Robust backstepping-based trajectory tracking control for quadrotors with time delays

被引:29
|
作者
Liu, Hao [1 ,2 ]
Zhao, Wanbing [1 ,2 ]
Hong, Sheng [3 ]
Lewis, Frank L. [4 ]
Yu, Yao [5 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Beihang Univ, Minist Educ, Key Lab Spacecraft Design Optimizat & Dynam Simul, Beijing 100191, Peoples R China
[3] Beihang Univ, Sch Cyber Sci & Technol, Beijing 100191, Peoples R China
[4] Univ Texas Arlington, Res Inst, Ft Worth, TX 76118 USA
[5] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
来源
IET CONTROL THEORY AND APPLICATIONS | 2019年 / 13卷 / 12期
基金
中国国家自然科学基金;
关键词
position control; uncertain systems; aircraft control; control system synthesis; robust control; nonlinear control systems; tracking; adaptive control; helicopters; control nonlinearities; control approach; controller parameters; on-line unidirectional tuning method; tracking errors; robust compensation theory; backstepping method; robust cascade trajectory tracking controller; input time delays; state; unmodelled uncertainties; nonlinearity; under-actuated system subject; quadrotor dynamical model; uncertain quadrotor systems; robust trajectory tracking control problem; quadrotors; robust backstepping-based trajectory tracking control; SLIDING MODE CONTROL; H-INFINITY CONTROL; SYSTEMS; STABILIZATION; HELICOPTER; VEHICLE;
D O I
10.1049/iet-cta.2018.6043
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this brief, the robust trajectory tracking control problem is addressed for uncertain quadrotor systems with time delays. The quadrotor dynamical model is an under-actuated system subject to non-linearity, unmodelled uncertainties, parametric perturbations, external disturbances, and state and input time delays. A robust cascade trajectory tracking controller is developed by the backstepping method and the robust compensation theory. Theoretical analysis is given to prove that the tracking errors can converge into the given neighbourhood of the origin ultimately. An on-line unidirectional tuning method is given to determine the controller parameters. Experimental results are provided to verify the effectiveness of the proposed control approach and the parameter tuning method.
引用
收藏
页码:1945 / 1954
页数:10
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