• DocumentCode
    2065020
  • Title

    An active suspension system for lunar crew mobility

  • Author

    Bluethmann, Bill ; Herrera, Ed ; Hulse, Aaron ; Figuered, Josh ; Junkin, Lucien ; Markee, Mason ; Ambrose, Robert O.

  • Author_Institution
    Software, Robot. & Simulation Div., NASA Johnson Space Center, Houston, TX, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    This paper describes the design and control of the first generation active suspension for NASA´s Chariot rover and Lunar Electric Rover (LER). Within the paper is a general overview of the needs and benefits of active suspensions for crew mobility systems on the lunar surface. In the spectrum of active suspensions, the Chariot system falls into the category of a series active or low bandwidth suspension. The passive suspension elements absorb the high frequency content of driving over rugged terrain and the active element sets the height of the suspension allowing the vehicle to conform to the terrain. This suspension system is capable of raising and lowering the vehicle, adjusting roll and pitch attitude for docking operations, leveling the chassis against gravity, and balancing the force across the six wheels during low speed operations. In addition to the existing system, initial results of an incremental design upgrade are discussed and future considerations for suspension systems for the lunar surface are described.
  • Keywords
    space vehicles; suspensions (mechanical components); vehicle dynamics; Chariot rover; active suspension system; low bandwidth suspension; lunar crew mobility system; lunar electric rover; passive suspension elements; series active suspension; Costs; Humans; Manufacturing; Moon; NASA; Space missions; Space technology; Supply chain management; Supply chains; Technological innovation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446895
  • Filename
    5446895