Dynamic modelling and experimental identification of four rotors helicopter parameters

被引：0

作者：

Derafa, L. ^{[1
]}

Madani, T. ^{[2
]}

Benallegue, A. ^{[2
]}

机构：

[1] Lab Controle & Commande EMP, Bordj El Bahri, Algiers 16111, Algeria

[2] Lab Ingn Syst Versailles, F-78140 Versailles, France

来源：

2006 IEEE INTERNATIONAL CONFERENCE ON INDUSTRIAL TECHNOLOGY, VOLS 1-6 | 2006年

关键词：

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

In this paper an experimental identification of dynamic parameters of a four rotors mini helicopter is presented. An appropriate model for identification and control synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects, aerodynamic friction. A comparison between simulated and real system is made in closed loop system using a same controller. The obtained results show the good estimation of the dynamic model.

引用

页码：2213 / +

页数：2