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Longitudinal attitude control of UAV based on fuzzy PID

  • Beihang University
  • Beijing New Aerotropolis

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

Abstract

Aiming at the characteristics of time-varying, nonlinear model of unmanned aerial vehicle (UAV), a fuzzy PID controller is proposed in this paper for longitudinal attitude of UAV with combination of fuzzy control algorithm and PID control algorithm. The proposed strategy is easy to be accepted and convenient for application. The fuzzy PID controller designed in this paper takes error and error change rate as input. The PID parameters are adjusted with fuzzy control rules such that the controlled object obtains a better dynamic and stable performance. The simulation results show that the designed fuzzy PID controller has the characteristics of fast response, small overshoot and small steady-state error.

Original languageEnglish
Title of host publication2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781538611715
DOIs
StatePublished - Aug 2018
Event2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, China
Duration: 10 Aug 201812 Aug 2018

Publication series

Name2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Conference

Conference2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Country/TerritoryChina
CityXiamen
Period10/08/1812/08/18

Keywords

  • Longitudinal attitude control
  • PID parameters
  • UAV
  • fuzzy control

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