Nonlinear Guidance and Control Laws for Three-Dimensional Target Tracking Applied to Unmanned Aerial Vehicles

被引：12

作者：

Subbarao, Kamesh ^{[1
]}

Ahmed, Mousumi ^{[1
]}

机构：

[1] Univ Texas Arlington, Dept Mech & Aerosp Engn, Arlington, TX 76019 USA

来源：

JOURNAL OF AEROSPACE ENGINEERING | 2014年 / 27卷 / 03期

关键词：

Trajectory tracking; Unmanned aerial vehicle (UAV); Nonlinear guidance; Backstepping;

D O I：

10.1061/(ASCE)AS.1943-5525.0000275

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, a backstepping-based nonlinear guidance controller is developed, designed for three-dimensional trajectory tracking for an unmanned aerial vehicle. The guidance law design assumes first-order dynamics for the speed, course/heading, and flight path angles. The three-dimensional kinematic model is simplified to yield a seemingly decoupled system that separates the course/heading from the flight path angle. A closed loop stability of the guidance laws via Lyapunov analysis is demonstrated, and the efficacy of the controller is illustrated for three representative cases.

引用

页码：604 / 610

页数：7

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