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The solar array-induced disturbance of the Hubble Space Telescope pointing systemThe investigation of the vibrational disturbances of the Hubble Space Telescope that were discovered soon after deployment in orbit is described in detail. It was found that the disturbances were particularly evident during orbital day-night crossings, and that the magnitudes of the disturbances were considerably larger than the design jitter requirements. This paper describes the process by which the vibrations were characterized and isolated to a particular mechanism. The analysis of the flight data and comparisons with computer simulation results showed that the source of the disturbances was the thermally driven deformation of the solar arrays in conjunction with frictional effects in the array mechanisms. The control system was successfully modified to attenuate the disturbances to tolerable levels pending mechanical and thermal redesign of the solar arrays. The new arrays were installed during the first space telescope servicing mission and, in combination with the enhanced control system algorithm, reduced the disturbances to satisfactory levels.
Document ID
19950021793
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Foster, C. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tinker, M. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nurre, G. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Till, W. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Structural Mechanics
Report/Patent Number
M-782
NAS 1.60:3556
NASA-TP-3556
Report Number: M-782
Report Number: NAS 1.60:3556
Report Number: NASA-TP-3556
Accession Number
95N28214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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