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Space Telescope pointing controlThe Space Telescope, a long life, high performance spacecraft deployed by the Space Shuttle, will carry five scientific instruments on its first mission. Its pointing control system will permit target-to-target maneuvering and precision pointing on a target star to support scientific objectives. Spacecraft attitude control is achieved by onboard computer processing of attitude and rate sensor data to generate reaction wheel torque commands. A momentum management control system is provided to desaturate the reaction wheels. This paper discusses the pointing control system and the control hardware investigations and improvements leading to system design.
Document ID
19840047774
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. Sunnyvale, CA, United States)
Rodden, J.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Tompetrini, K.
(Bendix Corp. Systems Div., Teterboro, NJ, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AAS PAPER 83-365
Report Number: AAS PAPER 83-365
Accession Number
84A30561
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

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