• DocumentCode
    490552
  • Title

    Arrow Mode Reboost Analysis for Space Station Freedom

  • Author

    Graham, Ronald E. ; DuFore, Valerie J.

  • Author_Institution
    Control Systems Branch, NASA Lewis Research Center, 21000 Brookpark Road, Cleveland OH 44135. ecaxron@ariel.lerc.nasa.gov
  • fYear
    1993
  • fDate
    2-4 June 1993
  • Firstpage
    2485
  • Lastpage
    2489
  • Abstract
    Early flights of Space Station Freedom are gravity-gradient stabilized, but reboost to higher altitude while in Arrow Mode, where its truss is aligned with the direction of flight. Power concerns led to a proposal to activate Freedom´s solar array beta gimbals for partial sun tracking during reboost. Further plume impingement concerns led to a baseline orientation of flight with the arrays leading. A baseline dynamic simulation for this maneuver is presented here. Several observations are made, particularly about large motions of the beta gimbals during the maneuver, and about simplified structural dynamic response of the arrays to the reboost and large slew environment. The results presented here may be used as a starting point for reboost analyses on other flight configurations, or in other orientations, or with higher-fidelity structural information.
  • Keywords
    Aerospace engineering; Control systems; Equations; Information analysis; Motion control; NASA; Proposals; Space stations; Sun; Torque;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1993
  • Conference_Location
    San Francisco, CA, USA
  • Print_ISBN
    0-7803-0860-3
  • Type

    conf

  • Filename
    4793337