Skip to main content
SpringerLink
Log in

Study on Pseudolite System for BeiDou Based on Dynamic and Independent Aircrafts Configuration

  • Conference paper
  • First Online:
China Satellite Navigation Conference (CSNC) 2013 Proceedings

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 244))

  • 1972 Accesses

Abstract

This paper presents a pseudolite system for BeiDou based on dynamic and independent aircrafts configuration. Firstly, high-altitude and long-endurance unmanned aerial vehicles and airships are needed to obtain the best configuration by analyzing GDOP. Then aiming at the pseudolites’ positioning, a new integrated scheme was proposed, where distance between two aircrafts is utilized to improve the positioning accuracy. Simulation results show that GDOP is less than 3.5 and position precision of the pseudolite is 1.2 m in the users’ area. The pseudolite system is able to provide moderate navigation service, when BeiDou position system is unavailable to users.

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

Access this chapter

Log in via an institution
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

Institutional subscriptions

References

  1. Li L (2009) Research of the deep integration of GPS/SINS navigation system. Shanghai Jiao Tong University, Shanghai

    Google Scholar 

  2. Malleswaran M, Angel Deborah S, Manjula S (2010) Integration of INS and GPS using radial basisfunction neural networks for vehicular navigation. In: 11th international conference control, automation, robotics and vision 010, pp 2427–2430

    Google Scholar 

  3. Liu J, Zeng Q, Zhao W (2010) Theory and application of navigation system. Northwest Industrial University Press, Xi’an

    Google Scholar 

  4. Cobb HS (1997) GPS pseudolites: theory, design, applications. USA:Standford University, California

    Google Scholar 

  5. Lee HK, Wang JL, Rizos C, et al (2002) Analysis of pseudolite augmentation for GPS airborne applications. In: IONGPS, Portland, Oregon, American

    Google Scholar 

  6. Yue Y, Lie H (2009) GAO guan-gen. Precision analysis of pseudolite positioning system. Chin J Sens Actuators 22(10):1432–1436

    Google Scholar 

  7. Meng J (2007) Study on pseudolite position technology and configuration. Zhengzhou:Information Engineering University

    Google Scholar 

  8. Yarlagadda R, Ali L, Al-Dhahir N, Hershey J (2000) GPS GDOP metric. IEE Proc Radar Sonar Navig 147(5):259–264

    Google Scholar 

  9. Zhnag N (2006) Altitude long-endurance UAV integrated navigation system. Northwestern Polytechnical University, Xi’an

    Google Scholar 

  10. Yuan G, Yuan K, Zhang H (2011) A variable proportion adaptive federal kalman filter for INS/ESGM/GPS/DVL integrated navigation system. In: 4th international joint conference on computational sciences and optimization 2011, pp 976–981

    Google Scholar 

  11. Yuan J, Fan S, Liu J (2011) Research on navigation performance of GPS/INS tightly integrated system. Aerosp Electron Warfare 27(2):17–21

    Google Scholar 

  12. Zhou J, Yuan J, Luo J (2009) Fully intergrated SINS/GPS navigation system based on federated filters. J Syst Simul 21(6):1562–1569

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Academy of Frontier Science, NanJing University of Aeronautics and Astronautics, NanJing, China

    Guohua Kang, Bing Hua & Fengying Zheng

  2. College of Automation Engineering, NanJing University of Aeronautics and Astronautics, NanJing, China

    Longyu Tan

Authors
  1. Guohua Kang
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Longyu Tan
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Bing Hua
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Fengying Zheng
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Guohua Kang .

Editor information

Editors and Affiliations

  1. , China Aerospace Sci. & Technology Corp., Chinese Academy of Sciences, Beijing, China, People's Republic

    Jiadong Sun

  2. China Satellite Navigation Office, Beijing, China, People's Republic

    Wenhai Jiao

  3. Chinese Academy of Sciences, Navigation Headquarters, Dengzhuang South Road, Beijing, 100094, China, People's Republic

    Haitao Wu

  4. Wuhan University, Wuhan, China, People's Republic

    Chuang Shi

Rights and permissions

Reprints and permissions

Copyright information

© 2013 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Kang, G., Tan, L., Hua, B., Zheng, F. (2013). Study on Pseudolite System for BeiDou Based on Dynamic and Independent Aircrafts Configuration. In: Sun, J., Jiao, W., Wu, H., Shi, C. (eds) China Satellite Navigation Conference (CSNC) 2013 Proceedings. Lecture Notes in Electrical Engineering, vol 244. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-37404-3_15

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-37404-3_15

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-37403-6

  • Online ISBN: 978-3-642-37404-3

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics

Search

Navigation