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A simplified dynamic model of Space Shuttle Main EngineA simplified dynamic model is presented of the Space Shuttle Main Engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at 25 different operating points of SSME. The simplified model was developed for use with a model-based diagnostic scheme for failure detection and diagnostics studies, as well as control design purposes.
Document ID
19920046665
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duyar, Ahmet (NASA Lewis Research Center Cleveland, OH, United States)
Eldem, Vasfi (Florida Atlantic University Boca Raton, United States)
Merrill, Walter (NASA Lewis Research Center Cleveland, OH, United States)
Guo, Ten-Huei (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 1991 American Control Conference
Location: Boston, MA
Country: United States
Start Date: June 26, 1991
End Date: June 28, 1991
Sponsors: American Automatic Control Council
Accession Number
92A29289
Distribution Limits
Public
Copyright
Other

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