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Author:

Zhu, Jiangmiao (Zhu, Jiangmiao.) | Dong, Xiaofei (Dong, Xiaofei.) | Huang, Yan (Huang, Yan.) | Sha, Yanru (Sha, Yanru.)

Indexed by:

EI

Abstract:

The integrated navigation system that combines the global positioning system (GPS) and the inertial navigation system (INS) has attracted widespread attention. In order to improve its positioning and navigation accuracy, Kalman filtering algorithms are usually used to process navigation data. This paper combines fuzzy control theory with Kalman filter, and proposes an integrated navigation algorithm based on fuzzy control theory, specifically observing each component of the residual error, using multiple fuzzy inference systems to modify the measurement noise variance matrix to approximate the real noise characteristic. Through multiple simulation experiments, the results show that the algorithm can effectively suppress the filtering divergence. © 2020 The Institution of Engineering and Technology.

Keyword:

Air navigation Global positioning system Kalman filters Inertial navigation systems Fuzzy inference Fuzzy control

Author Community:

  • [ 1 ] [Zhu, Jiangmiao]Beijing University of Technology, Beijing, China
  • [ 2 ] [Dong, Xiaofei]Beijing University of Technology, Beijing, China
  • [ 3 ] [Huang, Yan]Beijing Institute of Metrology, Beijing, China
  • [ 4 ] [Sha, Yanru]Beijing University of Technology, Beijing, China

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Source :

Year: 2020

Issue: 2

Volume: 2020

Page: 101-105

Language: English

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 9

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