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Space telescope - The next generationThe command handling approach as applied to fine guidance sensor guide star acquisition is described in order to illustrate the flexibility it provides to users of the Space Telescope. User control of pointing operations is detailed, and the pointing control system/fine guidance system interface is depicted along with the guide star acquisition sequence. Reaction wheel interaction with vehicle structural modes and the rate gyro assembly noise level are discussed and some test data are shown.
Document ID
19820062086
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Dougherty, H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Rodoni, C.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Rodden, J.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Tompetrini, K.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Dawson, J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Henry, J.
(Bendix Corp. Guidance Systems Div., Teterboro, NJ, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AAS 82-035
Report Number: AAS 82-035
Meeting Information
Meeting: Guidance and control 1982
Location: Keystone, CO
Country: United States
Start Date: January 30, 1982
End Date: February 3, 1982
Accession Number
82A45621
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

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