Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique

被引：145
|
作者：
Song, Zhankui [1 ]
Li, Hongxing [1 ]
Sun, Kaibiao [1 ]
机构：
[1] Dalian Univ Technol, Fac Elect Informat & Elect Engn, Dalian 116024, Peoples R China
来源：
ISA TRANSACTIONS | 2014年 / 53卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Finite time; Fast terminal sliding mode control; Double closed loops; Spacecraft attitude control; FLEXIBLE SPACECRAFT; RIGID SPACECRAFT; STABILIZATION; ROBUST; SATELLITE; DISTURBANCES; STABILITY; TRACKING; DESIGN;
D O I：
10.1016/j.isatra.2013.08.008
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 paper, a fast terminal sliding mode control (FTSMC) scheme with double closed loops is proposed for the spacecraft attitude control. The FTSMC laws are included both in an inner control loop and an outer control loop. Firstly, a fast terminal sliding surface (FTSS) is constructed, which can drive the inner loop tracking-error and the outer loop tracking-error on the FTSS to converge to zero in finite time. Secondly, FTSMC strategy is designed by using Lyaponov's method for ensuring the occurrence of the sliding motion in finite time, which can hold the character of fast transient response and improve the tracking accuracy. It is proved that FTSMC can guarantee the convergence of tracking-error in both approaching and sliding mode surface. Finally, simulation results demonstrate the effectiveness of the proposed control scheme. (C) 2013 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码：117 / 124
页数：8
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