• DocumentCode
    1747128
  • Title

    Establishing ultra-reliability by fault injection experiments

  • Author

    White, Allan L.

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • Volume
    1
  • fYear
    2001
  • fDate
    2001
  • Abstract
    A validation procedure combines field data, arguments-from-design, and fault injection experiments to demonstrate high reliability. This paper covers integrating these elements and deriving results that reduce the fault injection effort. A typical argument about the impossibility of demonstrating ultra reliability by experiment is presented to motivate the emphasis on reducing the experimental effort. An example is used to explain the integration of field data, fault injection, arguments-from-design, and performance monitoring. This validation procedure has stringent requirements, but it is shown that these requirements are common to other procedures. There is an extended analysis on number, type, and time of fault occurrence. These results are applied to a system with an extremely high reliability requirement. They reduce the experimental effort to a moderate level
  • Keywords
    aerospace control; design of experiments; fault diagnosis; fault tolerance; probability; reliability theory; Markov model approach comparison; arguments-from-design; binomial sampling; fault injection experiments; fault tolerance; infeasibility argument; integration of field data; natural life experiment; performance monitoring; probability derivations; stringent requirements; ultrahigh reliability; validation procedure; Aerospace control; Aerospace electronics; Aircraft; Concrete; Counting circuits; Digital control; Government; Monitoring; NASA; Protection;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2001, IEEE Proceedings.
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-6599-2
  • Type

    conf

  • DOI
    10.1109/AERO.2001.931699
  • Filename
    931699