Finite-time fault-tolerant control for rigid spacecraft with actuator saturations

被引：97
|
作者：
Lu, Kunfeng [1 ]
Xia, Yuanqing [1 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
来源：
IET CONTROL THEORY AND APPLICATIONS | 2013年 / 7卷 / 11期
基金：
中国国家自然科学基金;
关键词：
SLIDING-MODE CONTROL; ATTITUDE STABILIZATION; TRACKING;
D O I：
10.1049/iet-cta.2012.1031
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 study investigates the finite-time attitude-tracking problem for rigid spacecraft. A novel non-singular terminal sliding-mode control (NTSMC) law is designed to provide finite-time convergence and fast, high control precision even though inertia uncertainties and external disturbances affect the spacecraft systems under actuator failures and saturations. The proposed NTSMC scheme is chattering suppression and singularity-free. Simulation results are presented to demonstrate the efficiency of the proposed method.
引用
收藏
页码：1529 / 1539
页数：11
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