Finite-Time Sliding Mode Trajectory Tracking Control of Uncertain Mechanical Systems

被引:41
作者
Sun, Liang [1 ]
Zheng, Zewei [1 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国博士后科学基金;
关键词
Finite-time control; sliding mode control; trajectory tracking; uncertain mechanical systems; RIGID SPACECRAFT; CONVERGENCE;
D O I
10.1002/asjc.1377
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The problem of finite-time tracking control is studied for uncertain nonlinear mechanical systems. To achieve finite-time convergence of tracking errors, a simple linear sliding surface based on polynomial reference trajectory is proposed to enable the trajectory tracking errors to converge to zero in a finite time, which is assigned arbitrarily in advance. The sliding mode control technique is employed in the development of the finite-time controller to guarantee the excellent robustness of the closed-loop system. The proposed sliding mode scheme eliminates the reaching phase problem, so that the closed-loop system always holds the invariance property to parametric uncertainties and external disturbances. Lyapunov stability analysis is performed to show the global finite-time convergence of the tracking errors. A numerical example of a rigid spacecraft attitude tracking problem demonstrates the effectiveness of the proposed controller.
引用
收藏
页码:399 / 404
页数:6
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