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Ultrahigh-accuracy body-pointing system for the Large Space TelescopeThe Large Space Telescope (LST) is a 3-m diffraction-limited telescope. Pointing stability requirements necessary to assure diffraction-limited images are plus or minus 0.005 arc-sec, over possible experiment observation times of several hours. In order to determine whether these stringent pointing requirements could be met, a complex simulation model was defined which consisted of detailed dynamic representations of control moment gyros (CMGs) and reaction wheels (RWs), including their noise characteristics, dynamic sensor representations with sensor noise, shock mounts for the CMG actuators, a detailed representation of an image motion compensation (IMC) system, and a detailed flexible body structural model with all significant vehicle and solar panel bending modes. On the basis of both stability and performance studies utilizing this model, it was determined that a body-pointing system will meet LST requirements in the presence of CMG vibrational disturbances and sensor noise. The recommended system consists of three orthogonally mounted RWs for primary short-term control, and a cluster of CMG actuators for continuous RW desaturation and vehicle maneuvering.
Document ID
19760050020
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rybak, S. C.
(Bendix Corp. Denver, CO, United States)
Mayo, R. A.
(Bendix Corp. Denver, Colo., United States)
Lieberman, S. I.
(Bendix Corp. Denver, CO, United States)
Hartter, L. L.
(Bendix Research Laboratories Southfield, Mich., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1976
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 13
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76A32986
Funding Number(s)
CONTRACT_GRANT: NAS8-28983
CONTRACT_GRANT: NAS8-29152
Distribution Limits
Public
Copyright
Other

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