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Reconfigurable control design based on complete parametric approach for spacecraft rendezvous

  • Harbin Institute of Technology

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

Abstract

This paper studies the problem of reconfigurable fault tolerant controller design for linear time-invariant systems with measurement unavailability based on a complete parametric approach. The attention is focused on completely recovering eigenvalues of the pre-fault system by resynthesizing an output feedback controller while the restrictions on assignable eigenvalues of existing results are overcome. Further, the complete parametric method is introduced to give the parametric expressions for all output feedback matrices with the advantage of guaranteeing the stability of the reconfigured system. What's more, recon-figurable controllers for the spacecraft rendezvous system are studied as the example in cases of different measurement failure situations. Finally, numerical calculations are given and results show the effectiveness of the proposed method.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages7410-7415
Number of pages6
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
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

  • Complete Parametric Approach
  • Measurement Unavailability
  • Output Feedback
  • Reconfigurable Control
  • Spacecraft Rendezvous

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