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Composite attitude control for flexible spacecrafts with input saturation

  • Hua Liu*
  • , Yumin Zhang
  • , Chonggang Ren
  • *Corresponding author for this work

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

Abstract

We propose a new composite anti-disturbance control approach with guaranteed input saturation. Such a composite control has two hierarchical loops. The vibrations of flexible appendalges are formulated as one type of disturbances with bounded derivative, for which the disturbance-observer-based controller is designed to compensate in the feed-forward loop. Other disturbances originated from space environment, measurement, actuator and un-modeled dynamics, are merged into the second type of disturbance described by a norm bounded variable. H ∞ state-feedback controller is designed to attenuate the merged disturbance. The input saturation of the actuator is also taken into account in the controller design. The concerned problem is simplfied into a robust control problem via solution of linear matrix inequalities. Numerical simulations and comparisons show that by combining the disturbance observer with H ∞ control, the pointing accuracy of flexible spacecrafts can be improved.

Original languageEnglish
Title of host publicationProceedings of 2018 IEEE 3rd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2018
EditorsBing Xu
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages2325-2329
Number of pages5
ISBN (Electronic)9781538645086
DOIs
StatePublished - 14 Dec 2018
Event3rd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2018 - Chongqing, China
Duration: 12 Oct 201814 Oct 2018

Publication series

NameProceedings of 2018 IEEE 3rd Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2018

Conference

Conference3rd IEEE Advanced Information Technology, Electronic and Automation Control Conference, IAEAC 2018
Country/TerritoryChina
CityChongqing
Period12/10/1814/10/18

Keywords

  • Attitude control
  • Disturbance Observer Based Control
  • H∞ control
  • Input Saturation

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