Extended State Observer Based Sliding Mode Control for a Tilt Rotor UAV

被引:0
|
作者
Lin, Huangxing [1 ]
Fu, Rong [1 ]
Zeng, Jianping [1 ]
机构
[1] Xiamen Univ, Dept Automat, Xiamen 361005, Fujian, Peoples R China
基金
中国国家自然科学基金;
关键词
Tilt rotor; sliding mode control; extended state observer;
D O I
暂无
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 focuses on the transition flight control for a small tilt rotor unmanned aerial vehicle (UAV). Aiming at the longitudinal model of a tilt rotor UAV, a novel sliding mode control (SMC) method is proposed to guarantee that the states converge to the desired sliding surfaces in finite time. Moreover, extended state observers (ESOs) are provided to enhance the system's robustness to the uncertainties. Simulations show the effectiveness of the proposed approach.
引用
收藏
页码:3771 / 3775
页数:5
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