Orbital Stability Analysis of Two-Relay Controller in Second Order Systems via Lyapunov Functions and Its Application to a 3-DOF Underactuated Helicopter

Luis T. Aguilar, Daniel Espinoza

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

Abstract

This paper deals with the solution of the periodic motion problem in a 3-DOF under actuated helicopter. A two-relay controller was proposed in order to induce self-oscillations in the helicopter. A new framework for orbital stability analysis based on Lyapunov functions was proposed for the closed-loop system. The performance of the proposed two-relay controller to induce self-oscillations into a laboratory under actuated 3-DOF helicopter was verified by simulations.

Original languageEnglish
Title of host publicationProceedings - 2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages146-151
Number of pages6
ISBN (Electronic)9781479942237
DOIs
StatePublished - 2014
Event2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014 - Cuernavaca, Morelos, Mexico
Duration: 18 Nov 201421 Nov 2014

Publication series

NameProceedings - 2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014

Conference

Conference2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014
Country/TerritoryMexico
CityCuernavaca, Morelos
Period18/11/1421/11/14

Keywords

  • Two-relay controller
  • self-oscillations
  • underactuated systems

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