "near point"
             style of sub-point definition.  This makes it easy
             to verify the solar incidence angle.
             ./
             subsol_c ( "near point",  target,  et,
                        "LT+S",        obsrvr,  ssolpt  );

             /.
             Now find the sub-spacecraft point.  Use the
             "nearest point" definition of the sub-point
             here---this makes it easy to verify the emission
             angle.
             ./
             subpt_c  ( "near point",  target,  et,
                        "LT+S",        obsrvr,  sscpt,  &alt );

             /.
             Find the phase, solar incidence, and emission
             angles at the sub-solar point on the Earth as seen
             from Mars Observer at time et.
             ./
             illum_c ( target,  et,       "LT+S",    obsrvr,
                       ssolpt,  &sslphs,  &sslsol,   &sslemi );

             /.
             Do the same for the sub-spacecraft point.
             ./
             illum_c ( target,  et,       "LT+S",    obsrvr,
                       sscpt,   &sscphs,  &sscsol,   &sscemi );

             /.
             Convert the angles to degrees and write them out.
             ./
             sslphs *= dpr_c();
             sslsol *= dpr_c();
             sslemi *= dpr_c();

             sscphs *= dpr_c();
             sscsol *= dpr_c();
             sscemi *= dpr_c();

             printf ( "\n"
                      "UTC epoch is %s\n"
                      "\n"
                      "Illumination angles at the sub-solar point:\n"
                      "\n"
                      "Phase angle             (deg):  %f\n"
                      "Solar incidence angle   (deg):  %f\n"
                      "Emission angle          (deg):  %f\n"
                      "\n"
                      "The solar incidence angle should be 0.\n"
                      "The emission and phase angles should be "
                      "equal.\n"
                      "\n"
                      "\n"
                      "Illumination angles at the sub-s/c point:\n"
                      "\n"
                      "Phase angle             (deg):  %f\n"
                      "Solar incidence angle   (deg):  %f\n"
                      "Emission angle          (deg):  %f\n"
                      "\n"
                      "The emission angle should be 0.\n"
                      "The solar incidence and phase angles "
                      "should be equal.\n"
                      "\n"
                      "\n",
                      utc,
                      sslphs,
                      sslsol,
                      sslemi,
                      sscphs,
                      sscsol,
                      sscemi                                    );

             printf ( "\n" );

             return ( 0 );
          }

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

          UTC epoch is 2003 AUG 1 12:00:00

          Illumination angles at the sub-solar point:

          Phase angle             (deg):  149.314573
          Solar incidence angle   (deg):  0.000000
          Emission angle          (deg):  149.314573

          The solar incidence angle should be 0.
          The emission and phase angles should be equal.

          Illumination angles at the sub-s/c point:

          Phase angle             (deg):  121.932334
          Solar incidence angle   (deg):  121.932334
          Emission angle          (deg):  0.000000

          The emission angle should be 0.
          The solar incidence and phase angles should be equal.
#### Restrictions
       None.
#### Literature_References
       None.
#### Author_and_Institution
       C.H. Acton          (JPL)
       N.J. Bachman        (JPL)
       J. Diaz del Rio     (ODC Space)
       B.V. Semenov        (JPL)
#### Version
       -CSPICE Version 1.0.6, 01-NOV-2021 (JDR)

           Edited the header to comply with NAIF standard. Added
           example's problem statement and meta-kernel.

           Added entries #6 and #7 to -Exceptions section.

       -CSPICE Version 1.0.5, 10-JUL-2014 (NJB)

           Discussion of light time corrections was updated. Assertions
           that converged light time corrections are unlikely to be
           useful were removed.

       -CSPICE Version 1.0.4, 19-MAY-2010 (BVS)

           Index lines now state that this routine is deprecated.

       -CSPICE Version 1.0.3, 07-FEB-2008 (NJB)

           -Abstract now states that this routine is deprecated.

       -CSPICE Version 1.0.2, 22-JUL-2004 (NJB)

           Updated header to indicate that the `target' and `observer'
           input arguments can now contain string representations of
           integers.

       -CSPICE Version 1.1.2, 27-JUL-2003 (NJB) (CHA)

           Various header corrections were made. The example program
           was upgraded to use real kernels, and the program's output is
           shown.

       -CSPICE Version 1.1.1, 04-SEP-2002 (NJB)

           Updated -Index_Entries header section. Corrected error in
           erract_c call in header example.

       -CSPICE Version 1.1.0, 24-JUL-2001 (NJB)

           Changed prototype: input spoint is now type
           (ConstSpiceDouble [3]).  Implemented interface macro for
           casting spoint array to const.

       -CSPICE Version 1.0.0, 25-MAY-1999 (NJB)
#### Index_Entries
       DEPRECATED illumination angles
       DEPRECATED lighting angles
       DEPRECATED phase angle
       DEPRECATED emission angle
       DEPRECATED solar incidence angle
#### Link to routine illum_c source file illum_c.c

    Fri Dec 31 18:41:08 2021