DocumentCode
2592851
Title
Avionics system design for testability using a knowledge engineering approach
Author
Hallenbeck, Jill J. ; Kanopoulos, Nick
Author_Institution
Res. Triangle Inst., Research Triangle Park, NC, USA
fYear
1990
fDate
15-18 Oct 1990
Firstpage
260
Lastpage
264
Abstract
The authors present a design methodology and a knowledge-based computer-aided design (CAD) environment that allows an avionics system designer to incorporate testability into a design in a formal, verifiable way which also provides clear documentation for this activity. Prototype CAD tools have been built and have met with in-house use success. The design and implementation of the current prototype tools, collectively known as the test engineer´s assistant (TEA,) tools, are presented, along with an example application. All outline of a more robust system which should provide users with a more comprehensive environment with enhanced capabilities to better meet the challenges posed by the design methodology presented is given. In addition, the impact of using testability design tool´s to potentially reduce life cycle costs is discussed
Keywords
CAD; aerospace computing; aerospace testing; aircraft instrumentation; knowledge based systems; programming environments; CAD tools; aerospace testing; avionics system design; documentation; knowledge engineering; knowledge-based computer-aided design; life cycle costs; prototype CAD tools; test engineer´s assistant; testability; Aerospace electronics; Costs; Design automation; Design engineering; Design methodology; Documentation; Life testing; Prototypes; Robustness; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location
Virginia Beach, VA
Type
conf
DOI
10.1109/DASC.1990.111295
Filename
111295
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