• DocumentCode
    175483
  • Title

    Momentum Management of Chinese space station based on robust H∞

  • Author

    Lin Yue ; Jia Ying-min ; Gao Ya-nan ; Fan Song-tao

  • Author_Institution
    Beijing Inst. of Control Eng., Beijing, China
  • fYear
    2014
  • fDate
    May 31 2014-June 2 2014
  • Firstpage
    418
  • Lastpage
    422
  • Abstract
    For the requirement of multi-structure architecture, a controller based on robust H_∞ is proposed for LVLH angular momentum Management control method. The method is characterized by a combination of robust control and classical pole placement, and gives the system more robustness of parameter variation. Numerical simulation based on accurate dynamic model is proposed. Simulation result shows that controller meets the requirement of different structure of Chinese space station, and do not need to change control rate of system.
  • Keywords
    H control; aerospace control; numerical analysis; pole assignment; robust control; Chinese space station; LVLH angular momentum management control method; classical pole placement; multistructure architecture; numerical simulation; parameter variation; robust H∞; robust H_∞; robust control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (2014 CCDC), The 26th Chinese
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4799-3707-3
  • Type

    conf

  • DOI
    10.1109/CCDC.2014.6852184
  • Filename
    6852184