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Research on aircraft taxiing lateral control based on fuzzy controller

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.

Original languageEnglish
Title of host publicationProceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011
Pages582-587
Number of pages6
DOIs
StatePublished - 2011
Event2011 International Conference on Fluid Power and Mechatronics, FPM 2011 - Beijing, China
Duration: 17 Aug 2011 → 20 Aug 2011

Publication series

NameProceedings of 2011 International Conference on Fluid Power and Mechatronics, FPM 2011

Conference

Conference2011 International Conference on Fluid Power and Mechatronics, FPM 2011
Country/TerritoryChina
CityBeijing
Period17/08/11 → 20/08/11

Keywords

  • Anti-skid braking system
  • Fuzzy control
  • Lateral control
  • Reference velocity

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