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Sampled-data H control for attitude stabilization and vibration suppression of flexible spacecrafts

  • Baolong Zhu
  • , Zhiping Zhang
  • , Mingliang Suo
  • , Zhenhua Yu
  • , Shunli Li
  • School of Astronautics, Harbin Institute of Technology

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

Abstract

This paper develops a sampled-data H control strategy for attitude stabilization and vibration suppression of flexible spacecrafts. After introducing an impulsive observer-based sampled-data controller, the closed-loop system is built as a type of hybrid systems consisting a continuous-time and an impulsive differential system. Based on Lyapunov functional method, a sufficient condition is derived such that the closed-loop system is asymptotic stable and satisfies a prescribed H performance. The minimum attenuation level and desired controller parameters can be obtained by solving a convex optimization problem involving linear matrix inequalities (LMIs). An illustrative design example proves the effectiveness of the developed sampled-data control strategy.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages6376-6381
Number of pages6
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
Externally publishedYes
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

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

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • Attitude stabilization
  • Flexible spacecrafts
  • Sampled-data control
  • Vibration suppression

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