Attitude output feedback tracking control of satellites without angular velocity observers

Bing Xiao, Zhenzhou Fu, Yanning Guo

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

3 Scopus citations

Abstract

This work studies a difficult problem of rigid satellite attitude tracking control without angular velocity measurements. A new output feedback controller is presented by using attitude measurements only. The closed-loop tracking system is ensured to be asymptotically stable. The key feature of this approach is that in comparison with the conventional attitude output feedback control schemes by using angular velocity observers in the existing literature, any observer to estimate the unmeasured angular velocity is not required. The effectiveness of the developed approach is validated by a rigid satellite example with simulation results presented.

Original languageEnglish
Title of host publicationProceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages6544-6548
Number of pages5
ISBN (Electronic)9781538611272
DOIs
StatePublished - 15 Dec 2017
Externally publishedYes
Event43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017 - Beijing, China
Duration: 29 Oct 20171 Nov 2017

Publication series

NameProceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
Volume2017-January

Conference

Conference43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017
Country/TerritoryChina
CityBeijing
Period29/10/171/11/17

Keywords

  • asymptotic stability
  • attitude tracking
  • output feedback control
  • satellite
  • without angular velocity observers

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