• DocumentCode
    918817
  • Title

    Design for validation

  • Author

    Johnson, Sally C. ; Butler, Ricky W.

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • Volume
    7
  • Issue
    1
  • fYear
    1992
  • Firstpage
    38
  • Lastpage
    43
  • Abstract
    An approach is outlined for the development of ultrareliable avionics for civil air transports using 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. The impact of the design-for-validation philosophy on the system design process is then demonstrated by two simple examples. More details about the design-for-validation methodology are then given.<>
  • Keywords
    aircraft instrumentation; reliability; avionics; civil air transports; design-for-validation; formal methods; Aerospace electronics; Application software; Certification; Computer aided analysis; Engines; Failure analysis; Formal specifications; Hardware; NASA; Power system reliability;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.127129
  • Filename
    127129