• DocumentCode
    2840398
  • Title

    Design for validation [digital avionics]

  • Author

    Johnson, Sally C. ; Butler, Ricky W.

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • fYear
    1991
  • fDate
    14-17 Oct 1991
  • Firstpage
    487
  • Lastpage
    492
  • Abstract
    Outlines an approach for the development of ultrareliable digital avionics for civil air transports-a design-for-validation philosophy that includes rigorous application of formal methods. The basic concept of the methodology is introduced, and the role of formal methods is explored. System design begins with a detailed description of the system requirements written in a formal, mathematical language. The system design then proceeds in a hierarchical fashion from a highest-level specification of the system down to a detailed implementation level. Therefore, formal methods are applied to the total systems, not just to the individual subsystems, and all interactions between subsystems are formally described and understood. The impact of the design-for-validation philosophy on the system design process is demonstrated by two simple examples
  • Keywords
    aircraft instrumentation; digital instrumentation; reliability; civil air transports; formal methods; highest-level specification; subsystems; ultrareliable digital avionics; Aerospace electronics; Application software; Certification; Computer aided analysis; Design methodology; Engines; Failure analysis; Hardware; NASA; Power system reliability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
  • Conference_Location
    Los Angeles, CA
  • Type

    conf

  • DOI
    10.1109/DASC.1991.177214
  • Filename
    177214