Skip to main content

A Modified IAE Algorithm for GNSS and IMU Integration

  • Conference paper
  • First Online:
Proceedings of the 26th Conference of Spacecraft TT&C Technology in China

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 187))

Abstract

Innovation-based adaptive estimation (IAE), which is one of the proved Adaptive Kalman Filter (AKF) algorithms, can improve the accuracy of GNSS/IMU combined navigation system based on the condition that the received GNSS measurements are independently accurate enough. However, IAE is more likely to be subjected to bias and non-convergence with degraded measurements accuracy due to GNSS signal outage or low-cost receiver. In order to maintain the performance of integrated GNSS/IMU system with the coexistence of less accurate measurements, a modified IAE algorithm is proposed in this paper. The algorithm, named “IAE with measurements discarding strategy” (IAE-D), monitors the quality of the estimations and measurements in real-time, and discards the measurements when the estimations are accurate enough or the measurements are less qualified. Field test was carried out. Noise was imported to simulate different levels of measurements deterioration. Performance comparison between Extended Kalman Filter (EKF), IAE and IAE-D has been executed with real data. The results demonstrate that IAE-D has magnificent advantage over EKF and IAE in regard to stability and accuracy when the power level of measurements interference is relatively high.

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

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 169.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 169.99
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. Grewal MS, Weill LR, Andrews AP (2007) Global positioning systems inertial navigation and integration. Wiley, New Jersey

    Google Scholar 

  2. Groves PD (2008) Principles of GNSS, inertial, and multisensor integrated navigation systems. Artech House Press, Boston

    Google Scholar 

  3. Cox DB (1980) Integration of GPS with inertial navigation systems. The ION “Redbooks” 1:144–153

    Google Scholar 

  4. Greenspan RL (1996) GPS and inertial integration. Global Position Syst Theory Appl 1:87–220

    Google Scholar 

  5. Li P, Wang J, Feng Z (2008) GNSS/pseudolite signal re-acquisition with the aid of INS in short signal blockage scenarios. In: Proceedings of the international symposium on GPS/GNSS 2008

    Google Scholar 

  6. Grewal MS, Andrews AP (2008) Kalman filtering: theory and practice using MATLAB, 2nd edn. Wiley, New York

    Google Scholar 

  7. Toda NF, Schlee FH, Obsharsky P (1969) Region of Kalman filter convergence for several autonomous navigation modes. AIAA J 7:622–627

    Article  Google Scholar 

  8. White NA, Maybeck PS, Devilbiss SL (1996) MMAE detection of interference/jamming and spoofing in a DGPS-aided inertial system. Master thesis of Ohio University, Ohio

    Google Scholar 

  9. Hu C, Chen Y, Chen W (2001) Adaptive Kalman filtering for DGPS positioning. In: Proceedings of the international symposium on Kinematic systems in geodesy, geomatics and navigation (KIS)

    Google Scholar 

  10. Ding WD, Wang J, Chris R et al (2007) Improving adaptive Kalman estimation in GPS/INS integration. J Navig 60:517–529

    Article  Google Scholar 

  11. Mohamed AH, Schwarz KP (2003) Adaptive Kalman filtering for INS/GPS. J Geodesy 73:193–203

    Article  Google Scholar 

  12. Hide C, Moore T, Smith M (2003) Adaptive Kalman filtering for low cost GPS/INS. J Navig 56:143–152

    Article  Google Scholar 

  13. Li P, Lu M, Feng Z (2010) Positioning accuracy analysis for adaptive Kalman filtering in measurements degradation. Syst Eng Electron 32(7):1489–1492

    Google Scholar 

  14. Lu M, Li P, Feng Z (2009) Adaptive updating strategy for GNSS/IMU integration. In: Proceedings of the 22nd international technical meeting of the satellite division of the institute of navigation, Savannah, Georgia, pp 750–758

    Google Scholar 

  15. Boeing North American Inc (1997) C-MIGITS II user’s guide. Boeing defense & space group

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Peng Li .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2013 Tsinghua University Press, Beijing and Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Li, P., Li, C., Wu, X., Chen, Z. (2013). A Modified IAE Algorithm for GNSS and IMU Integration. In: Shen, R., Qian, W. (eds) Proceedings of the 26th Conference of Spacecraft TT&C Technology in China. Lecture Notes in Electrical Engineering, vol 187. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-33663-8_42

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-33663-8_42

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-33662-1

  • Online ISBN: 978-3-642-33663-8

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics