• DocumentCode
    2637094
  • Title

    Problems of Micro-satellite OBC and solving method based on reconfiguration technique

  • Author

    Dan, Zhao ; Guodong, Xu ; Yunhai, Geng

  • Author_Institution
    Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin
  • fYear
    2008
  • fDate
    10-12 Dec. 2008
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    The objective of this work is to solve the problems of On-board Computer (OBC) in Micro-satellite. With the limit of size and weight, and the requirement of multifunction and high-performance, itpsilas almost impossible to design an eligible Micro-satellite OBC by regular methods. To address this issue, this paper researches reconfiguration technique, and proposes one OBC design based on it. The reconfigurable OBC can achieve the multifunction and high processing ability, and there are several measures to ensure the reliability.
  • Keywords
    artificial satellites; field programmable gate arrays; reconfigurable architectures; spacecraft computers; micro-satellite on-board computer; reconfiguration technique; Attitude control; Costs; Data processing; Design methodology; Extraterrestrial measurements; Field programmable gate arrays; Hardware; Microprocessors; Military computing; Military satellites;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
  • Conference_Location
    Shenzhen
  • Print_ISBN
    978-1-4244-3908-9
  • Electronic_ISBN
    978-1-4244-2386-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2008.4776233
  • Filename
    4776233