Skip to main content

The Application of the GNSS Receiver in the Third Stage of China Lunar Exploration Program

  • Conference paper
  • First Online:

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 323))

Abstract

Lunar exploration puts forward higher requirements in terms of performances for the subsystems. As for the navigation system, the GPS receiver provides autonomous navigation service on board in Low Earth Orbit environment, so it calls for a possible extension to Earth-to-Moon missions. This paper, referring to the Third Stage of China Lunar Exploration Program mission which is “returning” in the three stages “circling landing and returning”, investigates such a possibility, considering present and foreseen available GNSS signals. Carrier-to-noise levels achievable during the mission are evaluated. Moreover, the high-sensitivity GNSS receiver system design is discussed.

This is a preview of subscription content, log in via an institution.

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   169.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD   219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Learn about institutional subscriptions

References

  1. Winternitz LMB, Bamford WA, Heckler GW (2009) A gps receiver for high-altitude satellite navigation. IEEE J Sel Top Sig Process 3(4):541–556

    Google Scholar 

  2. Palmerini GB, Sabatini M, Perrottac G (2009) En route to the moon using GNSS signals. Acta Astronaut 64:467–483

    Article  Google Scholar 

  3. Yang WL (2010) Phasing orbit design for Chinese lunar satellite CE-1. Chin Space Sci Technol 1:18–24

    Google Scholar 

  4. Beidou satellite navigation system—document of interface control for space signal (public service signal B1I 1.0 version.) http://www.beidou.gov.cn//2012/12/27. Cited 27 Dec 2012

  5. Xu DY, Kou YH (2011) The dual component combined tracking of GPS L5 signal. In: Special journal for the second China satellite navigation conference. pp 182–190

    Google Scholar 

  6. Psiaki ML (2001) Block acquisition of weak GPS signals in a software receiver. In: Proceedings of Institute of Navigation GPS. pp 2838–2850

    Google Scholar 

  7. Wen CY, Fu ZY, Qiu YH et al (2013) High orbit environment BDS weak signal tracking technology research. J Spacecraft TT&C Technol 32(6):43–51

    Google Scholar 

  8. Li XS, Guo W, Xie XB (2011) A high dynamic, weak signal in GPS bit synchronization method. J Electron Inf Technol 33(10):87–95

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Changyuan Wen .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2015 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Wen, C., Wang, M., Qi, L., Li, D., Qiu, Y. (2015). The Application of the GNSS Receiver in the Third Stage of China Lunar Exploration Program. In: Shen, R., Qian, W. (eds) Proceedings of the 27th Conference of Spacecraft TT&C Technology in China. Lecture Notes in Electrical Engineering, vol 323. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-44687-4_1

Download citation

  • DOI: https://doi.org/10.1007/978-3-662-44687-4_1

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-662-44686-7

  • Online ISBN: 978-3-662-44687-4

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics