Lyapunov-based trajectory tracking controller for a fixed-wing unmanned aerial vehicle in the presence of wind

被引:14
作者
Brezoescu, A. [1 ]
Lozano, R. [1 ]
Castillo, P. [1 ]
机构
[1] Univ Technol Compiegne, HEUDIASYC Lab UMR CNRS 7253, F-60203 Compiegne, France
关键词
adaptive control; Lyapunov stability; wind estimation; fixed-wing UAV; FLIGHT CONTROL;
D O I
10.1002/acs.2480
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper addresses the directional control problem of autonomous air vehicles in order to obtain trajectory tracking capabilities when flying in other than calm conditions. The control strategy is designed in the framework of the Lyapunov theory, and adaptive techniques are employed for online wind identification. An application of light fixed-wing unmanned aerial vehicles that consists in tracking straight-line paths between geo-referenced waypoints is first formulated, and the dynamic of the cross track error with respect to such trajectory is further obtained from the lateral airplane equations of motion. The dynamic order of the closed-loop adaptive system is guaranteed to be minimal by choosing the proper variables so that the tuning functions method could be applied. Several simulations taking into account unknown wind have been performed to analyze the behavior and the robustness of the control scheme. Copyright (c) 2014 John Wiley & Sons, Ltd.
引用
收藏
页码:372 / 384
页数:13
相关论文
共 22 条
[1]   Flight control of a rotary wing UAV using backstepping [J].
Ahmed, Bilal ;
Pota, Hemanshu R. ;
Garratt, Matt .
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2010, 20 (06) :639-658
[2]  
[Anonymous], 2007, P 15 MEDITERRANEAN C
[3]   Nonlinear adaptive flight control using neural networks [J].
Calise, AJ ;
Rysdyk, RT .
IEEE CONTROL SYSTEMS MAGAZINE, 1998, 18 (06) :14-25
[4]  
Etkins B., 1972, DYNAMICS ATMOSPHERIC
[5]   Coordinated standoff tracking of moving targets using Lyapunov guidance vector fields [J].
Frew, Eric W. ;
Lawrence, Dale A. ;
Morris, Steve .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (02) :290-306
[6]  
Gavilan F., 2011, IFAC Proc., V44, P1892, DOI [10.3182/20110828-6-IT-1002.01876, DOI 10.3182/20110828-6-IT-1002.01876]
[7]  
Harkergards O, 2003, THESIS LINKOPING U
[8]   Path Following for Unmanned Aerial Vehicles Using L1 Adaptive Augmentation of Commercial Autopilots [J].
Kaminer, Isaac ;
Pascoal, Antonio ;
Xargay, Enric ;
Hovakimyan, Naira ;
Cao, Chengyu ;
Dobrokhodov, Vladimir .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (02) :550-564
[9]   Modeling and control of a small autonomous aircraft having two tilting rotors [J].
Kendoul, Farid ;
Fantoni, Isabelle ;
Lozano, Rogelio .
IEEE TRANSACTIONS ON ROBOTICS, 2006, 22 (06) :1297-1302
[10]  
Khalils H, 1992, NONLINEAR SYSTEMS