• DocumentCode
    2368120
  • Title

    Hardware and software fault simulation

  • Author

    Stroph, R. ; Clarke, T.

  • Author_Institution
    York Univ., UK
  • fYear
    1998
  • fDate
    30 Sep-2 Oct 1998
  • Firstpage
    413
  • Lastpage
    419
  • Abstract
    This paper describes the technique of fault acceleration implementation for analysis of a fault tolerant system based on a transputer network. It is imperative that a fault tolerant system´s dependability is validated to ensure that its algorithms and mechanisms have been correctly implemented, and that it provides the required level of service. Hence, to undertake an investigation of fault tolerant approaches, it is necessary to realise a fault injection scheme which provides an acceleration of the occurrence of failures. This is a prerequisite, due to the very low natural failure rate, which makes it practically impossible to validate any fault tolerant mechanism otherwise. The fault injection mechanism was designed for a transputer-based fault tolerant application and is explained in detail. A helicopter flight control simulation is presented as a case study
  • Keywords
    virtual machines; case study; fault acceleration; fault injection scheme; fault tolerant system; hardware fault simulation; helicopter flight control simulation; software fault simulation; system dependability; transputer network;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Simulation '98. International Conference on (Conf. Publ. No. 457)
  • Conference_Location
    York
  • ISSN
    0537-9989
  • Print_ISBN
    0-85296-709-8
  • Type

    conf

  • DOI
    10.1049/cp:19980672
  • Filename
    731883