Modeling and control of a small autonomous aircraft having two tilting rotors

被引：0

作者：

Kendoul, Farid ^{[1
]}

Fantoni, Isabelle ^{[1
]}

Lozano, Rogelio ^{[1
]}

机构：

[1] Univ Technol Compiegne, Lab Heudiasyc, UMR 6599, CNRS, F-60200 Compiegne, France

来源：

2005 44th IEEE Conference on Decision and Control & European Control Conference, Vols 1-8 | 2005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：

This paper presents recent work concerning a small tiltrotor aircraft with a reduced number of rotors. After several attempts, the final design consists of two propellers mounted laterally. The direction of the thrust can be redirected by tilting the propellers laterally and longitudinally. A theoretical analysis of this. mechanism proves its effectiveness and the experimental results show that this aerodynamical configuration is very promising. A model of the full birotor dynamics is also presented in this paper and a controller based on the backstepping procedure is synthesized performing also an autonomous flight.

引用

页码：8144 / 8149

页数：6

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