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Design of Sliding Mode Controller with Self-adaption for a Morphing Aircraft

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

Abstract

With different flight conditions and tasks, the morphing aircraft can change its shape to obtain optimal aerodynamic performance. In this paper, a controller design method for linear parameter-varying (LPV) system is studied. Firstly, the establishment process of LPV model is introduced. The open loop dynamic responses of LPV model and actual nonlinear model are compared. Then, on the basis of satisfying the Linear Matrix Inequality (LMI) condition of Lyapunov stability, a class of finite time convergent self-adaptive sliding mode variable structure controller (ASMC) is designed, and the stability of the model is proved. Finally, the simulation result shows that the above controller can maintain global stability of variant process when the external upper bound is unknown.

Original languageEnglish
Title of host publicationProceedings 2018 Chinese Automation Congress, CAC 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages122-127
Number of pages6
ISBN (Electronic)9781728113128
DOIs
StatePublished - 2 Jul 2018
Event2018 Chinese Automation Congress, CAC 2018 - Xi'an, China
Duration: 30 Nov 20182 Dec 2018

Publication series

NameProceedings 2018 Chinese Automation Congress, CAC 2018

Conference

Conference2018 Chinese Automation Congress, CAC 2018
Country/TerritoryChina
CityXi'an
Period30/11/182/12/18

Keywords

  • LPV model
  • morphing aircraft
  • self-adaption
  • sliding mode control

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