Nonlinear characteristic model-based SMC and its application to flexible satellites

L. Chen, Y. Yan, C. Y. Sun

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

6 Citations (Scopus)

Abstract

This study investigates the sliding mode control (SMC) method based on the nonlinear characteristic model and its application to flexible satellites. A novel nonlinear dynamic sliding mode surface is designed depending on the nonlinear characteristic model. The expected advantage of the proposed SMC compared to the traditional SMC is to improve performances and robustness. The proposed results apply to a class of nonlinear systems and rely on the parameter estimation of the characteristic model. The theory is illustrated on the rapid maneuver and fast stability problem of the sun synchronous orbit satellite.

Original languageEnglish
Title of host publication19th IFAC World Congress IFAC 2014, Proceedings
EditorsEdward Boje, Xiaohua Xia
PublisherIFAC Secretariat
Pages4595-4600
Number of pages6
ISBN (Electronic)9783902823625
DOIs
Publication statusPublished - 2014
Externally publishedYes
Event19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 - Cape Town, South Africa
Duration: 24 Aug 201429 Aug 2014

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
Volume19
ISSN (Print)1474-6670

Conference

Conference19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014
Country/TerritorySouth Africa
CityCape Town
Period24/08/1429/08/14

Keywords

  • Characteristic model
  • Flexible satellite
  • Rapid maneuver
  • Sliding mode control

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