Nonlinear H∞ decoupling hover control of helicopter with parameter uncertainties

被引：0

作者：

Yang, CD ^{[1
]}

Liu, WH ^{[1
]}

机构：

[1] Natl Cheng Kung Univ, Inst Aeronaut & Astronaut, Tainan 701, Taiwan

来源：

PROCEEDINGS OF THE 2003 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2003年

关键词：

nonlinear H-infinity control; helicopter control; hovering mode; parameter uncertainty;

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：

Taking into account of parameter uncertainties within nonlinear helicopter model, we show in this paper that the six degree-of-freedom nonlinear H. controller designed for hovering helicopter can be exactly separated into two three degree-of-freedom controllers, one for translational motion and the other for rotational motion, even though longitudinal and lateral dynamics of helicopters in hovering are highly nonlinear and severely coupled.

引用

页码：3454 / 3459

页数：6

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