Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control

doi:10.1177/0954410017731590

CIOMP OpenIR

	Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control
	Fu, Chunyang 1; Tian, Yantao 1,2; Peng, Cheng 3; Gong, Xun 3; Zhang, Lei 1; Guo, Xiaojun 1
	2019
发表期刊	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
ISSN	0954-4100
卷号	233 期号:1 页码:180-196
通讯作者	Tian, Yantao(tianyt@jlu.edu.cn)
摘要	This paper deals with the controllers design using a novel siding mode control and proportional-derivative control for the trajectory tracking problem of a new multi-rotor aircraft, which experiences angular velocity sensor faults and external disturbances. The control system is divided into two parts: the inner loop for attitude subsystem and outer loop for position subsystem. For the inner loop, the angular velocity sensor faults, including bias, drift, loss of accuracy, and loss of effectiveness are considered as equivalent mismatched disturbances, while the system internal coupling, nonlinearity, and external disturbances are considered as equivalent matched disturbances. A novel sliding mode control approach is proposed for inner loop controller design, which includes a nonlinear disturbance observer to estimate both mismatched and matched disturbances, a novel switching surface based on the estimation of the mismatched disturbance to counteract its impact, a double power reaching law to attenuate the chattering problem, and a compensation for the matched disturbance to reduce the controller gains. The sensor faults are handled without fault detection and controller reconfiguration, making the method require less computation and easy implementation. The proposed method enhances the robustness without sacrificing the nominal properties. For outer loop, the proportional-derivative approach is used to design the virtual controller. The closed-loop system stability is proved by the Lyapunov theory. Finally, various simulation experiments are shown to validate the effectiveness, robustness, and the superiority of the proposed flight control scheme.
关键词	Multi-rotor aircraft sensor fault sliding mode control mismatched disturbance nonlinear disturbance observer chattering attenuation
DOI	10.1177/0954410017731590
关键词[WOS]	MISMATCHED UNCERTAIN SYSTEMS ; FLIGHT CONTROL ; SURFACE ; DESIGN ; HELICOPTER ; VEHICLE
收录类别	SCI
语种	英语
资助项目	National Natural Science Foundation of China[11372309] ; National Natural Science Foundation of China[61304017] ; Science & Technology Development Project of Jilin Province, China[20150204074GX] ; Jilin University 985 Project'' Engineering Bionic Sci ; National Natural Science Foundation of China[11372309] ; National Natural Science Foundation of China[61304017] ; Science & Technology Development Project of Jilin Province, China[20150204074GX] ; Jilin University 985 Project'' Engineering Bionic Sci
项目资助者	National Natural Science Foundation of China ; Science & Technology Development Project of Jilin Province, China ; Jilin University 985 Project'' Engineering Bionic Sci
WOS研究方向	Engineering
WOS类目	Engineering, Aerospace ; Engineering, Mechanical
WOS记录号	WOS:000454948300014
出版者	SAGE PUBLICATIONS LTD
引用统计	被引频次：11[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://ir.ciomp.ac.cn/handle/181722/60113
专题	中国科学院长春光学精密机械与物理研究所
通讯作者	Tian, Yantao
作者单位	1.Jilin Univ, Coll Commun Engn, Changchun, Jilin, Peoples R China 2.Jilin Univ, Key Lab Bion Engn, Minist Educ, Changchun, Jilin, Peoples R China 3.Chinese Acad Sci, Changchun Inst Opt Fine Mech & Phys, Changchun, Jilin, Peoples R China
推荐引用方式 GB/T 7714	Fu, Chunyang,Tian, Yantao,Peng, Cheng,et al. Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,2019,233(1):180-196.
APA	Fu, Chunyang,Tian, Yantao,Peng, Cheng,Gong, Xun,Zhang, Lei,&Guo, Xiaojun.(2019).Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,233(1),180-196.
MLA	Fu, Chunyang,et al."Sensor faults tolerance control for a novel multi-rotor aircraft based on sliding mode control".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING 233.1(2019):180-196.