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论文类型：期刊论文

发表时间：2014-01-01

发表刊物：ISA TRANSACTIONS

收录刊物：PubMed、SCIE、EI

卷号：53

期号：1

页面范围：117-124

ISSN号：0019-0578

关键字：Finite time; Fast terminal sliding mode control; Double closed loops; Spacecraft attitude control

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.