Real-Time Adaptive Model of Mainstream Parameters for Aircraft Engines Based on Oselm-Ekf

Author:

Guo Yingchen,Teng Jiazhu,Zhou Xin,Zou Zelong,Huang Jinquan,Lu Feng

Publisher

Elsevier BV

Reference31 articles.

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2. A novel compound fault-tolerant method based on online sequential extreme learning machine with cycle reservoir for turbofan engine direct thrust control;X Zhou;Aerospace Science and Technology,2023

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4. Degradation effects on combined cycle power plant performance-part I: gas turbine cycle component degradation effects;A Zwebek;ASME. J Eng Gas Turbines Power,2003

5. Hybrid state estimation for aircraft engine anomaly detection and fault accommodation;F Lu;AIAA Journal,2020

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