On Singular Perturbations of Flexible and Variable-Speed Wind Turbines
A model for the mechanical dynamics of a wind turbine is developed, which is the composition of three physical mechanisms: flexion, torsion, and rotational dynamics. A first contribution is the identification of the essential physical parameters that provide a time-scale separation of these three me...
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2012-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2012/860510 |
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doaj-ead098294aea4949874fc34ae2ce28a52020-11-24T23:05:13ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742012-01-01201210.1155/2012/860510860510On Singular Perturbations of Flexible and Variable-Speed Wind TurbinesR. Oulad Ben Zarouala0C. Vivas1J. Á. Acosta2L. El Bakkali3Departamento de Ingeniería de Sistemas y Automática, Universidad de Sevilla, Camino de los Descubrimientos s/n, 41092 Sevilla, SpainDepartamento de Ingeniería de Sistemas y Automática, Universidad de Sevilla, Camino de los Descubrimientos s/n, 41092 Sevilla, SpainDepartamento de Ingeniería de Sistemas y Automática, Universidad de Sevilla, Camino de los Descubrimientos s/n, 41092 Sevilla, SpainTeam Modelling and Simulation of Mechanical Systems, Faculty of Sciences at Tetouan, University Abdelmalek Essaadi, BP 2121, M’Hannech, 93002 Tetouan, MoroccoA model for the mechanical dynamics of a wind turbine is developed, which is the composition of three physical mechanisms: flexion, torsion, and rotational dynamics. A first contribution is the identification of the essential physical parameters that provide a time-scale separation of these three mechanisms. Under the assumption of singular perturbations the time-scale separation allows to work with a reduced model of order one. This reduction has been essential for the control of this system allowing to control designers to take into account only the reduced-order model. A second contribution consists in employing a measurement of the fore-aft nacelle acceleration with the reduced model, together with a Kalman filter to estimate the flexible DOFs of the system (tower and average blade deflection). The successful approach is tested on high-order nonlinear aeroelastic simulator (FAST).http://dx.doi.org/10.1155/2012/860510 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
R. Oulad Ben Zarouala C. Vivas J. Á. Acosta L. El Bakkali |
spellingShingle |
R. Oulad Ben Zarouala C. Vivas J. Á. Acosta L. El Bakkali On Singular Perturbations of Flexible and Variable-Speed Wind Turbines International Journal of Aerospace Engineering |
author_facet |
R. Oulad Ben Zarouala C. Vivas J. Á. Acosta L. El Bakkali |
author_sort |
R. Oulad Ben Zarouala |
title |
On Singular Perturbations of Flexible and Variable-Speed Wind Turbines |
title_short |
On Singular Perturbations of Flexible and Variable-Speed Wind Turbines |
title_full |
On Singular Perturbations of Flexible and Variable-Speed Wind Turbines |
title_fullStr |
On Singular Perturbations of Flexible and Variable-Speed Wind Turbines |
title_full_unstemmed |
On Singular Perturbations of Flexible and Variable-Speed Wind Turbines |
title_sort |
on singular perturbations of flexible and variable-speed wind turbines |
publisher |
Hindawi Limited |
series |
International Journal of Aerospace Engineering |
issn |
1687-5966 1687-5974 |
publishDate |
2012-01-01 |
description |
A model for the mechanical dynamics of a wind turbine is developed, which is the composition of three physical mechanisms: flexion, torsion, and rotational dynamics. A first contribution is the identification of the essential physical parameters that provide a time-scale separation of these three mechanisms. Under the assumption of singular perturbations the time-scale separation allows to work with a reduced model of order one. This reduction has been essential for the control of this system allowing to control designers to take into account only the reduced-order model. A second contribution consists in employing a measurement of the fore-aft nacelle acceleration with the reduced model, together with a Kalman filter to estimate the flexible DOFs of the system (tower and average blade deflection). The successful approach is tested on high-order nonlinear aeroelastic simulator (FAST). |
url |
http://dx.doi.org/10.1155/2012/860510 |
work_keys_str_mv |
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