Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies

被引：44

作者：

Chen, Zhiyong ^{[1
]}

Huang, Jie ^{[2
]}

机构：

[1] Univ Newcastle, Sch Elect Engn & Comp Sci, Callaghan, NSW 2308, Australia

[2] Chinese Univ Hong Kong, Dept Mech & Automat Engn, Shatin, Hong Kong, Peoples R China

来源：

INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL | 2014年 / 24卷 / 16期

基金：

澳大利亚研究理事会;

关键词：

nonlinear systems; adaptive control; spacecraft systems; output regulation; NONLINEAR OUTPUT REGULATION; INTERNAL-MODEL; SYSTEMS; STABILIZATION; FEEDBACK; DESIGN;

D O I：

10.1002/rnc.2983

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The asymptotic rejection of spacecraft systems under multi-tone sinusoidal disturbances has been studied recently for the case where the frequencies of the disturbance are known. In this paper, we further consider the case where the frequencies of the disturbance are unknown. We show that this case can be solved by an adaptive regulation technique. We also present some analysis on the convergence issue of the estimated frequencies to unknown frequencies. Copyright (c) 2013 John Wiley & Sons, Ltd.

引用

页码：2231 / 2242

页数：12

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