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Hubble Space Telescope fine guidance sensor control systemThe fine pointing information required for the extraordinary pointing stability of the Hubble Space Telescope (HST) is provided by the fine guidance sensor (FGS), which is capable of measuring extremely small pointing errors, of the order of 3 milliarcseconds. The FGS provides this fine pointing information over a relatively large, continuous range of angles of guide stars relative to the optical axis of the telescope. The FGS accomplishes this task by a judicious design involving the following: a two-axis high precision star selector servo system; an optical deflection system that provides high reduction from shaft angle to optical angle; a unique interferometer using Koester prisms and extremely sensitive photomultiplier tubes that enable the FGS to lock onto guide stars whose magnitude may be any value over a wide range of brightness (including 14.5 Mv and fainter); and the use the large aperture of the telescope itself to advantage. This paper describes the FGS control systems involved in achieving this performance, supported by test data.
Document ID
19900051968
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nurre, Gerald S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Anhouse, Stanley J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gullapalli, Sarma N.
(Perkin-Elmer Corp. Electro-Optics Technology Div., Danbury, CT, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Astronomy
Meeting Information
Meeting: Acquisition, Tracking, and Pointing III
Location: Orlando, FL
Country: United States
Start Date: March 27, 1989
End Date: March 29, 1989
Accession Number
90A39023
Funding Number(s)
CONTRACT_GRANT: NAS8-32700
Distribution Limits
Public
Copyright
Other

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