• DocumentCode
    2592560
  • Title

    A flexible fault tolerant processor for launch vehicle avionics systems

  • Author

    Taylor, R.C. ; Van Hoff, P. ; Walter, C.

  • Author_Institution
    Allied-Signal Aerosp. Co., Teterboro, NJ, USA
  • fYear
    1990
  • fDate
    15-18 Oct 1990
  • Firstpage
    147
  • Lastpage
    152
  • Abstract
    The multicomputer architecture for fault tolerance (MAFT), a highly flexible approach to achieving fault-tolerant data processing in launch vehicle avionics systems, is described. It offers a multi-lane building block method for designing real-time control systems which are capable of extremely reliable computations and which provide tolerance to a broad class of faults. MAFT is readily adaptable to computer processing applications in both expendable and reusable launch vehicles which carry critical or extremely high-cost payloads. MAFT is well suited for mission-critical processing functions, and can be implemented in a variety of data management system architectures, such as centralized, federated, or distributed configurations. MAFT provides a flexible, highly modular, easily maintained system, having low program life cycle costs
  • Keywords
    aerospace computer control; aerospace instrumentation; computer architecture; fault tolerant computing; multiprocessing systems; redundancy; distributed configuration; fault-tolerant data processing; federated configuration; flexible fault tolerant processor; launch vehicle avionics; life cycle costs; mission-critical processing functions; multi-lane building block; multicomputer architecture; real-time control systems; Aerospace electronics; Computer applications; Computer architecture; Control systems; Data processing; Design methodology; Fault tolerance; Fault tolerant systems; Real time systems; Vehicles;
  • 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.1990.111277
  • Filename
    111277