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Constructing space-based continuous navigation and communication system utilizing formation flying satellites on GEO orbit in deep space exploration

  • Hui Li*
  • , Qinyu Zhang
  • , Naitong Zhang
  • *Corresponding author for this work
  • Harbin Institute of Technology Shenzhen

Research output: Contribution to journalArticlepeer-review

Abstract

Two clusters of formation flying satellites with a relative angle on geosynchronous Earth orbit were used to construct a space-based continuous navigation system for deep space exploration. Adopting technique of passive navigation by multiple base-stations, formation flying satellites obtained high precision of navigation according to time and frequency difference of arrival of downlink signal from deep space explorer. Enhancing system timing and carrier frequency, and increasing the length of baselines help to improve precision of navigation. The precision of this navigation system is close to that of NASA's VLBI system.

Original languageEnglish
Pages (from-to)1185-1189
Number of pages5
JournalActa Astronautica
Volume65
Issue number9-10
DOIs
StatePublished - Nov 2009
Externally publishedYes

Keywords

  • Continuous navigation
  • Deep space exploration
  • Formation flying satellite
  • Geostationary Earth orbit
  • Space-based

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