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Computing and data transmission for the prediction steering of the Goonhilly satellite-communication aerialThe Goonhilly satellite-communication aerial uses an 85-ft. diameter paraboloidal reflector with waveguide feed at the focus. The aerial is movable in azimuth and elevation, and is provided with independent feedback control systems for these two motions. During a satellite pass, the aerial must be steered so that its axis points continuously, and with high accuracy, in the direction of the satellite. Of the various possible methods of achieving this result, that based on prediction of satellite position has been adopted for the first transatlantic communication experiments using the Telstar and Relay satellites. The process by which orbital predictions originating in the USA are converted to substantially continuous real-time azimuth and elevation pointing instructions at Goonhilly is described herein.
Document ID
19670002978
Acquisition Source
Goddard Space Flight Center
Document Type
Contribution to a larger work
Authors
E. C. Seaman
(Post Office Engineering Dept. London, United Kingdom)
W. E. Thompson
(Post Office Engineering Dept. London, United Kingdom)
Date Acquired
August 3, 2013
Publication Date
December 1, 1965
Publication Information
Publication: Telstar I
Publisher: National Aeronautics and Space Administration
Volume: NASA-SP-32/Vol. 4
Issue Publication Date: December 1, 1965
URL: https://ntrs.nasa.gov/citations/19670002972
Subject Category
Communications
Accession Number
67N12307
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
GROUND STATION
COMMUNICATIONS SATELLITE
STEERABLE ANTENNA
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