Design of sliding mode control system for automatic transition and hover of helicopter

Honggang Gao, Zhenghong Gao, Yangping Deng, Ziyu Zhao

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

2 Scopus citations

Abstract

In this paper, a T-S fuzzy model of helicopter transition and hover is established as the dynamic characteristics of the helicopter vary with decline of height and decrease of speed. Based on the performance index requirement of automatic transition and hover, the pole assignment method is used to determine the feedback control parameters and regulating controller in full envelope of the automatic transition and hover is designed according to the theory of parallel distributed compensation. Eventually the sliding mode control law is designed. The simulation results show that the designed system in this paper is feasible and effective.

Original languageEnglish
Title of host publication2017 3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages102-105
Number of pages4
ISBN (Electronic)9781538604847
DOIs
StatePublished - 26 Oct 2017
Event3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017 - Beijing, China
Duration: 17 Aug 201719 Aug 2017

Publication series

Name2017 3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017

Conference

Conference3rd IEEE International Conference on Control Science and Systems Engineering, ICCSSE 2017
Country/TerritoryChina
CityBeijing
Period17/08/1719/08/17

Keywords

  • T-S fuzzy model
  • automatic transition and hover
  • helicopter
  • sliding mode control

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