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A simplified dynamic model of the Space Shuttle main engineA simplified 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
19910014027
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duyar, Ahmet (Florida Atlantic Univ. Boca Raton., United States)
Eldem, Vasfi (Florida Atlantic Univ. 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
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Engineering (General)
Report/Patent Number
E-6133
NAS 1.15:104421
NASA-TM-104421
Meeting Information
Meeting: 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
91N23340
Funding Number(s)
PROJECT: RTOP 582-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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