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Attitude trackerLine array sensors produce data which has no inherent geometrical continuity. Hence, any platform attitude variation will be evidenced as a distortion when the data lines are displayed in the normal Cartesian raster. Ancillary sensing is required to establish the platform attitude to allow geometric rectification. This is normally provided by inertial or star reference attitude sensors. However, in the absence of such sensors or if performance of them is degraded, the required attitude information is lost. A strawman sensor design is proposed which utilizes small image areas on the ground to provide a series of motion vectors with which the platform attitude can be tracked; this allows the distorted image received by the normal image line sensor to be rectified.
Document ID
19820020860
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Billingsley, F. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: Proc. of the NASA Workshop on Registration and Rectification
Subject Category
Earth Resources And Remote Sensing
Accession Number
82N28736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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