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Multi-sensor Fault Diagnosis of Aircraft Engine Based on Kalman Filter Group

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Proceedings of 2016 Chinese Intelligent Systems Conference (CISC 2016)

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 404))

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Abstract

For the problem of Multi-sensor Fault Diagnosis in aircraft engine, according to the theory of Kalman filter, this paper proposed a novel fault diagnosis method based on Kalman filter group. Author used the engine model nonlinear system based on the least square fitting method, and the linear discrete system model of engine was obtained by discrete treatment. On this basis, further considering the effect of engine sensor fault and interferences, successively for single sensor and multi-sensor faults condition, we put forward the aircraft engine sensor fault diagnosis method based on Kalman filter group. The simulation results show that this method can quickly diagnose and have a good diagnostic accuracy for multiple sensor faults and gradual failure of the engine.

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References

  1. Xiang X (2004) Turbofan engine sensor fault diagnosis and fault tolerant control research [D]. Northwestern Polytechnical University, Xi’an

    Google Scholar 

  2. Gaoqian Z (2014) Fault diagnosis and fault tolerant control of aircraft engine sensor [D]. Nanjing University of Aeronautics and Astronautics, Nanjing

    Google Scholar 

  3. Mattern DL, Jaw LC, Guo T-H et al (1998) Using eural networks for sensor validation [M]. National Aeronautics and Space Administration, Lewis Research Center pp 73–114

    Google Scholar 

  4. Moller JC, Litt JS, Guo T-H (1998) Neural network-based sensor validation for turboshaft engines [R]. AIAA 98–3605

    Google Scholar 

  5. Aretakis N, Mathioudakis K (2004) A. stamatis. Identification of sensor faults on turbofan engines using pattern recognition techniques [J]. Control Eng Pract 12(7):827–836

    Article  Google Scholar 

  6. Benwei L, Zhaoyuan F, Yonghua W et al (2007) Research on sensor fault diagnosis of X type engine based on SVR [J]. J Aerosp Power 22(10):1754–1759

    Google Scholar 

  7. Feng L, Jinquan H, Li C et al (2009) Fault diagnosis of fusion aero engine sensor based on SPSO-SVR [J]. J Aerosp Power 24(8):1856–1865

    Google Scholar 

  8. Yongping Z, Jianguo S, Jiankang W (2009) Online parsimonious least squares support vector regression and its application [J]. Trans Nanjing Univ Aeronaut Astronaut 26(4):280–287

    MATH  Google Scholar 

  9. Zhao C (2012) Theoretical and experimental research on fault diagnosis and signal reconstruction of aero engine sensor [D]. Nanjing University of Aeronautics & Astronautics, Nanjing

    Google Scholar 

  10. Shiquan Y (2014) Fault diagnosis and fault tolerant control of aero engine actuator [D]. Nanjing University of Aeronautics & Astronautics, Nanjing

    Google Scholar 

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Correspondence to Lingfei Xiao .

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© 2016 Springer Science+Business Media Singapore

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Hu, J., Xiao, L. (2016). Multi-sensor Fault Diagnosis of Aircraft Engine Based on Kalman Filter Group. In: Jia, Y., Du, J., Zhang, W., Li, H. (eds) Proceedings of 2016 Chinese Intelligent Systems Conference. CISC 2016. Lecture Notes in Electrical Engineering, vol 404. Springer, Singapore. https://doi.org/10.1007/978-981-10-2338-5_36

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  • DOI: https://doi.org/10.1007/978-981-10-2338-5_36

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-2337-8

  • Online ISBN: 978-981-10-2338-5

  • eBook Packages: Computer ScienceComputer Science (R0)

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