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Fault-tolerant control for a Multi-propeller Aerostat based on sliding mode control allocation method
Liang, K.K.1; Chen L(陈丽)2; Liu JG(刘金国)3
Department空间自动化技术研究室
Conference Name11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019
Conference DateJuly 5-7, 2019
Conference PlaceXiamen, China
Author of SourceAcademy 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
Source PublicationProceedings of 2019 11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019
PublisherIEEE
Publication PlaceNew York
2019
Pages529-534
Indexed ByEI
EI Accession number20204409440781
Contribution Rank3
ISBN978-1-7281-0681-6
KeywordMulti-propeller Aerostat fault-tolerant control trajectory tacking control sliding mode control control allocation
AbstractThis 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.
Language英语
Document Type会议论文
Identifierhttp://ir.sia.cn/handle/173321/27838
Collection空间自动化技术研究室
Corresponding AuthorChen L(陈丽)
Affiliation1.School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China
2.School of Air Transportation, Shanghai University of Engineering Science, Shanghai 201620, China
3.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences(CAS), Shenyang 110016, China
Recommended Citation
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]//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. New York:IEEE,2019:529-534.
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