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Dynamically Adjusting Filter Gain Method for Suppressing GNSS Observation Outliers in Integrated Navigation

Published online by Cambridge University Press:  29 June 2018

Lihui Wang*
Affiliation:
(Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China)
Kangyi Zhi
Affiliation:
(Beijing Institute of Control Engineering, Beijing 100081, China)
Bin Li
Affiliation:
(Beijing Research Center of Intelligent Equipment for Agriculture, Beijing 100097, China)
Yuexin Zhang
Affiliation:
(Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China)
*

Abstract

Global Navigation Satellite Systems (GNSSs) are easily influenced by the external environment. Signals may be lost or become abnormal thereby causing outliers. The filter gain of the standard Kalman filter of a loosely coupled GNSS/inertial navigation system cannot change with the outliers of the GNSS, causing large deviations in the filtering results. In this paper, a method based on a χ2-test and a dynamically adjusting filter gain method are proposed to detect and separately to suppress GNSS observation outliers in integrated navigation. An indicator of an innovation vector is constructed, and a χ2-test is performed for this indicator. If it fails the test, the corresponding observation value is considered as an outlier. A scale factor is constructed according to this outlier, which is then used to lower the filter gain dynamically to decrease the influence of outliers. The simulation results demonstrate that the observation outlier processing method does not affect the normal values under normal circumstances; it can also discriminate between single and continuous outliers without errors or omissions. The impact time of outliers is greatly reduced, and the system performance is improved by more than 90%. Experimental results indicate that the proposed methods are effective in suppressing GNSS observation outliers in integrated navigation.

Type
Research Article
Copyright
Copyright © The Royal Institute of Navigation 2018 

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References

REFERENCES

Angrisano, A., Petovello, M. and Pagliano, G. (2010). GNSS/INS Integration in Vehicular Urban Navigation. Proceedings of ION GNSS, Portland, 2124 Sep.Google Scholar
Chang, G. (2014). Loosely Coupled INS/GPS Integration with Constant Lever Arm using Marginal Unscented Kalman Filter. The Journal of Navigation, 67(3), 419436.Google Scholar
Godha, S. (2006). Performance Evaluation of Low Cost MEMS-Based IMU Integrated with GNSS for Land Vehicle Navigation Application. M.Sc Thesis, Department of Geomatics Engineering, University of Calgary, UCGE Report 20239.Google Scholar
Hu, G.G., Liu, Y.H., Gao, S.S. and Yang, Y. (2015). Improved strong tracking UKF and its application in INS/GPS integrated navigation. Journal of Chinese Inertial Technology, 22(05), 634639.Google Scholar
Koch, K. (2014). Robust estimations for the nonlinear Gauss Helmert model by the expectation maximization algorithm. Journal of Geodesy, 88(3), 263271.Google Scholar
Li, K., Jin, J.H. and Chang, G.B. (2015). Detection and Resistance of the Outlying Observation in GNSS /INS Integrated Navigation System. Hydrographic Surveying and Charting, 35(1), 2529.Google Scholar
Liu, S., Sun, F.P., Chen, P. et al. (2012). A Survey of Time Synchronization Solutions in GPS/INS Integrated Systems. GNSS world of China, 37(1), 5356.Google Scholar
Luo, J.J., Ma, W.H., Yuan, J.P. and Yue, X.K. (2012). Principle and Application of Integrated Navigation. Xi'an: Northwestern Polytechnic University Press.Google Scholar
Miao, Y.W., Zhou, W., Tian, L. and Cui, Z.W. (2016). Extended Robust Kalman Filter Based on Innovation Chi-Square Test Algorithm and Its Application. Geomatics and Information Science of Wuhan University, 41(2), 269–73.Google Scholar
Quan, W., Liu, B.Q., Gong, X.L. and Fang, J.C. (2011). INS/CNS/GNSS Integrated Navigation Technology. Beijing: National Defense Industry Press.Google Scholar
Simon, D. (2006). Optimal state estimation: Kalman, H∞, and nonlinear approach. New Jersey: Wiley-Interscience.Google Scholar
Woodman, O.J. (2007) An Introduction to Inertial Navigation. University of Cambridge, Computer Laboratory, Tech. Rep. UCAMCL-TR-696.Google Scholar
Yedukondalu, K., Sarma, A. D. and Ashwani, K. (2013). Spectral analysis and mitigation of GPS multipath error using digital filtering for static applications. IETE Journal of Research, 59(2), 156166.Google Scholar