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Initial performance improvements due to design modifications for the Pointing Control System on the Hubble Space TelescopeShortly after Hubble Space Telescope was deployed on orbit it became apparent that the Pointing Control System was experiencing unexpectedly large disturbances during certain portions of the orbit. While these disturbances were most pronounced during transitions of the Earth's shadow, significant disruptions to the pointing occurred at other times in the orbit. Careful analysis of the flight data has lead to the conclusion that the disturbances are caused by a combination of rapid thermal deformations of the Solar Arrays together with striction-friction mechanisms within the array that randomly release stored thermal/mechanical energy. This paper describes the baseline pointing control system design and the flight data that characterized the effects of the extraneous disturbances. The paper goes on to describe the procedure for modifying the onboard controller to attenuate the disturbances to levels consistent with the science operations. Flight data demonstrating the improved performance are shown and are tabulated to compare performance prior to and after phase I of the redesign.
Document ID
19930031608
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nurre, G. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sharkey, J. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Waites, H. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Guidance and control 1991; Proceedings of the Annual Rocky Mountain Guidance and Control Conference, Keystone, CO, Feb. 2-6, 1991 (A93-15576 03-12)
Publisher: Univelt, Inc.
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 91-071
Report Number: AAS PAPER 91-071
Accession Number
93A15605
Distribution Limits
Public
Copyright
Other

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