• DocumentCode
    1733195
  • Title

    Plug-and-play fast-assembling satellite control system

  • Author

    Yuan Dehu ; He Liang ; Lu Shan ; Han Fei ; Chen Shaohua ; Zhan Pengyu ; Sun Lujun ; Hu Kun ; Li Baohua

  • Author_Institution
    Shanghai Inst. of Spaceflight Control Technol., Shanghai, China
  • fYear
    2013
  • Firstpage
    7326
  • Lastpage
    7329
  • Abstract
    The design scheme of a kind of plug-and-play fast-assembling satellite control system was proposed in this paper. The overall architecture of the system was introduced. The on-board computer simulator, the plug-and-play modular and the host computer software were designed respectively. And the plug-and-play time series of satellite control system devices was also described. The proposed plug-and-play satellite scheme can extremely reduce the time of coordination, development and integrated test, cut down the cost of satellite development, and enhance the reliability of spacecraft, so as to lay a good technology foundation for the development of micro-nano spacecraft and operationally responsive spacecraft.
  • Keywords
    aerospace control; artificial satellites; control system CAD; time series; design scheme; host computer software design; micro-nano spacecraft development; onboard computer simulator; plug-and-play fast-assembling satellite control system; plug-and-play satellite scheme; plug-and-play time series; spacecraft reliability; system architecture; Control systems; Electronic mail; Intelligent control; Laboratories; Satellites; Space vehicles; Sun; Fast Assembling; Plug and Play; Satellite Control System;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6640726