• DocumentCode
    1709567
  • Title

    Spacecraft guidance and robust attitude control with precise pointing the flexible antennas

  • Author

    Somov, Ye.I. ; Butyrin, S.A. ; Somov, S.Ye.

  • Author_Institution
    Samara Sci. Center, Russian Acad. of Sci. (RAS), Samara, Russia
  • fYear
    2009
  • Firstpage
    1057
  • Lastpage
    1062
  • Abstract
    New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on spacecraft attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
  • Keywords
    antennas; attitude control; robust control; space vehicles; digital robust control; flexible antennas; physical hysteresis damping; robust attitude control; spacecraft guidance; spacecraft structure oscillations; Attitude control; Control systems; Damping; Differential equations; Friction; Hysteresis; Large-scale systems; Mathematical model; Robust control; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, (CCA) & Intelligent Control, (ISIC), 2009 IEEE
  • Conference_Location
    St. Petersburg
  • Print_ISBN
    978-1-4244-4601-8
  • Electronic_ISBN
    978-1-4244-4602-5
  • Type

    conf

  • DOI
    10.1109/CCA.2009.5281102
  • Filename
    5281102
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1709567