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A computer system for geosynchronous satellite navigationA computer system specifically designed to estimate and predict Geostationary Operational Environmental Satellite (GOES-4) navigation parameters using Earth imagery is described. The estimates are needed for spacecraft maneuvers while prediction provide the capability for near real-time image registration. System software is composed of four functional subsystems: (1) data base management; (2) image processing; (3) navigation; and (4) output. Hardware consists of a host minicomputer, a cathode ray tube terminal, a graphics/video display unit, and associated input/output peripherals. System validity is established through the processing of actual imagery obtained by sensors on board the Synchronous Meteorological Satellite (SMS-2). Results indicate the system is capable of operationally providing both accurate GOES-4 navigation estimates and images with a potential registration accuracy of several picture elements (pixels).
Document ID
19810010681
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Koch, D. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-82063
Meeting Information
Meeting: IEEE Position Location and Navigation Symp. (PLANS 80)
Location: Atlantic City, NJ
Country: United States
Start Date: December 8, 1980
End Date: December 11, 1980
Accession Number
81N19208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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