• DocumentCode
    1132570
  • Title

    Control of Synchronous Orbit Using Lyapunov Stability Theory

  • Author

    Ahmed, N.U. ; Sen, A.K.

  • Author_Institution
    University of Ottawa
  • Issue
    1
  • fYear
    1981
  • Firstpage
    48
  • Lastpage
    53
  • Abstract
    A state-dependent control law is proposed using the Lyapunov stability theorem and its usefulness for closed-loop control of a synchronous orbit is investigated. It is shown that a sequential scheme using a modified control law provides a more practical means of orbit control.
  • Keywords
    Acceleration; Councils; Equations; Force control; Lyapunov method; Satellites;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1981.309035
  • Filename
    4102441
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1132570