• DocumentCode
    3046363
  • Title

    Kinematics and simulations of space manipulator in three work modes

  • Author

    Zhang, Fuhai ; Fu, Yili ; Yan, Shibo ; Wang, Shuguo

  • Author_Institution
    State Key Lab. of Robot. & Syst., Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    572
  • Lastpage
    577
  • Abstract
    In recent years, research on space robotics has attracted considerable attention. Kinematics of the free-flying or free-floating space manipulator system, including a spacecraft and a manipulator mounted on the spacecraft, is a significant problem. In free-floating work mode, the spacecraft will move freely in response to the disturbances caused by the manipulator motions. From the view of application, change of the spacecraft attitude for the space manipulator system is not desirable. Therefore, it is of significance to adopt the free-floating with zero-disturbance spacecraft attitude work mode. This paper presents an overview of the kinematics of the space manipulator system. Position and velocity kinematics solutions in three work modes are analyzed. The kinematics differences among the three work modes are formulated. The simulation results validate the effectiveness of the kinematics solutions in the three work modes.
  • Keywords
    aerospace control; manipulator kinematics; motion control; position control; space vehicles; velocity control; free floating space manipulator system; free flying space manipulator system; manipulator motions; position kinematics solutions; space manipulator; space robotics; spacecraft attitude; three work modes; velocity kinematics solutions; Aerospace electronics; Jacobian matrices; Joints; Kinematics; Manipulator dynamics; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633417
  • Filename
    5633417