Integrated fault estimation and fault-tolerant control for a flexible regional aircraft

被引：0
|
作者：
Yishi LIU [1 ,2 ]
Sheng HONG [1 ]
Enrico ZIO [3 ,4 ,5 ]
Jianwei LIU [1 ]
机构：
[1] 不详
[2] School of Cyber Science and Technology, Beihang University
[3] 不详
[4] School of Automation Science and Electrical Engineering, Beihang University
[5] Department of Energy, Politecnico di Milano
[6] MINES Paris Tech, PSL Research University,CRC
[7] Eminent Scholar, Department of Nuclear Engineering, College of Engineering, Kyung Hee University
[8] 不详
来源：
Chinese Journal of Aeronautics | 2022年 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The article focuses on the design and application of an active reconfigurable controller that mitigates the effects of gust load and actuator faults on a flexible aircraft. A novel integrated adaptive output feedback scheme is investigated to address the actuator faults. The real-time fault values provided by the fault estimation module are considered in the reconfigurable control law to improve the fault-tolerant capability. The estimate values of faults and control gains are calculated by analyzing the stability of the overall system. The proposed controller is simulated using a flexible aircraft model with a discrete ‘1-cosine' gust, and the results show that it can effectively mitigate the wing root moments and recover the flight maneuver stability after the aircraft suffered from gusts.
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页码：390 / 399
页数：10
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