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Distributed adaptive finite-time configuration control of spacecraft formation

  • Harbin Institute of Technology

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

Abstract

This paper designed a finite-time configuration control law that can weaken chattering under the directed communication topology. The leader information is available to only a portion of the followers and the existence of generalized disturbance in the dynamics model is considered. By defining the error function of relative configuration and selecting the appropriate variables of the finite-time high-order sliding-mode control, the sign function appears in the derivative of the control force, a strictly distributed configuration control law with the integral form of sign function is obtained and improves the convergence speed while reducing the chattering. An adaptive estimation law is proposed when the upper bound of the generalized disturbance is unknown. The finite-time characteristics of the proposed distributed adaptive control law are proved by Lyapunov method. Through the simulation analysis and comparison with other algorithm, the validity of the proposed algorithm is verified.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages8649-8655
Number of pages7
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

  • Spacecraft formation control
  • distributed control
  • finite-time control
  • formation configuration control

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