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Adaptive fading Kalman filter with applications in integrated navigation system

  • Yanrui Geng*
  • , Zhongxing Cui
  • , Hongyue Zhang
  • , Jiancheng Fang
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

The reasons of the instability of Kalman filter were analyzed from the stability of Kalman filter. A group of adaptive estimation methods of Kalman filter fading factor were developed and simulated in GPS/SINS (global position system and strapdown inertial navigation system) integrated navigation system. The characteristic that the filter residuals were zero-mean Gaussian white noise vectors was used and a chi-square distribution variable was made while computing the fading factor. The fading factor was computed by testing each element of the filter residual vector. The results show that the proposed algorithms can estimate the fading factor adaptively, restrain filtering divergence and has the less computation burden than other algorithms.

Original languageEnglish
Pages (from-to)434-437
Number of pages4
JournalBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
Volume30
Issue number5
StatePublished - May 2004

Keywords

  • Adaptive filtering
  • Global position system
  • Kalman filtering
  • Strapdown inertial navigation system

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