Modeling and Control of a Quadrotor UAV

被引：0

作者：

Walid, Mizouri ^{[1
]}

Slaheddine, Najar ^{[1
]}

Mohamed, Aoun ^{[1
]}

Lamjed, Bouabdallah ^{[1
]}

机构：

[1] Univ Gabes, Natl Engn Sch Gabes ENIG, Zrig Eddakhlania, Tunisia

来源：

201415th International Conference on Sciences & Techniques of Automatic Control & Computer Engineering (STA'2014) | 2014年

关键词：

Quadrotor; Unmanned Aerial Vehicles(UAV); Modelling; PD control; Trajectory;

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：

In the recent years, the control of Unmanned Aerial Vehicles (UAV) has become one of the most interesting field of research, especially for Vertical Take-Off and Landing vehicles (VTOL), due to the needs to such system, the simplicity of their construction and due to the important technological advances in control boards, sensors, communication tools, energy storage. In this paper, a mathematical model has been developed with Lagrange formalism and a control approach based on Proportional Derivative PD controller has been built and provided with numerical simulation in MATLAB/Simulink.

引用

页码：343 / 348

页数：6

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