Fault Tolerant Control Using a Fixed-time Second Order Sliding Mode

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

Abstract

In this article, a fault tolerant control (FTC) is proposed for a longitudinal aircraft model. A mathematic model for a pitch plane missile motion is established by considering actuator faults and system uncertainties. Subsequently, to achieve superior tracking performance compared with other sliding mode observers (SMO), a sliding model observer is designed to approximate system uncertainties and actuator faults as the lumped disturbances. Finally, a fixed-time second-order sliding mode controller is designed. Simulation results are given to show the effectiveness and advantages of the proposed method.

Original languageEnglish
Title of host publicationProceedings - 2019 2nd International Conference of Intelligent Robotic and Control Engineering, IRCE 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages91-95
Number of pages5
ISBN (Electronic)9781728141923
DOIs
StatePublished - Aug 2019
Event2nd International Conference of Intelligent Robotic and Control Engineering, IRCE 2019 - Singapore, Singapore
Duration: 26 Aug 201929 Aug 2019

Publication series

NameProceedings - 2019 2nd International Conference of Intelligent Robotic and Control Engineering, IRCE 2019

Conference

Conference2nd International Conference of Intelligent Robotic and Control Engineering, IRCE 2019
Country/TerritorySingapore
CitySingapore
Period26/08/1929/08/19

Keywords

  • actuator faults
  • fault tolerant control
  • fixed-time SMO
  • longitudinal aircraft model system
  • uncertainties

Fingerprint

Dive into the research topics of 'Fault Tolerant Control Using a Fixed-time Second Order Sliding Mode'. Together they form a unique fingerprint.

Cite this