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

doi:10.1109/ICEEE.2015.7357963

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

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

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.

Original language	English
Title of host publication	2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781467378390
DOIs	https://doi.org/10.1109/ICEEE.2015.7357963
State	Published - 14 Dec 2015
Event	12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015 - Mexico City, Mexico Duration: 26 Oct 2015 → 30 Oct 2015

Publication series

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

Conference

Conference	12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015
Country/Territory	Mexico
City	Mexico City
Period	26/10/15 → 30/10/15

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10.1109/ICEEE.2015.7357963

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Aguilar-Ibanez, C., Suarez-Castanon, M. S., Cruz-Cortes, N., & Mendoza-Mendoza, J. (2015). Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy. In 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015 Article 7357963 (2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICEEE.2015.7357963

Aguilar-Ibanez, Carlos ; Suarez-Castanon, Miguel S. ; Cruz-Cortes, Nareli et al. / Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy. 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015. Institute of Electrical and Electronics Engineers Inc., 2015. (2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015).

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

abstract = "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.",

author = "Carlos Aguilar-Ibanez and Suarez-Castanon, {Miguel S.} and Nareli Cruz-Cortes and Julio Mendoza-Mendoza",

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Aguilar-Ibanez, C , Suarez-Castanon, MS, Cruz-Cortes, N & Mendoza-Mendoza, J 2015, Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy. in 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015., 7357963, 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015, Institute of Electrical and Electronics Engineers Inc., 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015, Mexico City, Mexico, 26/10/15. https://doi.org/10.1109/ICEEE.2015.7357963

Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy. / Aguilar-Ibanez, Carlos ; Suarez-Castanon, Miguel S.; Cruz-Cortes, Nareli et al.
2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015. Institute of Electrical and Electronics Engineers Inc., 2015. 7357963 (2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Mendoza-Mendoza, Julio

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N2 - 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.

AB - 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.

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Aguilar-Ibanez C , Suarez-Castanon MS, Cruz-Cortes N, Mendoza-Mendoza J. Output feedback stabilization for a PVTOL aircraft based on a sliding mode combined with an energy control strategy. In 2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015. Institute of Electrical and Electronics Engineers Inc. 2015. 7357963. (2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control, CCE 2015). doi: 10.1109/ICEEE.2015.7357963

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

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