Automatic Landing controller Design and Simulation of Flying-Wing Unmanned Aerial Vehicle

被引：0

作者：

Zhang Jianfeng ^{[1
]}

Jia Caijuan ^{[1
]}

机构：

[1] Northwestern Polytech Univ, Inst 365, Xian 710072, Peoples R China

来源：

PROCEEDINGS OF 2013 2ND INTERNATIONAL CONFERENCE ON MEASUREMENT, INFORMATION AND CONTROL (ICMIC 2013), VOLS 1 & 2 | 2013年

关键词：

automatic landing; flying-wing; unmanned aerial vehicle; simulation;

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 method of guidance and control for automatic landing of flying-wing unmanned aerial vehicle (UAV) is proposed in this paper. Based on wind tunnel data of a flying-wing aircraft, small disturbance equations of the flying-wing aircraft is built using MATLAB. With the help of the model, automatic landing plan and control law is designed. Simulation and analysis are finished based on non-linear equations. The final simulation results show that the guidance and control law can meet the requirements of automatic landing of UAV, and has excellent static and dynamic performances.

引用

页码：893 / 896

页数：4

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