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Identification and interpretation of patterns in rocket engine data: Artificial intelligence and neural network approachesThis paper describes an expert system which is designed to perform automatic data analysis, identify anomalous events, and determine the characteristic features of these events. We have employed both artificial intelligence and neural net approaches in the design of this expert system. The artificial intelligence approach is useful because it provides (1) the use of human experts' knowledge of sensor behavior and faulty engine conditions in interpreting data; (2) the use of engine design knowledge and physical sensor locations in establishing relationships among the events of multiple sensors; (3) the use of stored analysis of past data of faulty engine conditions; and (4) the use of knowledge-based reasoning in distinguishing sensor failure from actual faults. The neural network approach appears promising because neural nets (1) can be trained on extremely noisy data and produce classifications which are more robust under noisy conditions than other classification techniques; (2) avoid the necessity of noise removal by digital filtering and therefore avoid the need to make assumptions about frequency bands or other signal characteristics of anomalous behavior; (3) can, in effect, generate their own feature detectors based on the characteristics of the sensor data used in training; and (4) are inherently parallel and therefore are potentially implementable in special-purpose parallel hardware.
Document ID
19960022971
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Ali, Moonis
(Tennessee Univ. Space Inst. Tullahoma, TN United States)
Whitehead, Bruce
(Tennessee Univ. Space Inst. Tullahoma, TN United States)
Gupta, Uday K.
(Tennessee Univ. Space Inst. Tullahoma, TN United States)
Ferber, Harry
(Tennessee Univ. Space Inst. Tullahoma, TN United States)
Date Acquired
August 17, 2013
Publication Date
October 26, 1989
Publication Information
Publication: Overview of the Center for Advanced Space Propulsion
Subject Category
Cybernetics
Accession Number
96N71342
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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