• DocumentCode
    3032077
  • Title

    The research of bi-elliptic flyaround maneuver

  • Author

    Hui, Zhao ; Xinglong, Li ; Baoqing, Yang

  • Author_Institution
    Control & Simulation Center, Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    267
  • Lastpage
    271
  • Abstract
    The flyaround maneuvers have a broad application prospects in the future space activities. In this paper, a coplanar bi-elliptic flyaround maneuver by impulsive thrust control is discussed; the necessary conditions of the bi-elliptic flyaround formation are deduced based on the Hill´s equation. Simulation results verify the superiority of the bi-elliptic flyaround maneuver compared with the natural flyaround maneuver.
  • Keywords
    aerospace control; force control; Hill´s equation; bielliptic flyaround formation; coplanar bielliptic flyaround maneuver; future space activities; impulsive thrust control; Aerospace electronics; Equations; Mathematical model; Orbits; Satellites; Simulation; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5632537
  • Filename
    5632537
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3032077