• DocumentCode
    2969151
  • Title

    A scalable platform for run-time reconfigurable satellite payload processing

  • Author

    Hagemeyer, Jens ; Hilgenstein, A. ; Jungewelter, D. ; Cozzi, Dario ; Felicetti, C. ; Rueckert, U. ; Korf, Sebastian ; Koester, M. ; Margaglia, F. ; Porrmann, Mario ; Dittmann, F. ; Ditze, Michael ; Harris, J. ; Sterpone, L. ; Ilstad, Jorgen

  • Author_Institution
    Center of Excellence Cognitive Interaction Technol., Bielefeld Univ., Bielefeld, Germany
  • fYear
    2012
  • fDate
    25-28 June 2012
  • Firstpage
    9
  • Lastpage
    16
  • Abstract
    Reconfigurable hardware is gaining a steadily growing interest in the domain of space applications. The ability to reconfigure the information processing infrastructure at runtime together with the high computational power of today´s FPGA architectures at relatively low power makes these devices interesting candidates for data processing in space applications. Partial dynamic reconfiguration of FPGAs enables maximum flexibility and can be utilized for performance increase, for improving energy efficiency, and for enhanced fault tolerance. To be able to prove the effectiveness of these novel approaches for satellite payload processing, a highly scalable prototyping environment has been developed, combining dynamically reconfigurable FPGAs with the required interfaces such as SpaceWire, MIL-STD-1553B, and SpaceFibre. Up to 30 SpaceWire interfaces, 5 copper-based SpaceFibre interfaces, and 270 GPIOs can be realized and combined with one to five dynamically reconfigurable Xilinx FPGAs and up to 20 GByte of working memory. The implemented approach for dynamic reconfiguration enables partial reconfiguration at 400 MByte/s. Blind and readback scrubbing is supported and the scrub rate can be adapted individually for different parts of the design.
  • Keywords
    aerospace computing; artificial satellites; fault tolerance; field programmable gate arrays; user interfaces; GPIO; MIL-STD-1553B interface; SpaceWire interface; blind scrubbing; byte rate 400 MByte/s; copper-based SpaceFibre interface; data processing; energy efficiency; fault tolerance; high computational power; information processing infrastructure; partial dynamic reconfiguration; readback scrubbing; reconfigurable Xilinx FPGA architecture; reconfigurable hardware; run-time reconfigurable satellite payload processing; scalable prototyping environment; space application; working memory; Bridges; Computer architecture; Field programmable gate arrays; Hardware; Process control; Prototypes; Tiles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Adaptive Hardware and Systems (AHS), 2012 NASA/ESA Conference on
  • Conference_Location
    Erlangen
  • Print_ISBN
    978-1-4673-1915-7
  • Electronic_ISBN
    978-1-4673-1914-0
  • Type

    conf

  • DOI
    10.1109/AHS.2012.6268642
  • Filename
    6268642