• DocumentCode
    19089
  • Title

    X-ray pulsar/starlight Doppler integrated navigation for formation flight with ephemerides errors

  • Author

    Liu, J. ; Fang, J.C. ; Ma, X. ; Kang, Z.W. ; Wu, J.

  • Author_Institution
    Sch. of Instrum. Sci. & Opto-Electron. Eng., Beihang Univ., Wuhan, China
  • Volume
    30
  • Issue
    3
  • fYear
    2015
  • fDate
    Mar-15
  • Firstpage
    30
  • Lastpage
    39
  • Abstract
    Currently, the deep space explorer formation fight is a novel area of aerospace technique [15]. The formation fight can increase redundancy backup, decentralize the cost, and provide a multi-platform for the deep space exploration [17]. For the deep space explorer formation fight, both absolute and relative navigation accuracies are crucial, especially the relative one. Orbit determination of a spacecraft is primarily performed at a ground station [4]. Unfortunately, subject to the long distance between the explorer and the earth, traditional ground station-based navigation methods cannot provide high-accuracy and real-time navigation information. Consequently, the autonomous navigation systems [12], [13], which observe the celestial bodies to obtain the navigation information, are highly attractive.
  • Keywords
    Doppler effect; X-ray binary stars; astronomical ephemerides; satellite ground stations; satellite navigation; space communication links; X-ray pulsar; aerospace technique; autonomous navigation system; deep space explorer formation flight; ephemerides error; ground station; orbit determination; redundancy backup; spacecraft; starlight Doppler integrated navigation; Doppler radar; Orbits; Real-time systems; Satellite navigation; Space exploration; Space research; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.2014.140074
  • Filename
    7081637