• DocumentCode
    592779
  • Title

    Development of an eddy current brake system for detumbling malfunctioning satellites

  • Author

    Sugai, Fumihito ; Abiko, Satoko ; Tsujita, Teppei ; Xin Jiang ; Uchiyama, Masaru

  • Author_Institution
    Dept. of Mech. Syst. & Design, Tohoku Univ., Sendai, Japan
  • fYear
    2012
  • fDate
    16-18 Dec. 2012
  • Firstpage
    325
  • Lastpage
    330
  • Abstract
    This paper proposes a new method to detumble uncontrolled large space debris such as malfunctioning satellites. There are many researches about a space robot capturing and deorbiting space debris. However it is generally very difficult to capture tumbling targets such as the malfunctioning satellites because these targets are out of control in attitude and rotate with nutational motion. Hence we propose a new way to detumble them with an eddy current brake. The eddy current brake can detumble the uncontrolled targets without any contact. In this paper, we describe design and development of a linear induction motor type of eddy current brake. Experimental verification is carried out to verify the performance of the developed eddy current brake in order to fulfill the requirement for detumbling the uncontrolled satellite.
  • Keywords
    aerospace robotics; artificial satellites; attitude control; eddy current braking; linear induction motors; space debris; attitude control; deorbiting; eddy current brake system development; linear induction motor; malfunctioning satellite detumbling method; performance verification; rotation control; space robot; uncontrolled large space debris; uncontrolled satellite detumbling; Coils; Eddy currents; Force; Robots; Satellites; Space vehicles; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    System Integration (SII), 2012 IEEE/SICE International Symposium on
  • Conference_Location
    Fukuoka
  • Print_ISBN
    978-1-4673-1496-1
  • Type

    conf

  • DOI
    10.1109/SII.2012.6427330
  • Filename
    6427330