Flight control design using extended state observer and non-smooth feedback

被引：0

作者：

Huang, Y ^{[1
]}

Xu, KK ^{[1
]}

Han, JQ ^{[1
]}

Lam, J ^{[1
]}

机构：

[1] Chinese Acad Sci, AMSS, Inst Syst Sci, Beijing 100864, Peoples R China

来源：

PROCEEDINGS OF THE 40TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-5 | 2001年

关键词：

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：

This paper proposes a novel nonlinear approach for high performance flight control design. The dynamic linearization is accomplished via a kind of unknown input observer, called Extended State Observer. A non-smooth feedback law is employed to achieve the desirable dynamic performances. A Lyapunov function is constructed for the proposed method.

引用

页码：223 / 228

页数：6

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