Decentralized H control for attitude coordination of spacecraft formation

Pingli Lu*, Gang Liu, Xiangdong Liu

*Corresponding author for this work

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

1 Citation (Scopus)

Abstract

In this paper, a robust H decentralized controller is proposed for attitude coordination of spacecraft formation flying with external disturbance based on the relative attitudes and angular velocities of neighboring spacecraft. The controller is composed of nonlinear terms for performance enhancement and linear terms for attitude coordination and stabilization. The proposed control method guarantees the attitude alignment with zero final angular velocity and robust disturbance attenuation for spacecraft formation when the communication topology is connected. A feature of the proposed approach is that the robust H controller parameters can be obtained by solving linear matrix inequalities (LMIs), which makes the design more transparent. Finally, the numerical simulations of a spacecraft formation are provided to show the effectiveness of the proposed consensus algorithm.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages3171-3176
Number of pages6
ISBN (Electronic)9789881563934
DOIs
Publication statusPublished - 7 Sept 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

  • Attitude coordination
  • linear matrix inequality
  • multiple spacecraft
  • nonlinear H control
  • spacecraft formation

Fingerprint

Dive into the research topics of 'Decentralized H control for attitude coordination of spacecraft formation'. Together they form a unique fingerprint.

Cite this