Modeling and Control of a Tilt tri-rotor Airplane

被引：0
|
作者：
Duc Anh Ta
Fantoni, Isabelle
Lozano, Rogelio
机构：
来源：
2012 AMERICAN CONTROL CONFERENCE (ACC) | 2012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：
A helicopter offers the capability of hover, slow forward displacement, vertical take-off and landing while a conventional airplane has the performance of fast forward movement, long reach and superior endurance. The aim of this paper is to present the modelling and control of a tilt tri-rotor UAV's configuration that combines the advantages of both rotary wing and fixed wing vehicle.
引用
收藏
页码：131 / 136
页数：6
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