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
收藏
页码：604 / 610
页数：7
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