Attitude control for quadrotors subjected to wind disturbances via active disturbance rejection control and integral sliding mode control

被引:72
作者
Zhao, Ling [1 ,2 ]
Dai, LiuWei [1 ]
Xia, Yuanqing [3 ]
Li, Peng [4 ]
机构
[1] Yanshan Univ, Sch Mech Engn, Qinhuangdao 066004, Hebei, Peoples R China
[2] Tianjin Univ, State Key Lab Precis Measuring Technol & Instrume, Tianjin 300072, Peoples R China
[3] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[4] Yanshan Univ, Inst Elect Engn, Qinhuangdao 066004, Hebei, Peoples R China
基金
北京市自然科学基金; 中国国家自然科学基金;
关键词
Quadrotors; Attitude control; Wind disturbances; Active disturbance rejection control; Integral sliding mode control; TRAJECTORY TRACKING CONTROL; EXTENDED STATE OBSERVER; HELICOPTER SUBJECT; SYSTEMS; STABILIZATION; VEHICLE; DESIGN; UAV;
D O I
10.1016/j.ymssp.2019.04.040
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, attitude control is investigated for a quadrotor subjected to wind disturbances based on a double closed-loop control strategy. The double closed-loop control strategy integrates advantages of active disturbance rejection control and integral sliding mode control. A nonlinear extended state observer is adopted in the inner loop to estimate internal uncertain dynamics and external wind disturbances timely for the quadrotor. Furthermore, both estimation errors of the nonlinear extended state observer and tracking errors of the double closed-loop control strategy are shown to be convergent through Lyapunov theory. Finally, experimental results are provided to demonstrate effectiveness of the proposed method. (C) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页码:531 / 545
页数:15
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