• DocumentCode
    3028288
  • Title

    A selecting method in collision risk assessment

  • Author

    Zhang, Rongzhi ; Zhou, Fengqi ; Wang, Xiuhong ; Wang, Xinfeng

  • Author_Institution
    Northwestern Polytech. Univ., Xi´´an, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    841
  • Lastpage
    844
  • Abstract
    With the increase of space debris, the technology of spacecraft collision avoidance has become more and more important. In this paper, an analytical method of selecting objects is investigated based on mean elements, which is free from the restriction of the spacecraft launch time and the instantaneous position. If only the launch orbit of a spacecraft is known, this method can be used to select potential dangerous objects from thousands of space objects for several days before the launch window of the mission.
  • Keywords
    collision avoidance; position control; risk management; space vehicles; collision risk assessment; instantaneous position; launch window; selecting method; space debris; space objects; spacecraft collision avoidance; spacecraft launch time; Collision avoidance; Filtering; Optimization; Orbits; Satellites; Space debris; 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.2010.5632329
  • Filename
    5632329