• DocumentCode
    1680152
  • Title

    Kolmogorov-Arnold-Moser torus orbit prediction from two-line element sets

  • Author

    Abay, Rasit ; Wiesel, William E.

  • Author_Institution
    Turkish Air Force, Konya, Turkey
  • fYear
    2015
  • Firstpage
    137
  • Lastpage
    142
  • Abstract
    A new method for orbit prediction, which is as accurate as numerical methods and as fast as analytical methods, in terms of computational time, is needed. Kolmogorov-Arnold-Moser (KAM) torus orbit prediction method is a modern orbit determination that can meet the aforementioned needs. This paper presents a differential correction technique to create parameters needed by the new theory and an approximate accuracy analysis of the new orbit determination method by using Simplified General Perturbations 4 (SGP4) and Two-Line Element Set (TLE) as observational data.
  • Keywords
    Earth orbit; satellite communication; Kolmogorov-Arnold-Moser torus orbit prediction method; SGP4; TLE; approximate accuracy analysis; differential correction technique; modern orbit determination; simplified general perturbations 4; two-line element sets; Accuracy; Convergence; Covariance matrices; Fitting; Low earth orbit satellites; Orbits; Space vehicles; KAM torus; SGP4; TLE; differential correction; low eccentricity; orbit determination;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Recent Advances in Space Technologies (RAST), 2015 7th International Conference on
  • Conference_Location
    Istanbul
  • Print_ISBN
    978-1-4673-7760-7
  • Type

    conf

  • DOI
    10.1109/RAST.2015.7208329
  • Filename
    7208329