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Takagi-Sugeno Fuzzy Model based attitude control for Flexible Spacecraft via Disturbance Observer

  • Harbin Institute of Technology Shenzhen

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

Abstract

Attitude stabilization control via disturbance observer for flexible spacecraft is studied in this paper. First, a model based on Takagi-Sugeno fuzzy system of flexible spacecraft is established. In the case of spacecraft subjected to the external disturbance, the external disturbance and flexible accessories are treated as one disturbance. Furthermore, the lumped disturbance is no longer limited by bounded or zero-order derivatives. Then, a disturbance observer is proposed to estimate it while the gains are determined by the convergence condition of the estimation error. According to the obtained estimate, an integral sliding surface is selected so that the control law is partially composed of PDCC. At last, the effectiveness of the disturbance observer and attitude control law are illustrated by an example of a flexible spacecraft.

Original languageEnglish
Title of host publicationProceedings of the 39th Chinese Control Conference, CCC 2020
EditorsJun Fu, Jian Sun
PublisherIEEE Computer Society
Pages712-717
Number of pages6
ISBN (Electronic)9789881563903
DOIs
StatePublished - Jul 2020
Externally publishedYes
Event39th Chinese Control Conference, CCC 2020 - Shenyang, China
Duration: 27 Jul 202029 Jul 2020

Publication series

NameChinese Control Conference, CCC
Volume2020-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference39th Chinese Control Conference, CCC 2020
Country/TerritoryChina
CityShenyang
Period27/07/2029/07/20

Keywords

  • Quaternion model
  • Takagi-Sugeno fuzzy model
  • attitude control

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