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Attitude coordination control of spacecraft formation flying using rotation matrix

  • Harbin Institute of Technology

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

Abstract

We investigate the attitude coordination control of spacecraft formation flying associated with time-varying reference attitude tracking. The proposed control scheme is directly developed on special orthogonal group(SO(3)) to avoid ambiguities and singularities associated with the attitude representation of Rodrigues parameters or quaternions. The controller is presented by using a novel attitude error based on SO(3). Strict stability analysis is performed with the proper Lyapunov function. Simulation results are provided to demonstrate the effectiveness of the proposed control approach.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages6891-6895
Number of pages5
ISBN (Print)9789881563835
StatePublished - 18 Oct 2013
Event32nd Chinese Control Conference, CCC 2013 - Xi'an, China
Duration: 26 Jul 201328 Jul 2013

Publication series

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

Conference

Conference32nd Chinese Control Conference, CCC 2013
Country/TerritoryChina
CityXi'an
Period26/07/1328/07/13

Keywords

  • Attitude representation
  • Coordination control
  • Spacecraft formation flying
  • Special orthogonal group

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