南方科技大学知识苑(SUSTech KC): Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach

题名	Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
作者	Duan Guangquan 1; Liu Guo-Ping1,2
通讯作者	Duan Guangquan
发表日期	2022-04-01
DOI	10.1007/s11424-022-1492-y
发表期刊	Journal of Systems Science & Complexity 影响因子和分区
ISSN	1009-6124
EISSN	1559-7067
卷号	35 期号:2页码:623-640
摘要	This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization control of combined spacecraft. The stability of the system is proved by introducing Lyapunov function. Numerical simulation of the combined spacecraft and physical experiment based on the combined spacecraft simulator (CSS) are completed. Both simulation and experiment results demonstrate the effectiveness and practicability of the optimal controller of fully-actuated system.
关键词	Attitude control combined spacecraft fully-actuated system optimal controller orbit control
相关链接	[来源记录]
收录类别	SCI ; EI
语种	英语
学校署名	其他
资助项目	National Natural Science Foundation of China[62173255,62188101]
WOS研究方向	Mathematics
WOS类目	Mathematics, Interdisciplinary Applications
WOS记录号	WOS:000786419800013
出版者	SPRINGER HEIDELBERG
EI入藏号	20221611987177
EI主题词	Controllers ; Lyapunov functions ; Orbits ; Spacecraft ; System stability
EI分类号	Spacecraft, General:655.1 ; Specific Variables Control:731.3 ; Control Equipment:732.1 ; Mathematics:921 ; Systems Science:961
来源库	Web of Science
引用统计	被引频次[WOS]：26
成果类型	期刊论文
条目标识符	http://sustech.caswiz.com/handle/2SGJ60CL/333465
专题	工学院_电子与电气工程系
作者单位	1.Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Peoples R China 2.Southern Univ Sci & Technol, Dept Elect & Elect Engn, Shenzhen 518055, Peoples R China
推荐引用方式 GB/T 7714	Duan Guangquan,Liu Guo-Ping. Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach[J]. Journal of Systems Science & Complexity,2022,35(2):623-640.
APA	Duan Guangquan,&Liu Guo-Ping.(2022).Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach.Journal of Systems Science & Complexity,35(2),623-640.
MLA	Duan Guangquan,et al."Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach".Journal of Systems Science & Complexity 35.2(2022):623-640.