Robust adaptive spacecraft attitude tracking control based on similar skew-symmetric structure

被引：7
|
作者：
Liu, Yi-Cheng [1 ]
Zhang, Jing [1 ]
Zhang, Tao [2 ]
Song, Jing-Yan [2 ]
机构：
[1] Sichuan Univ, Coll Elect Engn & Informat Technol, Chengdu 610065, Peoples R China
[2] Tsinghua Univ, Dept Automat, Beijing 100084, Peoples R China
来源：
COMPUTERS & ELECTRICAL ENGINEERING | 2016年 / 56卷
基金：
中国国家自然科学基金;
关键词：
Similar skew-symmetric structure; Attitude tracking; Robust adaptive; Backstepping; Disturbance attenuation; RIGID SPACECRAFT; NONLINEAR TRACKING; MANEUVERS; DESIGN; DISTURBANCES;
D O I：
10.1016/j.compeleceng.2016.10.007
中图分类号：
TP3 [计算技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper addresses robust adaptive attitude tracking control for spacecrafts with unknown inertia parameters and bounded external disturbances. The similar skew-symmetric structure is chosen as the desired structure for the closed loop system when there exist no uncertainties. Based on this idea, a backstepping scheme is proposed to design the controller, and adaptive compensation and robust compensation are introduced to deal with the uncertainty of the inertia parameters and the external disturbances respectively. Theoretical analysis shows that fast response and high tracking precision can both be obtained by regulating the related parameters in the proposed controller. Simulation results are provided to demonstrate the effectiveness of the proposed attitude tracking control algorithm. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码：784 / 794
页数：11
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