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Implementation of a research prototype onboard fault monitoring and diagnosis systemDue to the dynamic and complex nature of in-flight fault monitoring and diagnosis, a research effort was undertaken at NASA Langley Research Center to investigate the application of artificial intelligence techniques for improved situational awareness. Under this research effort, concepts were developed and a software architecture was designed to address the complexities of onboard monitoring and diagnosis. This paper describes the implementation of these concepts in a computer program called FaultFinder. The implementation of the monitoring, diagnosis, and interface functions as separate modules is discussed, as well as the blackboard designed for the communication of these modules. Some related issues concerning the future installation of FaultFinder in an aircraft are also discussed.
Document ID
19880025313
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palmer, Michael T.
(NASA Langley Research Center Hampton, VA, United States)
Abbott, Kathy H.
(NASA Langley Research Center Hampton, VA, United States)
Schutte, Paul C.
(NASA Langley Research Center Hampton, VA, United States)
Ricks, Wendell R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Systems Analysis
Report/Patent Number
AIAA PAPER 87-2777
Meeting Information
Meeting: AIAA Computers in Aerospace Conference
Location: Wakefield, MA
Country: United States
Start Date: October 7, 1987
End Date: October 9, 1987
Accession Number
88A12540
Distribution Limits
Public
Copyright
Other

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