Disturbance observer based finite-time coordinated attitude tracking control for spacecraft on SO(3)

被引：7
|
作者：
Shi Zhen [1 ]
Xie Yaen [2 ]
Deng Chengchen [1 ]
Zhao Kun [1 ]
He Yushan [1 ]
Hao Yong [1 ]
机构：
[1] Harbin Engn Univ, Coll Automat, Harbin 150001, Peoples R China
[2] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Peoples R China
来源：
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS | 2020年 / 31卷 / 06期
基金：
中国国家自然科学基金;
关键词：
coordinated attitude control; disturbance observer; rotation matrix; attitude synchronization control; MULTIPLE SPACECRAFT; SYNCHRONIZATION;
D O I：
10.23919/JSEE.2020.000098
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
To solve the problem of attitude synchronization control for spacecraft formation flying (SFF) suffering from external disturbances under a directed communication topology, a sliding mode disturbance observer (SMDO) based on the finite-time control strategy is developed to observe the time-varying external disturbance via estimating the upper bound of its first derivative. Meanwhile, the rotation matrix is employed to describe the attitude of SFF for the purpose of the avoidance of singularity and unwinding phenomenon. As for the attitude synchronization and the tracking control architecture, a sliding mode surface (SMS) is given such that the control objective can be achieved. The effectiveness and the validity of the proposed method are elaborated via theoretical analysis and numerical simulations.
引用
收藏
页码：1274 / 1285
页数：12
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