Robust control of an uncertain UAV via high-order sliding mode compensation

被引:8
|
作者
Davila, Jorge [1 ]
Salazar, Sergio [2 ]
机构
[1] ESIME UPT, Sect Grad Studies & Res, IPN, Mexico City, DF, Mexico
[2] LAFMIA, CINVESTAV, IPN, Mexico City, DF, Mexico
来源
IFAC PAPERSONLINE | 2017年 / 50卷 / 01期
关键词
Attitude control; Quadrotor systems; High-Order Sliding Modes; BACKSTEPPING CONTROL; TRACKING;
D O I
10.1016/j.ifacol.2017.08.1636
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 article addresses the design of a robust tracking controller for a quadrotor Unmanned Aircraft Vehicle (UAV). The dynamics of the quadrotor contains uncertainties, nonlinearities and external disturbances that are not considered for the designing of the controller, which is designed using a combination of state-feedback linearization and high order sliding modes. A state-feedback linearizing controller is applied for tracking of reference signals on the nominal model of the quadrotor, while the high-order sliding mode is applied to compensate for uncertainties and external disturbances in the dynamics. It is shown in numerical simulations that the proposed controller provides exact tracking in the absence of noise. Experimental results in a laboratory prototype illustrates the workability of the proposed methodology. (C) 2017, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
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页码:11553 / 11558
页数:6
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