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Engine Data Interpretation System (EDIS), phase 2A prototype of an expert system was developed which applies qualitative constraint-based reasoning to the task of post-test analysis of data resulting from a rocket engine firing. Data anomalies are detected and corresponding faults are diagnosed. Engine behavior is reconstructed using measured data and knowledge about engine behavior. Knowledge about common faults guides but does not restrict the search for the best explanation in terms of hypothesized faults. The system contains domain knowledge about the behavior of common rocket engine components and was configured for use with the Space Shuttle Main Engine (SSME). A graphical user interface allows an expert user to intimately interact with the system during diagnosis. The system was applied to data taken during actual SSME tests where data anomalies were observed.
Document ID
19920005905
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cost, Thomas L.
(Alabama Univ. Huntsville, AL, United States)
Hofmann, Martin O.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
UAH-ME-91-101
NASA-CR-184279
NAS 1.26:184279
Report Number: UAH-ME-91-101
Report Number: NASA-CR-184279
Report Number: NAS 1.26:184279
Accession Number
92N15123
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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