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Cooperative orbital control for satellite swarms with nonsingular terminal sliding mode and finite-time extended state observer

  • Harbin Institute of Technology

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

Abstract

In this paper, a nonsingular fast terminal sliding mode control law based on finite-time convergent extended state observer is designed for building large-scale swarm orbital configurations. First, a finite-time extended state observer is proposed to estimate the unknown external disturbance including J2 perturbation, atmosphere drag, etc. Second, based on the disturbance estimation, an orbital coordinated control law is developed to maintain the given configuration to achieve space missions. Finally, a simulation example is presented to illustrate the effectiveness of the proposed orbital coordinated control approach.

Original languageEnglish
Title of host publicationIECON 2022 - 48th Annual Conference of the IEEE Industrial Electronics Society
PublisherIEEE Computer Society
ISBN (Electronic)9781665480253
DOIs
StatePublished - 2022
Event48th Annual Conference of the IEEE Industrial Electronics Society, IECON 2022 - Brussels, Belgium
Duration: 17 Oct 202220 Oct 2022

Publication series

NameIECON Proceedings (Industrial Electronics Conference)
Volume2022-October
ISSN (Print)2162-4704
ISSN (Electronic)2577-1647

Conference

Conference48th Annual Conference of the IEEE Industrial Electronics Society, IECON 2022
Country/TerritoryBelgium
CityBrussels
Period17/10/2220/10/22

Keywords

  • extended state observer
  • finite time control
  • satellite swarm
  • sliding mode control

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