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A knowledge based application of the extended aircraft interrogation and display systemA family of multiple-processor ground support test equipment was used to test digital flight-control systems on high-performance research aircraft. A unit recently built for the F-18 high alpha research vehicle project is the latest model in a series called the extended aircraft interrogation and display system. The primary feature emphasized monitors the aircraft MIL-STD-1553B data buses and provides real-time engineering units displays of flight-control parameters. A customized software package was developed to provide real-time data interpretation based on rules embodied in a highly structured knowledge database. The configuration of this extended aircraft interrogation and display system is briefly described, and the evolution of the rule based package and its application to failure modes and effects testing on the F-18 high alpha research vehicle is discussed.
Document ID
19910022560
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Glover, Richard D.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Larson, Richard R.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Computer Systems
Report/Patent Number
H-1706
NAS 1.15:4327
NASA-TM-4327
Report Number: H-1706
Report Number: NAS 1.15:4327
Report Number: NASA-TM-4327
Accession Number
91N31874
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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