Event-Triggered Adaptive Path-Following Control for Micro Helicopter

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

Abstract

This paper references a kind of path-following problem of a micro helicopter, which bases on the theories of vector field guidance method, adaptive sliding mode control, and event-triggered control. Firstly, to satisfy the requirements of aircraft position tracking, a method for accurate vector field guidance method is present. Secondly, in order to track the desired attitude which is calculated by the yaw after the vector field guidance method with disturbances, an adaptive sliding mode attitude controller is designed. Thirdly, to maintain the desired velocity, an adaptive velocity controller is introduced. Moreover, an event-triggered control method optimizes the controller’s outputting frequency. Stability analysis indicates that all variables are ultimately bounded. At the same time, the simulation results demonstrate the effectiveness of the mentioned control algorithm.

Original languageEnglish
Title of host publicationProceedings of 2019 Chinese Intelligent Systems Conference - Volume I
EditorsYingmin Jia, Junping Du, Weicun Zhang
PublisherSpringer Verlag
Pages670-680
Number of pages11
ISBN (Print)9789813296817
DOIs
StatePublished - 2020
EventChinese Intelligent Systems Conference, CISC 2019 - Haikou, China
Duration: 26 Oct 201927 Oct 2019

Publication series

NameLecture Notes in Electrical Engineering
Volume592
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceChinese Intelligent Systems Conference, CISC 2019
Country/TerritoryChina
CityHaikou
Period26/10/1927/10/19

Keywords

  • Event-trigger
  • Micro helicopter
  • Path-following
  • Sliding mode
  • Vector field

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