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

  • J. Liu*
  • , J. C. Fang
  • , X. Ma
  • , Z. W. Kang
  • , J. Wu
  • *Corresponding author for this work
  • Beihang University
  • Wuhan University of Science and Technology
  • Hunan University

Research output: Contribution to journalArticlepeer-review

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.

Original languageEnglish
Article number7081637
Pages (from-to)30-39
Number of pages10
JournalIEEE Aerospace and Electronic Systems Magazine
Volume30
Issue number3
DOIs
StatePublished - 1 Mar 2015

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