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Qualitative model-based diagnostics for rocket systemsA diagnostic software package is currently being developed at NASA LeRC that utilizes qualitative model-based reasoning techniques. These techniques can provide diagnostic information about the operational condition of the modeled rocket engine system or subsystem. The diagnostic package combines a qualitative model solver with a constraint suspension algorithm. The constraint suspension algorithm directs the solver's operation to provide valuable fault isolation information about the modeled system. A qualitative model of the Space Shuttle Main Engine's oxidizer supply components was generated. A diagnostic application based on this qualitative model was constructed to process four test cases: three numerical simulations and one actual test firing. The diagnostic tool's fault isolation output compared favorably with the input fault condition.
Document ID
19930065677
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maul, William
(NASA Lewis Research Center Cleveland, OH, United States)
Meyer, Claudia
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Jankovsky, Amy
(NASA Lewis Research Center Cleveland, OH, United States)
Fulton, Christopher
(Analex Corp. Brook Park, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-1779
Report Number: AIAA PAPER 93-1779
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, AIAA, SAE, ASEE
Accession Number
93A49674
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

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