Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization

被引：652
作者：
Du, Haibo [1 ]
Li, Shihua [1 ]
Qian, Chunjiang [2 ]
机构：
[1] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[2] Univ Texas San Antonio, Dept Elect & Comp Engn, San Antonio, TX 78249 USA
来源：
IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 2011年 / 56卷 / 11期
基金：
高等学校博士学科点专项科研基金;
关键词：
Attitude control; attitude synchronization; finite-time control; spacecraft; STABILIZATION; FEEDBACK; VELOCITY; SYSTEMS;
D O I：
10.1109/TAC.2011.2159419
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This note investigates the finite-time attitude control problems for a single spacecraft and multiple spacecraft. First of all, a finite-time controller is designed to solve finite-time attitude tracking problem for a single spacecraft. Rigorous proof shows that the desired attitude can be tracked in finite time in the absence of disturbances. In the presence of disturbances, the tracking errors can reach a region around the origin in finite time. Then, based on the neighbor rule, a distributed finite-time attitude control law is proposed for a group of spacecraft with a leader-follower architecture. Under the finite-time control law, the attitude synchronization can be achieved in finite time.
引用
收藏
页码：2711 / 2717
页数：7
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