Observer-Based Finite-Time Attitude Containment Control of Multiple Spacecraft Systems

被引：28
|
作者：
Chen, Xiao [1 ]
Zhao, Lin [1 ]
机构：
[1] Qingdao Univ, Coll Automat, Qingdao 266071, Peoples R China
来源：
IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS II-EXPRESS BRIEFS | 2021年 / 68卷 / 04期
基金：
中国国家自然科学基金;
关键词：
Attitude control; Backstepping; Space vehicles; Protocols; Observers; Uncertainty; Synchronization; Cooperative attitude control; containment control; output feedback; finite-time control; backstepping;
D O I：
10.1109/TCSII.2020.3024941
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In this brief, the output feedback based finite-time attitude containment control problem for multiple spacecrafts is investigated. A novel finite-time command filtered backstepping containment control scheme is proposed for attitude systems with unmeasurable states, inertia uncertainties, external disturbances and input saturations, which can not only guarantee the containment control errors converge to the sufficient small neighborhood of the origin in finite-time, but also overcome the computation complexity problem in traditional backstepping. The simulation results show the effectiveness of the proposed control scheme.
引用
收藏
页码：1273 / 1277
页数：5
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