USGS

Isis 2 Documentation


mar10cal Documentation

mar10cal - Radiometric correction of Mariner 10 images (Experimental)
MAR10CAL performs a dark curent correction and linearization of
Mariner 10 images.  Key documents to refer to:

  MVM 73 TV Subsystem Calibration Report, M. Benesh and M. Morrill,
    JPL 615-148, 1973.
  Acquisition and Description of Mariner 10 Television Science Data
    at Mercury, G.E. Danielson, K.P. Klaasen, J.L. Anderson, Jour.
    Geophys. Research, Vol. 80, No. 17, pp 2357-2393, 1975 (and other
    articles in this issue).

It should be noted that the flat field and sensitivity fluctuates as
a function of vidicon temperature (especially for camera A).
The camera heater was  not functioning during encounters 2 and 3
and thus these encounters use a different calibration than the
1st encounter.  Reliable non-linearity correction is thus available
only for encounter 1 images.

CAUTION:  the program will process the encounter 2 and 3 images but
	the results are not reliable for any quantitative applications
	such as albedo measurements (absolute or relative) or
	photoclinometry.

The situation is not hopeless, much effort has gone into deriving a
fix for the 2nd and 3rd encounter frames and a future update of mar10cal
will incorporate this work.

Programmer:  Tracie Sucharski, U.S.G.S., Flagstaff, and Mark Robinson,
		 Northwestern University

ParmDescriptionDefault
FROM
Input cube file name
 (Default extension is .cub)
NONE
TO
Output cube file name
 (Default extension is .cub)
NONE
COFILE
8-band coefficient file
--
DCFILE
Dark current file
(Optional)
--
MASK
Uses a range of values to decide
whether to process a pixel
YES
BLEMMASK
Apply blemish removal mask
YES
XPARM
Approximation for iterative
solution
75.0
ABSCOEF
Absolute sensitivity coefficient
--
EXPOFF
Exposure offset
(added to exposure)
--
OTYPE
Output pixel type
 NULL = input type
    1 = 8 bit
    2 = 16 bit
    3 = 32 bit
3
ORANGE
Output min/max data range
--
USERNOTE
User comment
" "

ADDITIONAL NOTES:

ParmDescription
FROM
Input cube file name.  If the file extension is omitted,
then ".cub" will be assumed.
TO
Output cube file name.  If the file extension is omitted,
then ".cub" will be assumed.
COFILE
A cube file containing the calibration coefficients.  This
file should have eight bands, bands 1-4 are the coefficients
for inverting the third order equation, bands 5-6 are the
minimum and maximum values to process.  Bands 5-6 are only
used if the MASK parameter is set to "YES".  If MASK is set,
pixels with values outside of this range are set to NULL in
the output.  The mask assures that only pixels with dns in
the range of the prelaunch fit are calibrated, dns outside
this range are interpolations and may contain large errors.
In most cases the default should be used and the files
derived from the prelaunch calibration flat fields
will be used.  These files are named -

$ISISMAR10DATA/mariner_10_"First 3 letters of FILTER_NAME"_
	"INSTRUMENT_ID"_coef.cub.

See also
1) Robinson et al., Jour. Geophys. Res., 97, p.18265-18274,
	1992.
2) Robinson and Lucey, Science, 275, p. 197-200, 1997.
3) Robinson et al., abstracts of Lunar Planetary Sci. Conf.
        XXVIII, p. 1187-1188, Lunar and Planetary Inst,
        Houston, TX, 1997.

DCFILE
This parameter allows the user to use an alternate dark
current file. In most cases, the default should be used for
this parameter to indicate the derived dark current file is
to be used.  The name of the derived dark current file is
$ISISMAR10DATA/mariner_10_"INSTRUMENT_ID"_dc.cub.  The
INSTRUMENT_ID wil have a value of "A" or "B".

MASK
If MASK is set to "YES", bands 5-6 are the minimum and
maximum values to process.  Any values outside of this range
are set to NULL in the output file.  Caution should be used
in setting MASK to "NO" - the resulting dns may have less
than optimal radiometric integrity.
ABSCOEF
After dark removal and linearity correction an absolute
coefficent needs to be applied to put the data in units of
radiance.  These coefficents (1 for each camera-filter
combination) are still being refined.  The values are being
derived by forcing global mosaics (photometrically
corrected) to Earth based measurements.

for futher explanation see;

1) Robinson and Lucey, Science, 275, p. 197-200.
2) Robinson et al., abstract of Lunar Planetary Sci. Conf.
        XXVIII, p. 1187-1188, 1997.

contact Mark Robinson at Northwestern University for latest
values.
	robinson@earth.nwu.edu

EXPOFF
Offset to be added to Exposure time.  If the default of
NULL is used the following values are added to the offset:

  Camera A EXPOFF = 0.316 msecs
  Camera B EXPOFF = 3.060 msecs

These values are taken directly from the Benesh and Morrill
JPL calibration document.  They state that there are some
unknowns with these values... Read the section on their
page 38.

OTYPE
Output pixel data type.  Permitted values are:
 NULL = output type is same as input file pixel type
    1 = 8-bit (integer with type conversion parameters)
    2 = 16-bit (integer with type conversion parameters)
    3 = 32-bit (floating point)
When processed data are being written back into the input
file, the output pixel type must be the same as the
existing pixel type in the input file.

ORANGE
Output pixel data range.  If ORANGE is NULL, then the
CORE_BASE and CORE_MULTIPLIER in the output file will be
set to represent the same range of data as the input file.

If OTYPE=1 (8-bit) or OTYPE=2 (16-bit), then the CORE_BASE
and CORE_MULTIPLIER in the output file will be set to values
that allow representing the specified range of output
values.  Output values outside this range will be stored as
a special "representation saturation" value.

The ORANGE parameter is ignored if OTYPE=3 (32-bit) since
the CORE_BASE and CORE_MULTIPLIER are not applicable to
floating point pixel values.

**NOTE** For a more detailed explanation of ORANGE, tutor
the orange.pdf.

USERNOTE
Comment from the user.  This will be recorded in the ISIS
session log file and also in the History entry that is put
into the History object of the output file.

Last updated: Jan 31 2005
File: pdfs2.html

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