Leader-following adaptive consensus of multiple uncertain rigid spacecraft systems

作     者：He CAI Jie HUANG 

作者机构：Shenzhen Research Institute The Chinese University of Hong Kong Department of Mechanical and Automation Engineering The Chinese University of Hong KongShatin N.T. 

出 版 物：《Science China(Information Sciences)》 (中国科学:信息科学(英文版))

年 卷 期：2016年第59卷第1期

页      面：6-18页

核心收录：

学科分类：08[工学] 081105[工学-导航、制导与控制] 0811[工学-控制科学与工程] 

基　　金：been supported in part by National Natural Science Foundation of China(Grant No.61174049) Research Grants Council of the Hong Kong Special Administration Region(Grant No.412813) 

主　　题：adaptive control attitude consensus multi-agent system nonlinear distributed observer parameter convergence 

摘      要：The existing results on the leader-following attitude consensus for multiple rigid spacecraft systems assume that all the parameters of the spacecraft systems are known exactly and the information flow among the followers is bidirectional. In this paper, we remove these two assumptions. First, by introducing a new Lyapunov function, we allow the communication network to be directed. Second, we convert the leader-following consensus problem into an adaptive stabilization problem of a well defined error system. Then, under the standard assumption that the state of the leader system can reach every follower through a directed path, we further show that this stabilization problem is solvable by a distributed adaptive control law. Moreover, we also present the sufficient condition for guaranteeing the convergence of the estimated parameters to the unknown actual parameters.