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An ultrahigh-accuracy body pointing system for the Large Space TelescopeThe Large Space Telescope (LST) program is aimed at placing a three-meter diffraction-limited telescope in a 270-nm orbit to perform astronomical observations that are not possible with earth-based telescopes. A complex simulation model is described which was developed to determine whether the stringent pointing stability requirements could be met. The model (programmed on a hybrid computer) included detailed dynamic representation of control moment gyros (CMGs) and reaction wheels (RWs), including their noise characteristics; dynamic sensor representation (including noise); shockmounts for the CMG actuators; detailed representation of an image motion compensation system; and a detailed flexible body vehicle model. Stability and performance studies based on the simulation model showed that the 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
19750043081
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rybak, S. C.
Mayo, R. A.
(Bendix Corp. Navigation and Control Div., Denver, Colo., United States)
Lieberman, S. I.
Hartter, L. L.
(Bendix Research Laboratories Southfield, Mich., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: International Federation of Automatic Control, Symposium on Automatic Control in Space
Location: Tsakhkadzor
Country: Soviet Union
Start Date: August 26, 1974
End Date: August 31, 1974
Accession Number
75A27153
Funding Number(s)
CONTRACT_GRANT: NAS8-29152
CONTRACT_GRANT: NAS8-28983
Distribution Limits
Public
Copyright
Other

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