Design for aircraft engine multi-objective controllers with switching characteristics

IMR OpenIR

	Design for aircraft engine multi-objective controllers with switching characteristics
其他题名	Design for aircraft engine multi-objective controllers with switching characteristics
	Liu Xiaofeng 1; Shi Jing 1; Qi Yiwen 2; Yuan Ye 1
	2014
发表期刊	Chinese Journal of Aeronautics
ISSN	1000-9361
卷号	27 期号:5 页码:1097-1110
摘要	The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formulated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions.
其他摘要	The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formu-lated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions.
关键词	Aircraft engine Compensatory controller Min/Max switching Multi-objectives control Smooth switching Switching scheme Motor vehicles. Aeronautics. Astronautics TL1-4050
收录类别	CSCD
语种	英语
资助项目	[National Natural Science Foundation of China] ; [Innovation Plan of Aero Engine Complex System Safety by the Ministry of Education Chang Jiang Scholars of China]
CSCD记录号	CSCD:5279795
引用统计
文献类型	期刊论文
条目标识符	http://ir.imr.ac.cn/handle/321006/147516
专题	中国科学院金属研究所
作者单位	1.北京航空航天大学 2.中国科学院金属研究所
推荐引用方式 GB/T 7714	Liu Xiaofeng,Shi Jing,Qi Yiwen,et al. Design for aircraft engine multi-objective controllers with switching characteristics[J]. Chinese Journal of Aeronautics,2014,27(5):1097-1110.
APA	Liu Xiaofeng,Shi Jing,Qi Yiwen,&Yuan Ye.(2014).Design for aircraft engine multi-objective controllers with switching characteristics.Chinese Journal of Aeronautics,27(5),1097-1110.
MLA	Liu Xiaofeng,et al."Design for aircraft engine multi-objective controllers with switching characteristics".Chinese Journal of Aeronautics 27.5(2014):1097-1110.