Sliding mode control attitude tracking of rigid spacecraft using adaptive back-stepping method

Chunmei Yu, Kunfeng Lu, Yuanqing Xia, Hailiang Liu

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

2 Citations (Scopus)

Abstract

The attitude tracking control problem for a rigid spacecraft system is investigated in this paper. A novel adaptive approach is proposed with the utilization of sliding mode control (SMC) and backstepping technique (BT) to achieve accurate attitude tracking control for spacecraft system in the presence of inertia uncertainties and external disturbances. Finally, simulation results are presented to illustrate effectiveness of the control strategies.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages3281-3286
Number of pages6
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

  • Adaptive control
  • Attitude tracking
  • Backstepping technique
  • Sliding mode control

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