• DocumentCode
    2638021
  • Title

    Probability based collision monitoring method within formation flying

  • Author

    Wang, Ji-he ; Zhang, Jin-Xiu ; Cao, Xi-bin

  • Author_Institution
    Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin
  • fYear
    2008
  • fDate
    10-12 Dec. 2008
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    A probability density function based collision monitoring method within formation flying is developed and simulated. The approach for collision monitoring presented in this paper is to propagate the uncertainty covariance using linear relative dynamic model and integrate collision probability density function over the defined collision region (the combined shape of satellites) to calculate the collision probability between two individual satellites in formation. The calculated collision probability in this paper, considering the shape of combined satellites, and the probability is calculated at instantaneous time, so it is suitable to predict when and how fast a collision might be happened. Simulations results show that the along-track projected two-dimensional (X-Z plane) collision probability is the most reliable as the along-track uncertainty is much higher than the radial and cross-track components. In addition, results show that the collision probability is sensitive to the geometry of formation and the uncertainty covariance. Moreover, the methodology developed in this paper has been used to test the passive operational safety of different formation geometry.
  • Keywords
    artificial satellites; covariance analysis; position control; X-Z plane; along-track projected two-dimensional collision probability; along-track uncertainty; collision probability density function; formation flying; formation geometry; linear relative dynamic model; passive operational safety; probability based collision monitoring method; satellite shape; uncertainty covariance; Ellipsoids; Information geometry; Monitoring; Probability density function; Satellites; Shape; Space debris; Space technology; Space vehicles; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
  • Conference_Location
    Shenzhen
  • Print_ISBN
    978-1-4244-3908-9
  • Electronic_ISBN
    978-1-4244-2386-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2008.4776292
  • Filename
    4776292