Attitude control of a helicopter model by nonlinear sampled-data H∞ control

被引：0

作者：

Kato, A ^{[1
]}

Kobayashi, T ^{[1
]}

Katayama, H ^{[1
]}

Ichikawa, A ^{[1
]}

机构：

[1] Shizuoka Univ, Hamamatsu, Shizuoka 4328561, Japan

来源：

SICE 2003 ANNUAL CONFERENCE, VOLS 1-3 | 2003年

关键词：

H infinity control; affine nonlinear sampled-data system; helicopter model;

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：

We consider the attitude control of a helicopter model by affine nonlinear sampled-data H,, control. We first show that the nonliner dynamics of a helicopter model can be rewritten as an affine nonlinear system and then we design output feedback H-infinity controller. We show by simulation and experimental results that the output feedback H-infinity controller works

引用

页码：930 / 935

页数：6

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