Real-time fault detection method based on belief rule base for aircraft navigation system-Reference-Cited by-同舟云学术

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Real-time fault detection method based on belief rule base for aircraft navigation system

Published:2013-06 Issue:3 Volume:26 Page:717-729
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Zhao Xin,Wang Shicheng,Zhang Jinsheng,Fan Zhiliang,Min Haibo

Funder

the National High-tech Research and Development Program of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Lughofer ED, Klement EP, Lujan JM, Guardiola C. Model-based fault detection in multi-sensor measurement systems. In: Proceedings of 2004 2nd International IEEE Conference on Intelligent Systems. 2004. p. 184–9.

2. Fault prediction model based on evidential reasoning approach;Si;Sci China Ser F-Inf Sci,2010

3. Fault detection, identification and reconstruction for gyroscope in satellite based on independent component analysis;Li;Acta Astronaut,2011

4. Effective fault diagnosis based on strong tracking UKF;Han;Aircraft Eng Aerosp Technol,2011

5. A Cramer-Rao-type estimation lower bound for system with measurement fault;Rapoport;IEEE Trans Automatic Control,2005

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