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Global fast terminal sliding mode control for quadrotor UAV

  • Oualid Doukhi
  • , Abdurrazzaq Fayjie
  • , Deok Jin Lee*
  • *Corresponding author for this work
  • Kunsan National University

Research output: Contribution to conferenceConference paperpeer-review

Abstract

This paper presents the mathematical model of the quadrotor unmanned aerial vehicle (UVA) and then proposes a Global Fast Terminal Sliding Mode Controller to achieve trajectory tracking capability, the control system is decoupled into two parts, inner loop for attitude control and outer loop for position control, the stability analyses for the proposed controller is proven via Lyapunov stability theory. Simulations are conducted to demonstrate the effectiveness of the designed global fast terminal sliding mode controller comparing it with the regular sliding mode control.

Original languageEnglish
Title of host publicationICCAS 2017 - 2017 17th International Conference on Control, Automation and Systems - Proceedings
PublisherIEEE Computer Society
Pages1180-1182
Number of pages3
ISBN (Electronic)9788993215137
DOIs
StatePublished - 2017.12.13
Event17th International Conference on Control, Automation and Systems, ICCAS 2017 - Jeju, Korea, Republic of
Duration: 2017.10.182017.10.21

Publication series

NameInternational Conference on Control, Automation and Systems
Volume2017-October
ISSN (Print)1598-7833

Conference

Conference17th International Conference on Control, Automation and Systems, ICCAS 2017
Country/TerritoryKorea, Republic of
CityJeju
Period17.10.1817.10.21

Keywords

  • Fast Terminal Sliding Mode Control
  • Quadrotor
  • Trajectory Tracking
  • Unnamed aerial vehicle(UVA)

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