A fractional order sliding mode controller design for spacecraft attitude control system

Tianyi Zeng, Xuemei Ren, Yao Zhang

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

8 Citations (Scopus)

Abstract

As fractional order sliding mode controller has its unique advantages, it has been widely studied in recently years. This paper will discuss about the fractional order sliding mode controller and design a controller which is used into the spacecraft attitude system so that it can be with more quickness and strong robustness. A new sliding mode surface is proposed and it is proved that the system can be stable and can convergence in a finite time under this sliding mode surface. Simulation results show that this method can make the spacecraft attitude system has better performance.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages3379-3382
Number of pages4
ISBN (Electronic)9789881563897
DOIs
Publication statusPublished - 11 Sept 2015
Event34th Chinese Control Conference, CCC 2015 - Hangzhou, China
Duration: 28 Jul 201530 Jul 2015

Publication series

NameChinese Control Conference, CCC
Volume2015-September
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference34th Chinese Control Conference, CCC 2015
Country/TerritoryChina
CityHangzhou
Period28/07/1530/07/15

Keywords

  • Fractional order
  • sliding mode control
  • spacecraft attitude control

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