• DocumentCode
    3116147
  • Title

    Study on the landing mechanism employed in asteroid exploration

  • Author

    Zhao, Zhijun ; Zhao, Jingdong ; Liu, Hong

  • Author_Institution
    State Key Lab. of Robot. & Syst., Harbin Inst. of Technol., Harbin, China
  • fYear
    2012
  • fDate
    5-8 Aug. 2012
  • Firstpage
    1032
  • Lastpage
    1037
  • Abstract
    Different landing exploration modes of small bodies are discussed. A landing mechanism employed in the asteroid landing exploration is designed. It contains landing foot, landing gear, cardan, buffer mechanism, equipment base, anchor system, and so on. The landing mechanism could fold up to reduce space occupation in the spacecraft. It could fix itself on the landing slope under microgravity via the anchor system. The anchor system´s penetrating and anchoring capability is examined in the frozen earth. The landing performance under microgravity is tested on the air-floating platform. Experiments show that the landing mechanism could perform landing under microgravity and anchoring itself firmly on the landing slope.
  • Keywords
    aerospace components; anchors; asteroids; gears; space vehicles; air floating platform; anchor system; asteroid landing exploration; buffer mechanism; cardan; frozen earth; landing foot; landing gear; landing mechanism; microgravity landing performance; Acceleration; Damping; Earth; Foot; Force; Gears; Space vehicles; Anchoring. Microgravity; Asteroid exploration; Landing mechanism;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation (ICMA), 2012 International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4673-1275-2
  • Type

    conf

  • DOI
    10.1109/ICMA.2012.6283392
  • Filename
    6283392