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

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

Resumen

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.

Idioma originalInglés
Título de la publicación alojadaProceedings - 2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014
EditorialInstitute of Electrical and Electronics Engineers Inc.
Páginas146-151
Número de páginas6
ISBN (versión digital)9781479942237
DOI
EstadoPublicada - 2014
Evento2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014 - Cuernavaca, Morelos, México
Duración: 18 nov. 201421 nov. 2014

Serie de la publicación

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

Conferencia

Conferencia2014 IEEE International Conference on Mechatronics, Electronics, and Automotive Engineering, ICMEAE 2014
País/TerritorioMéxico
CiudadCuernavaca, Morelos
Período18/11/1421/11/14

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