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Onboard image correctionA processor architecture for performing onboard geometric and radiometric correction of LANDSAT imagery is described. The design uses a general purpose processor to calculate the distortion values at selected points in the image and a special purpose processor to resample (calculate distortion at each image point and interpolate the intensity) the sensor output data. A distinct special purpose processor is used for each spectral band. Because of the sensor's high output data rate, 80 M bit per second, the special purpose processors use a pipeline architecture. Sizing has been done on both the general and special purpose hardware.
Document ID
19800019899
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Martin, D. R.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Smaulon, A. S.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Hamori, A. S.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
80N28400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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