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Identification of Space Shuttle Main Engine dynamicsSystem identification techniques are used to represent the dynamic behavior of the Space Shuttle Main Engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood method.
Document ID
19890066697
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duyar, Ahmet (NASA Lewis Research Center Cleveland, OH, United States)
Guo, Ten-Huei (NASA Lewis Research Center Cleveland, OH, United States)
Merrill, Walter C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 1989 American Control Conference
Location: Pittsburgh, PA
Country: United States
Start Date: June 21, 1989
End Date: June 23, 1989
Accession Number
89A54068
Distribution Limits
Public
Copyright
Other

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