Aircraft Engine Sensor Fault Diagnostics Based on Estimation of Engines Health Degradation

bank, the real faults that have occurred can be detected and isolated. The on-line fault detection algorithm has the ability of maintaining the effectiveness over the engine's lifetime and is verified by simulation using a nonlinear engine model.

作 者： Xue Wei Guo Yingqing   作者單位： School of Power and Energy, Northwestern Polytechnical University, Xi 'an 710072, China  刊 名： 中國航空學報（英文版）  ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS  年，卷(期)： 2009 22(1)  分類號： V2  關鍵詞： aerospace propulsion system   Kalman filter   health degradation   sensor fault diagnostics  

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