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Space Telescope pointing controlThe Space Telescope Pointing Control System is used to slew the optical axis of the telescope from one target star region of the celestial sphere to the next, and to maintain precision pointing on the target star. A digital computer is employed in the processing of attitude and rate sensor data, in order to generate torque commands for the reaction wheels. The System comprises four major elements: a command generator, the electronic control system, attitude update processing, and momentum management. Emphasis is given to control-related flexibility effects of the Space Telescope's solar cell array and vehicle, and the acquisition methodology and development testing employed, in addition to Pointing Control System design features.
Document ID
19830056216
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dougherty, H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Rodoni, C.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Tompetrini, K.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Nakashima, A.
(Bendix Corp. Guidance Systems Div., Teterboro, NJ, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Instrumentation
Meeting Information
Meeting: Automatic control in space 1982
Location: Noordwijkerhout
Country: Netherlands
Start Date: July 5, 1982
End Date: July 9, 1982
Accession Number
83A37434
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

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