• DocumentCode
    1880778
  • Title

    SpaceWire standard and improved wormhole router design

  • Author

    Yi, Dalu ; Yu, Lixin ; Fei, Haidong ; Wang, Xingyou

  • Author_Institution
    Beijing Microelectron. Technol. Inst., Beijing, China
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    Fast growth in information technology extends the means of data transfer. Especially in recent years, many more measures have been proposed in order to raise the data rate. SpaceWire is a serial, high-speed, bi-directional, full duplex, point-to-point data transfer protocol, which is defined by ESA (European Space Agency) in 2003. Wormhole routing adopted by SpaceWire reduces router buffer and makes SpaceWire routers suited to be designed as AISCs. However, blocking problem adhered to wormhole routing limits the network throughput seriously. This paper starts with an introduction to the SpaceWire standard. From the angle of ASIC design, the author deeply analyzes what SpaceWire does to improve router´s performance in three aspects. After that, a VLSI design of Spacewire router compliant with the Spacewire standard is presented, and simulation result of this router is provided.
  • Keywords
    VLSI; aerospace computing; aerospace instrumentation; application specific integrated circuits; integrated circuit design; multiprocessor interconnection networks; network routing; protocols; AD 2003; ASIC design; European Space Agency; SpaceWire routers; SpaceWire standard; VLSI design; blocking problem; data rate; improved wormhole router design; information technology; network throughput; point-to-point data transfer protocol; router buffer; router performance; wormhole routing; Clocks; Radiation detectors; Routing; Routing protocols; Switches; Transmitters;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187103
  • Filename
    6187103