• DocumentCode
    3572775
  • Title

    Station-keeping control method for GEO satellite based on relative orbit dynamics

  • Author

    Yang Wenbo ; Li Shaoyuan ; Li Ning

  • Author_Institution
    Dept. of Autom., Shanghai Jiao Tong Univ., Shanghai, China
  • fYear
    2014
  • Firstpage
    1682
  • Lastpage
    1687
  • Abstract
    Based on the analysis of relative orbit dynamics for GEO (geostationary orbit, GEO) satellite and LQG (Linear Quadratic Gaussian, LQG) algorithm, this paper proposed a station-keeping control method for GEO satellite, which realized north-south station-keeping and west-east station-keeping simultaneously. To further verify the effectiveness of the proposed method, corresponding mathematical simulation is carried out. Simulation results show that the proposed method can obtain good control precision compared with conventional station-keeping control method of GEO satellite. Thus, the proposed method is suitable for station-keeping control of GEO satellite.
  • Keywords
    artificial satellites; linear quadratic control; GEO satellite; LQG algorithm; control precision; geostationary orbit satellite; linear quadratic Gaussian algorithm; mathematical simulation; north-south station-keeping; relative orbit dynamics; station-keeping control method; west-east station-keeping; Acceleration; Control systems; Equations; Mathematical model; Orbits; Satellites; Vectors; GEO satellite; Linear Quadratic Gaussian; relative orbit dynamic; station-keeping;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation (WCICA), 2014 11th World Congress on
  • Type

    conf

  • DOI
    10.1109/WCICA.2014.7052973
  • Filename
    7052973