Event-Triggered Finite-Time Adaptive Coordinated Control for Spacecraft Formation Flying Under Actuator Faults

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

Abstract

For attitude coordination tracking of spacecraft formation flying affected by external disturbances, actuator faults, and limited communication, this paper investigates a finite-time adaptive coordinated control law. To suppress the influence of external disturbances and actuator faults, an adaptive sliding mode controller is adopted. To reduce the communication between neighboring spacecraft, a distributed event-triggered control scheme is designed. Under the scheme, the communication channel only transmits information at the trigger instants that are decided by the predefined triggering condition. Based on the Lyapunov theorem, the stability of the closed-loop system can be proved. The effectiveness of the scheme is verified by simulation results.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
EditorsLiang Yan, Haibin Duan, Yimin Deng, Liang Yan
PublisherSpringer Science and Business Media Deutschland GmbH
Pages2043-2052
Number of pages10
ISBN (Print)9789811966125
DOIs
StatePublished - 2023
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China
Duration: 5 Aug 20227 Aug 2022

Publication series

NameLecture Notes in Electrical Engineering
Volume845 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2022
Country/TerritoryChina
CityHarbin
Period5/08/227/08/22

Keywords

  • Actuator faults
  • External disturbances
  • Finite-time adaptive coordinated control
  • Limited communication
  • Spacecraft formation flying

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