四元数
控制理论(社会学)
观察员(物理)
非线性系统
姿态控制
航天器
国家(计算机科学)
控制(管理)
国家观察员
分散系统
共识
计算机科学
班级(哲学)
数学
多智能体系统
控制工程
工程类
物理
人工智能
航空航天工程
算法
量子力学
几何学
出处
期刊:Automatica
[Elsevier]
日期:2014-04-01
卷期号:50 (4): 1109-1115
被引量:203
标识
DOI:10.1016/j.automatica.2014.01.003
摘要
In this paper, we consider the leader-following consensus problem for a multiple rigid spacecraft system whose attitude is represented by the unit quaternion. Most results on this problem rely on the assumption that every follower can access the state of the leader and are obtained via a decentralized control manner. By developing a nonlinear distributed observer for the leader system, we can solve this problem via a distributed control scheme under the mild assumptions that the state of the leader can reach every follower through a path and that the communication between followers is bidirectional. Moreover, our result can accommodate a class of desired angular velocities generated by a marginally stable linear autonomous system.
科研通智能强力驱动
Strongly Powered by AbleSci AI