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State space representation of the open-loop dynamics of the Space Shuttle Main EngineA parameter and structure estimation technique for multivariable systems is used to obtain state space representation of open loop dynamics of the Space Shuttle Main Engine (SSME). The parameterization being used is both minimal and unique. The simplified linear models may be used for fault detection studies and control system design and development.
Document ID
19920036983
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Duyar, Ahmet (Florida Atlantic Univ. Boca Raton, FL, United States)
Eldem, Vasfi (Florida Atlantic University Boca Raton, United States)
Merrill, Walter C. (Florida Atlantic Univ. Boca Raton, FL, United States)
Guo, Ten-Huei (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
December 1, 1991
Publication Information
Publication: ASME, Transactions, Journal of Dynamic Systems, Measurement, and Control
Volume: 113
ISSN: 0022-0434
Subject Category
Spacecraft Propulsion And Power
Accession Number
92A19607
Distribution Limits
Public
Copyright
Other

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