Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy

Carlos Aguilar-Ibanez, Miguel S. Suarez-Castanon, Nareli Cruz-Cortes, Julio Mendoza-Mendoza

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

Resumen

A control strategy for the regulation of a PVTOL, based on output-feedback, is introduced. To this end, a couple of controllers or actuators that operate concurrently are proposed. One of them stabilizes the vertical variable in finite time, by means of a novel sliding mode controller. The other actuator uses the energy control approach to balance, simultaneously, the horizontal and angular variables. The needed velocity is computed using the well-known supertwisting algorithm, which works independently of the controllers. To verify the performance of the stabilizing strategy, a numerical experiment and a numerical comparison among two well-known control strategies, were carried out.

Idioma originalInglés
Título de la publicación alojada2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015
EditorialInstitute of Electrical and Electronics Engineers Inc.
ISBN (versión digital)9781467378390
DOI
EstadoPublicada - 14 dic. 2015
Evento12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015 - Mexico City, México
Duración: 26 oct. 201530 oct. 2015

Serie de la publicación

Nombre2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015

Conferencia

Conferencia12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015
País/TerritorioMéxico
CiudadMexico City
Período26/10/1530/10/15

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