Distributed Attitude Synchronization Control for Multiple Flexible Spacecraft Using Adaptive Sliding Mode

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	Distributed Attitude Synchronization Control for Multiple Flexible Spacecraft Using Adaptive Sliding Mode; Distributed Attitude Synchronization Control for Multiple Flexible Spacecraft Using Adaptive Sliding Mode
	Qishao Wang ; Yu Chen ; Zhisheng Duan
	2017
关键词	Attitude Synchronization Flexible Spacecraft Sliding Mode Adaptive Control Attitude Synchronization Flexible Spacecraft Sliding Mode Adaptive Control
英文摘要	This paper investigates the distributed attitude synchronization and tracking problem for a group of flexible spacecraft in the presence of external disturbances.The spacecraft formation is studied in an undirected leader-following architecture and the time-varying reference attitude is represented by a dynamic virtual leader.Applying the adaptive sliding mode mechanism,a distributed modified Rodriguez parameters-based synchronization control law is proposed for flexible spacecraft without using the elastic vibration modes.It is proved that the attitude synchronization can be achieved asymptotically under the control algorithm through the Lyapunov's stability analysis.A numerical simulation example of multiple flexible spacecraft formation is given to demonstrate the effectiveness of the proposed method.; This paper investigates the distributed attitude synchronization and tracking problem for a group of flexible spacecraft in the presence of external disturbances.The spacecraft formation is studied in an undirected leader-following architecture and the time-varying reference attitude is represented by a dynamic virtual leader.Applying the adaptive sliding mode mechanism,a distributed modified Rodriguez parameters-based synchronization control law is proposed for flexible spacecraft without using the elasti; 中国自动化学会控制理论专业委员会; 6
会议录	第36届中国控制会议
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/479537]
专题	工学院
推荐引用方式 GB/T 7714	Qishao Wang,Yu Chen,Zhisheng Duan. Distributed Attitude Synchronization Control for Multiple Flexible Spacecraft Using Adaptive Sliding Mode, Distributed Attitude Synchronization Control for Multiple Flexible Spacecraft Using Adaptive Sliding Mode[C]. 见:.