• 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