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The TOYSAT structural control experimentThe Lockheed TOYSAT experiment is described. The experiment was designed to test hypothesis concerning the application of optimal control theory to flexible spacecraft. The theory is presented, and results described.
Document ID
19830027806
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Breakwell, J. A.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Chambers, G. J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1983
Publication Information
Publication: JPL Proc. of the Workshop on Appl. of Distributed System Theory to the Control of Large Space Struct.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
83N36077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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