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A rule-based system for real-time analysis of control systemsAn approach to automate the real-time analysis of flight critical health monitoring and system status is being developed and evaluated at the NASA Dryden Flight Research Facility. A software package was developed in-house and installed as part of the extended aircraft interrogation and display system. This design features a knowledge-base structure in the form of rules to formulate interpretation and decision logic of real-time data. This technique has been applied for ground verification and validation testing and flight testing monitoring where quick, real-time, safety-of-flight decisions can be very critical. In many cases post processing and manual analysis of flight system data are not required. The processing is described of real-time data for analysis along with the output format which features a message stack display. The development, construction, and testing of the rule-driven knowledge base, along with an application using the X-31A flight test program, are presented.
Document ID
19930002431
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Larson, Richard R.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Millard, D. Edward
(Computer Sciences Corp. Edwards AFB, CA., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Engineering (General)
Report/Patent Number
H-1859
NAS 1.15:104258
NASA-TM-104258
Meeting Information
Meeting: IEEE/AIAA Digital Avionics Systems Conference
Location: Seattle, WA
Country: United States
Start Date: October 5, 1992
End Date: October 8, 1992
Accession Number
93N11619
Funding Number(s)
PROJECT: RTOP 505-64-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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