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Robust adaptive dynamic surface control for attitude tracking of spacecraft

  • Chengbao Zhou
  • , Di Zhou*
  • *Corresponding author for this work
  • Harbin Institute of Technology

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

Abstract

The spacecraft attitude motion equations described by the Euler angles are expressed in vector form and viewed as two blocks, a kinematics block and a dynamics block. Based on Lyapunov stability theory, a robust dynamic surface control algorithm is designed for the nonlinear control system of attitude tracking of spacecraft in the presence of parameter uncertainty and external disturbances. Then, the robust dynamic surface algorithm is combined with an adaptive update law such that the controller can be used when the inertial moments of the attitude control system are not known. Lyapunov analysis shows that this adaptive controller can also guarantee the asymptotical stability of Euler angles. Finally, the effectiveness of the presented control algorithms is verified via simulations.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages5782-5788
Number of pages7
ISBN (Electronic)9789881563897
DOIs
StatePublished - 11 Sep 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
  • Dynamic surface control
  • Nonlinear control
  • Robust control
  • Spacecraft

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