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Cross-coupling Attitude Synchronous Control of Satellite Formation via Fast Terminal Sliding Mode

  • Shuo Han
  • , Yinhao Ju*
  • , Siqi Chen
  • , Feilong Tang
  • , Yiming Wang
  • , Guanghui Sun
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology
  • Harbin Institute of Technology
  • China University of Petroleum (East China)

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

Abstract

In this paper, a novel attitude synchronous control strategy, by combining the cross-coupling synchronous method and non-singular fast terminal sliding mode controller (NFTSMC), is proposed for satellite formation systems with external disturbances and perturbations. First, the attitude dynamics and kinematics models of the considered satellite are presented. Second, to realize robust and fast attitude synchronization control, a NFTSMC is designed, whose convergence and stability are ensured based on Lyapunov theory. Then, an effective cross-coupling synchronous method, considering the synchronous error of adjacent satellites attitude control, is proposed, which can achieve the preferable unified regulation of satellite formation. Finally, sufficient numerical simulations are provided to verify the effectiveness and synchronizability of the proposed control strategy.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control and Decision Conference, CCDC 2024
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages4736-4741
Number of pages6
ISBN (Electronic)9798350387780
DOIs
StatePublished - 2024
Externally publishedYes
Event36th Chinese Control and Decision Conference, CCDC 2024 - Xi'an, China
Duration: 25 May 202427 May 2024

Publication series

NameProceedings of the 36th Chinese Control and Decision Conference, CCDC 2024

Conference

Conference36th Chinese Control and Decision Conference, CCDC 2024
Country/TerritoryChina
CityXi'an
Period25/05/2427/05/24

Keywords

  • attitude control
  • cross-coupling synchronous
  • satellite formation systems
  • sliding mode control

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