• DocumentCode
    2593290
  • Title

    Fault-tolerant parallel processors for avionics with reduced maintenance

  • Author

    Rennels, David A. ; Rohr, John A.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    1990
  • fDate
    15-18 Oct 1990
  • Firstpage
    372
  • Lastpage
    377
  • Abstract
    Architectural issues and approaches for implementing fault-tolerant parallel processors in avionics systems and other dedicated applications requiring high levels of dependability are discussed. For these systems it is desirable to provide both a high degree of fault tolerance and a system that can operate for extended periods of time without external maintenance. With current technology it is possible to operate dependably for months between maintenance events. The longer-term goal should be maintenance-free operation (a computer that outlasts its host system). It is argued that new high-density packaging techniques may make this type of long-life fault-tolerant design an attractive choice in controlling the life-cycle costs of the next generation of systems
  • Keywords
    aerospace computing; aircraft instrumentation; fault tolerant computing; maintenance engineering; packaging; parallel architectures; aircraft instrumentation; avionics; computer architecture; dedicated applications; dependability; fault-tolerant parallel processors; high-density packaging; life-cycle costs; reduced maintenance; Aerospace electronics; Circuit faults; Fault tolerance; Fault tolerant systems; Hardware; Integrated circuit packaging; Operating systems; Propulsion; Protection; Redundancy;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
  • Conference_Location
    Virginia Beach, VA
  • Type

    conf

  • DOI
    10.1109/DASC.1990.111317
  • Filename
    111317