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
收藏
页码：3454 / 3459
页数：6
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