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Adaptive fuzzy attitude control of satellite based on linearization

  • P. Guan*
  • , X. J. Liu
  • , F. Lara-Rosano
  • , J. B. Chen
  • *Corresponding author for this work
  • Beijing Institute of Technology
  • Universidad Nacional Autónoma de México

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

Abstract

Input-output (I/O) linearization is a typical control method in the nonlinear multi-input multi-output (MIMO) system. In this paper, adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The proposed control method is applied to the attitude maneuver control of the flexible satellite, which is a complex nonlinear system. The basic control structure is presented. The selection of the controller parameter, which guarantee the attitude stabilization of the satellite with parameter uncertainties, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties to increase the robustness of the controller. Simulation results show that precise attitude control is accomplished in spite of the uncertainty in the system.

Original languageEnglish
Title of host publicationProceedings of the 2004 American Control Conference (AAC)
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1091-1096
Number of pages6
ISBN (Print)0780383354
DOIs
Publication statusPublished - 2004
Event2004 American Control Conference, AAC 2004 - Boston, MA, United States
Duration: 30 Jun 20042 Jul 2004

Publication series

NameProceedings of the American Control Conference
Volume2
ISSN (Print)0743-1619

Conference

Conference2004 American Control Conference, AAC 2004
Country/TerritoryUnited States
CityBoston, MA
Period30/06/042/07/04

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