@inproceedings{14af8066a59f408da99682f80c98b1a2,
title = "Non-singular terminal sliding mode controller for spacecraft attitude stabilization",
abstract = "In this paper, the finite-time attitude control problem for rigid spacecraft with external disturbance is addressed. First, a problem of existing non-singular terminal sliding mode is raised, and then we design a non-singular finite-time attitude controller by using a special Lyapunov function with a power integrator form, which enables the system states converge to a residual set in a finite time. Further, an adaptive non-singular terminal sliding mode controller is proposed to deal with the external disturbance. Numerical simulations are performed to illustrate the effectiveness of the proposed control schemes with fast convergence, high accuracy and good disturbance rejection property in the spacecraft control system.",
keywords = "adaptive control, finite-time control, spacecraft attitude stabilization, terminal sliding mode",
author = "Chuanjiang Li and Boyan Jiang and Qinghua Zhu and Chentao Yu",
note = "Publisher Copyright: {\textcopyright} 2015 Technical Committee on Control Theory, Chinese Association of Automation.; 34th Chinese Control Conference, CCC 2015 ; Conference date: 28-07-2015 Through 30-07-2015",
year = "2015",
month = sep,
day = "11",
doi = "10.1109/ChiCC.2015.7259755",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "907--912",
editor = "Qianchuan Zhao and Shirong Liu",
booktitle = "Proceedings of the 34th Chinese Control Conference, CCC 2015",
address = "美国",
}