• DocumentCode
    2469680
  • Title

    Low-cost active anti-gravity suspension system

  • Author

    Jagannathan, Shankar ; Fenn, Ralph C. ; Johnson, Bruce G.

  • Author_Institution
    SatCon Technol. Corp., Cambridge, MA, USA
  • Volume
    5
  • fYear
    1995
  • fDate
    21-23 Jun 1995
  • Firstpage
    3606
  • Abstract
    Recently, SatCon Technology Corporation has successfully demonstrated a novel anti-gravity suspension for NASA Langley. This approach consists of a passive gravity-unload mechanism enhanced with an active inertia-controller. The passive gravity-unload is achieved by supporting the suspended body with a counterbalanced cable system. The suspension is unique because it has essentially zero stiffness and zero damping relative to conventional approaches. The effect of suspension stiffness on the dynamics of the suspended article is essentially eliminated. During this phase, a hardware demonstration of this concept providing a vertical anti-gravity suspension using low-cost, off-the-shelf components was developed. The results achieved are compared with the capabilities of available mechanical suspensions systems to attain zero-gravity environments. Finally, a discussion is provided on extending this concept to three dimensions using an actively-controlled translational table
  • Keywords
    aerospace biophysics; aerospace simulation; dynamics; space research; zero gravity experiments; SatCon Technology Corporation; active anti-gravity suspension system; active inertia-controller; actively-controlled translational table; counterbalanced cable system; dynamics; passive gravity-unload mechanism; zero-gravity environments; Acceleration; Biological system modeling; Drag; Gravity; Humans; Laboratories; NASA; Space technology; Springs; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, Proceedings of the 1995
  • Conference_Location
    Seattle, WA
  • Print_ISBN
    0-7803-2445-5
  • Type

    conf

  • DOI
    10.1109/ACC.1995.533809
  • Filename
    533809