Finite-time Formation Reconfiguration of Multiple Spacecraft with Collision Avoidance Problems

被引:0
|
作者
Zhou Ning [1 ]
Chen Riqing [1 ]
Xia Yuanqing [2 ]
Huang Jie [3 ]
机构
[1] Fujian Agr & Forestry Univ, Coll Comp & Informat Sci, Fuzhou 350002, Peoples R China
[2] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[3] Univ Groningen, Fac Math & Nat Sci, NL-9747 AG Groningen, Netherlands
关键词
Formation Reconfiguration; Finite-time Control; Obstacle Avoidance; Coordination Control; ATTITUDE COORDINATION CONTROL; OPTIMIZATION;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, the problem of finite-time formation reconfiguration control for a platoon of multiple spacecraft is discussed. Each spacecraft is in the presence of external disturbances. By employing a novel predesigned desired velocity and an elaborate adaptive law, a finite-time coordination control scheme is presented to drive all the spacecraft to implement the formation reconfiguration task in unknown obstacle environments without using accurate mathematical model. Finally, numerical example shows that the proposed algorithm successfully implements the formation reconfiguration task and achieves high control accuracy without breaking any priority rules.
引用
收藏
页码:3200 / 3205
页数:6
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