• DocumentCode
    2650479
  • Title

    Design and Development of a 5-DOF Air-Bearing Spacecraft Simulator

  • Author

    Jian, Xu ; Gang, Bao ; QinJun, Yang ; Jun, Li

  • Author_Institution
    Res. Center of Pneumatics, Harbin Inst. of Technol., Harbin
  • fYear
    2009
  • fDate
    1-2 Feb. 2009
  • Firstpage
    126
  • Lastpage
    130
  • Abstract
    The Five Degrees of Freedom Air-bearing Spacecraft Simulator (5DOFASS) is designed at Harbin Institute of Technology for the purpose of simulating spacecraft autonomous formation flying and orbital maneuver. The 5DOFASS contains an attitude platform supported on a hemispherical air-bearing and a translation platform floated on three linear air-bearing feet, which provides a very low friction and 0-g environment in an Earth-bound laboratory. In this paper, the design and development of the 5DOFASS is described in detail, including working principle, structure, and control system. Some ongoing research problems and future plans are reported at the end of the article.
  • Keywords
    aerospace control; aerospace simulation; product design; zero gravity experiments; 0-g environment; 5-DOF air-bearing spacecraft simulator; 5DOFASS; Earth-bound laboratory; attitude platform; five degrees of freedom; hemispherical air-bearing; linear air-bearing feet; orbital maneuver; spacecraft autonomous formation flying; very low friction; Aerospace electronics; Computational modeling; Control systems; Foot; Friction; Propulsion; Robotics and automation; Space technology; Space vehicles; Testing; air-bearing; cold gas propulsion system; image process; spacecraft simulator;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Informatics in Control, Automation and Robotics, 2009. CAR '09. International Asia Conference on
  • Conference_Location
    Bangkok
  • Print_ISBN
    978-1-4244-3331-5
  • Type

    conf

  • DOI
    10.1109/CAR.2009.7
  • Filename
    4777209