• DocumentCode
    613682
  • Title

    A new efficient algorithm for tracking LEO satellites

  • Author

    Khanlari, A. ; Mansourkiaie, Fatemeh

  • Author_Institution
    Memorial Univ. of Newfoundland, St. John´s, NL, Canada
  • fYear
    2013
  • fDate
    15-18 April 2013
  • Firstpage
    587
  • Lastpage
    590
  • Abstract
    The methods of tracking Low Earth Orbit (LEO) satellites can be grouped into two different categories: “signal-based” and “program-based” methods. In this paper, we employ a new program-based tracking method to trace satellites, using Two Line orbital Elements (TLE). Using TLE is a simple and well-known method for tracking satellites; however, this paper presents a new algorithm for tracking satellites, based on TLE files. This algorithm, uses an available TLE file to estimate the satellite´s position and to update the orbital elements, for any desired time that we are interested in tracing the satellite. The results show that the algorithm is accurate and reliable.
  • Keywords
    artificial satellites; satellite navigation; LEO satellites tracking; TLE; low Earth orbit satellites; program-based tracking method; satellite position; signal-based method; two line orbital element; Equations; Low earth orbit satellites; Mathematical model; Orbits; Reliability; Vectors; LEO satellites; Orbital elements; Program-based tracking; TLE component;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems Conference (SysCon), 2013 IEEE International
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    978-1-4673-3107-4
  • Type

    conf

  • DOI
    10.1109/SysCon.2013.6549941
  • Filename
    6549941