Robust vertical takeoff and landing aircraft control via integral sliding mode

被引：28

作者：

Huang, YJ

Kuo, TC

Way, HK

机构：

[1] Yuan Ze Univ, Dept Elect Engn, Chungli, Taiwan

[2] Natl Chiao Tung Univ, Dept Commun Engn, Hsinchu, Taiwan

来源：

IEE PROCEEDINGS-CONTROL THEORY AND APPLICATIONS | 2003年 / 150卷 / 04期

关键词：

D O I：

10.1049/ip-cta:20030593

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Reduced equivalent systems have inherent closed-loop poles at the origin in the sliding mode for conventional sliding mode control (SMC). A systematic design strategy is developed for arbitrarily placing all SMC closed-loop poles. The speed control of a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight is investigated. An outstanding output tracking performance and robustness against system parameter uncertainties and external disturbances are achieved.

引用

页码：383 / 388

页数：6

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