Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method

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	Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method
	Liang, K.K.2; Chen L(陈丽)1; Liu JG(刘金国)3
	2019
会议日期	July 5-7, 2019
会议地点	Xiamen, China
关键词	Multi-propeller Aerostat fault-tolerant control trajectory tacking control sliding mode control control allocation
页码	529-534
英文摘要	This article develops a fault-tolerant control strategy for a multi-propeller aerostat based on sliding mode control allocation approach. And the loss of effectiveness of propeller faults and the wind disturbance is considered in the system. The proposed control approach consists of two modules: the upper-level virtual control part, which is developed to enable the closed loop system asymptotically stable; the lower-level control allocation part, which can accommodate the propeller faults, and redistribute the virtual control vector to the available propellers. Stability analysis indicates that the aerostat plant is globally asymptotically stable. The validity of the developed fault tolerant control strategy is proved through simulation results based on a simplified multi-propeller aerostat with propeller faults.
源文献作者	Academy of Opto-Electronics, Chinese Academy of Science ; Fujian Association of Automation ; IEEE Beijing Section ; Technical Committee on Fault Detection, Supervision, and Safety for Technical Processes, Chinese Association of Automation
产权排序	3
会议录	Proceedings of 2019 11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019
会议录出版者	IEEE
会议录出版地	New York
语种	英语
ISBN号	978-1-7281-0681-6
内容类型	会议论文
源URL	[http://ir.sia.cn/handle/173321/27838]
专题	沈阳自动化研究所_空间自动化技术研究室
通讯作者	Chen L(陈丽)
作者单位	1.School of Air Transportation, Shanghai University of Engineering Science, Shanghai 201620, China 2.School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China 3.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences(CAS), Shenyang 110016, China
推荐引用方式 GB/T 7714	Liang, K.K.,Chen L,Liu JG. Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method[C]. 见:. Xiamen, China. July 5-7, 2019.