Modified adaptive control for multi-spacecraft attitude coordination problems

Zhuo Zhang, Huiping Li

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

2 Scopus citations

Abstract

The distributed control of spacecraft attitude coordination problems is developed in this paper. An adaptive sliding-mode (SM) controller is designed to steer the attitude of multiple spacecrafts to synchronously reach zero. Then a modified chattering-free controller is proposed to eliminate the chattering of control inputs caused by the switching function. By utilizing the Lyapunov stability theory, we can prove that the presented approach ensures the multi-spacecraft attitude converge into a limited range. Finally, numerical examples are provided to illustrate that the modified control approach can achieve high control accuracy with eliminating the chattering in the presence of external disturbances and model uncertainties.

Original languageEnglish
Title of host publicationProceedings of 2018 IEEE 7th Data Driven Control and Learning Systems Conference, DDCLS 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages730-735
Number of pages6
ISBN (Electronic)9781538626184
DOIs
StatePublished - 30 Oct 2018
Event7th IEEE Data Driven Control and Learning Systems Conference, DDCLS 2018 - Enshi, Hubei Province, China
Duration: 25 May 201827 May 2018

Publication series

NameProceedings of 2018 IEEE 7th Data Driven Control and Learning Systems Conference, DDCLS 2018

Conference

Conference7th IEEE Data Driven Control and Learning Systems Conference, DDCLS 2018
Country/TerritoryChina
CityEnshi, Hubei Province
Period25/05/1827/05/18

Keywords

  • adaptive control
  • attitude coordination
  • chattering-free
  • distributed control
  • Multiple spacecraft

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