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Real-time diagnostics for a reusable rocket engineA hierarchical, decentralized diagnostic system is proposed for the Real-Time Diagnostic System component of the Intelligent Control System (ICS) for reusable rocket engines. The proposed diagnostic system has three layers of information processing: condition monitoring, fault mode detection, and expert system diagnostics. The condition monitoring layer is the first level of signal processing. Here, important features of the sensor data are extracted. These processed data are then used by the higher level fault mode detection layer to do preliminary diagnosis on potential faults at the component level. Because of the closely coupled nature of the rocket engine propulsion system components, it is expected that a given engine condition may trigger more than one fault mode detector. Expert knowledge is needed to resolve the conflicting reports from the various failure mode detectors. This is the function of the diagnostic expert layer. Here, the heuristic nature of this decision process makes it desirable to use an expert system approach. Implementation of the real-time diagnostic system described above requires a wide spectrum of information processing capability. Generally, in the condition monitoring layer, fast data processing is often needed for feature extraction and signal conditioning. This is usually followed by some detection logic to determine the selected faults on the component level. Three different techniques are used to attack different fault detection problems in the NASA LeRC ICS testbed simulation. The first technique employed is the neural network application for real-time sensor validation which includes failure detection, isolation, and accommodation. The second approach demonstrated is the model-based fault diagnosis system using on-line parameter identification. Besides these model based diagnostic schemes, there are still many failure modes which need to be diagnosed by the heuristic expert knowledge. The heuristic expert knowledge is implemented using a real-time expert system tool called G2 by Gensym Corp. Finally, the distributed diagnostic system requires another level of intelligence to oversee the fault mode reports generated by component fault detectors. The decision making at this level can best be done using a rule-based expert system. This level of expert knowledge is also implemented using G2.
Document ID
19930009829
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Guo, T. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Merrill, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Duyar, A.
(Florida Atlantic Univ. Boca Raton., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Cybernetics
Report/Patent Number
NAS 1.15:105792
E-7222
NASA-TM-105792
Report Number: NAS 1.15:105792
Report Number: E-7222
Report Number: NASA-TM-105792
Accession Number
93N19018
Funding Number(s)
PROJECT: RTOP 582-01-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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