Trajectory tracking control for micro unmanned aerial vehicles

被引：1

作者：

Zhai Ruiyong ^{[1
]}

Zhang Wendong ^{[1
]}

Zhou Zhaoying ^{[2
]}

Sang Shengbo ^{[1
]}

Li Pengwei ^{[1
]}

机构：

[1] Taiyuan Univ Technol, MicroNano Syst Res Ctr, Taiyuan, Peoples R China

[2] Tsinghua Univ, Dept Precis Instruments & Mechanol, Beijing, Peoples R China

来源：

ADVANCES IN APPLIED SCIENCE AND INDUSTRIAL TECHNOLOGY, PTS 1 AND 2 | 2013年 / 798-799卷

关键词：

Unmanned air vehicle (UAV); Lateral control; Longitudinal control; Micro-electro mechanical system (MEMS);

D O I：

10.4028/www.scientific.net/AMR.798-799.448

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

This article considers the problem of trajectory tracking control for a micro fixed-wing unmanned air vehicle (UAV). With Bank-to-Turn (BTT) method to manage lateral deviation control of UAV, this paper discusses the outer loop guidance system, which separates the vehicle guidance problems into lateral control loop and longitudinal control loop. Based on the kinematic model of the coordinated turning of UAV, the aircraft can track a pre-specified flight path with desired error range. Flight test results on a fixed-wing UAV have indicated that the trajectory tracking control law is quite effective.

引用

页码：448 / +

页数：2

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