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Research study on stabilization and control: Modern sampled data control theoryA numerical analysis of spacecraft stability parameters was conducted. The analysis is based on a digital approximation by point by point state comparison. The technique used is that of approximating a continuous data system by a sampled data model by comparison of the states of the two systems. Application of the method to the digital redesign of the simplified one axis dynamics of the Skylab is presented.
Document ID
19730014088
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuo, B. C.
(Systems Research Labs., Inc. Champaign, IL, United States)
Singh, G.
(Systems Research Labs., Inc. Champaign, IL, United States)
Yackel, R. A.
(Systems Research Labs., Inc. Champaign, IL, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-124223
Report Number: NASA-CR-124223
Accession Number
73N22815
Funding Number(s)
CONTRACT_GRANT: NAS8-28584
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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