• DocumentCode
    536296
  • Title

    Electromagnetic satellite cluster collision prediction and avoidance

  • Author

    Su, Jianmin ; Dong, Yunfeng

  • Author_Institution
    Astronaut. Acad., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • Volume
    2
  • fYear
    2010
  • fDate
    29-31 Oct. 2010
  • Firstpage
    767
  • Lastpage
    770
  • Abstract
    A two-spacecraft cluster in deep space collision prediction and avoidance is discussed in this paper, with double-integral model as dynamics model. Collision probability calculation is based on relative motion states and covariance matrix prediction. Collision avoidance mechanism, employing electromagnetic force as control force, distance and distance rate as feedback, will start when collision probability is beyond upper limit. Control law was designed by making use of Lyapunov method, aimed to avoid collision and make distance rate approach to zero.
  • Keywords
    Lyapunov methods; artificial satellites; collision avoidance; covariance matrices; electromagnetic forces; feedback; integral equations; Lyapunov method; collision probability calculation; control force; covariance matrix prediction; double integral model; dynamics model; electromagnetic force; electromagnetic satellite cluster collision avoidance; electromagnetic satellite cluster collision prediction; feedback; two spacecraft cluster; Electromagnetics; Extraterrestrial measurements; Indium tin oxide; Position measurement; Predictive models;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Computing and Intelligent Systems (ICIS), 2010 IEEE International Conference on
  • Conference_Location
    Xiamen
  • Print_ISBN
    978-1-4244-6582-8
  • Type

    conf

  • DOI
    10.1109/ICICISYS.2010.5658625
  • Filename
    5658625