• DocumentCode
    2968844
  • Title

    The research of real-time estimation method on tether parameters for tethered satellite

  • Author

    Yong, He ; Bin, Liang ; WenFu, Xu ; Cheng, Li

  • Author_Institution
    Shenzhen Grad. Sch., Harbin Inst. of Technol., Shenzhen, China
  • fYear
    2009
  • fDate
    22-24 June 2009
  • Firstpage
    148
  • Lastpage
    153
  • Abstract
    Most existing control methods of tethered satellite system were established on the knowing of tether parameters, but how to get the parameters needs to be solved. In this paper, a real-time estimator is developed to get the parameters. Firstly, we analyze the shortcomings resulting from directly solving the system equations to get tether parameters. Secondly, the equations are simplified and the corresponding problems are thoroughly investigated. And lastly, combing the measurements of a three-axis tether tensiometer with the information of attitude sensor, we use the Extended Kalman Filter to estimate the parameters in real time. The proposed estimator not only reduces the complexity of system model, but also improves the parameters´ precision. Simulation results verify the validity of this method.
  • Keywords
    Kalman filters; artificial satellites; attitude control; parameter estimation; attitude sensor; extended Kalman filter; real-time estimation method; satellite attitude control system; tether parameters; tethered satellite system; Automation; Control systems; Equations; Extraterrestrial measurements; Helium; Length measurement; Parameter estimation; Satellites; Space shuttles; Space technology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information and Automation, 2009. ICIA '09. International Conference on
  • Conference_Location
    Zhuhai, Macau
  • Print_ISBN
    978-1-4244-3607-1
  • Electronic_ISBN
    978-1-4244-3608-8
  • Type

    conf

  • DOI
    10.1109/ICINFA.2009.5204910
  • Filename
    5204910