• DocumentCode
    2593397
  • Title

    An error bound for instantaneous coverage

  • Author

    White, Allan L.

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • fYear
    1991
  • fDate
    29-31 Jan 1991
  • Firstpage
    587
  • Lastpage
    591
  • Abstract
    An error bound is derived for a reliability model approximation method. The approximation method is appropriate for the semi-Markov models of reconfigurable systems that are designed to achieve extremely high reliability. The reliability model approximation method consists of replacing a detailed description of a reconfiguration process with the probabilities of the possible outcomes of the reconfiguration process. These probabilities are included in the model as instantaneous jumps from the fault-occurrence state. Since little time is spent in the reconfiguration states, instantaneous jumps are a close approximation to the original model. This approximation procedure is shown to produce an overestimation for the probability of system failure, and an error bound is derived for this overestimation
  • Keywords
    error analysis; failure analysis; reliability; approximation method; error bound; fault-occurrence state; reconfigurable systems; reliability model; semi-Markov models; Aerospace control; Aircraft; Approximation methods; Computer architecture; Digital control; Digital systems; Life testing; NASA; Redundancy; System recovery;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1991. Proceedings., Annual
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    0-87942-661-6
  • Type

    conf

  • DOI
    10.1109/ARMS.1991.154503
  • Filename
    154503