Experimental identification of the transfer function model of a scale VTOL system by PRBS signals under ground effect

Cristian Carangui; Paul Delgado; Marco Carpio; Diego Paul Chacon-Troya

doi:10.1109/ICA-ACCA.2016.7778464

Experimental identification of the transfer function model of a scale VTOL system by PRBS signals under ground effect

Cristian Carangui
, Paul Delgado
, Marco Carpio
, Diego Paul Chacon-Troya

Producción científica: Contribución a una conferencia › Documento

1 Cita (Scopus)

Resumen

© 2016 IEEE. Change from a resting state to a full launch on any device that has the characteristic of flight and vertical landing is a major challenge when the control system must be designed. In this sense, there are different effects that alter its dynamics. In this paper, an experimental method based on pseudo-random bit signals (PRBS) is proposed to identify the transfer function of a vertical take-off and landing (VTOL) system. According to the results, an equation for the system response is proposed to describe the performance of the mechanism. The modeling of the whole VTOL system is studied under the ground effect. Matlab and LabVIEW software were used to perform the research.

Idioma original	Inglés
DOI	https://doi.org/10.1109/ICA-ACCA.2016.7778464
Estado	Publicada - 8 dic. 2016
Evento	2016 IEEE International Conference on Automatica, ICA-ACCA 2016 - University of Talca, Curicó, Chile Duración: 19 oct. 2016 → 21 oct. 2016

Conferencia

Conferencia	2016 IEEE International Conference on Automatica, ICA-ACCA 2016
Título abreviado	ICA-ACCA 2016
País/Territorio	Chile
Ciudad	Curicó
Período	19/10/16 → 21/10/16

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317A Electricidad y energía

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10.1109/ICA-ACCA.2016.7778464

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title = "Experimental identification of the transfer function model of a scale VTOL system by PRBS signals under ground effect",

abstract = "{\textcopyright} 2016 IEEE. Change from a resting state to a full launch on any device that has the characteristic of flight and vertical landing is a major challenge when the control system must be designed. In this sense, there are different effects that alter its dynamics. In this paper, an experimental method based on pseudo-random bit signals (PRBS) is proposed to identify the transfer function of a vertical take-off and landing (VTOL) system. According to the results, an equation for the system response is proposed to describe the performance of the mechanism. The modeling of the whole VTOL system is studied under the ground effect. Matlab and LabVIEW software were used to perform the research.",

author = "Cristian Carangui and Paul Delgado and Marco Carpio and Chacon-Troya, \{Diego Paul\}",

year = "2016",

month = dec,

day = "8",

doi = "10.1109/ICA-ACCA.2016.7778464",

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AU - Carangui, Cristian

AU - Delgado, Paul

AU - Carpio, Marco

AU - Chacon-Troya, Diego Paul

PY - 2016/12/8

Y1 - 2016/12/8

N2 - © 2016 IEEE. Change from a resting state to a full launch on any device that has the characteristic of flight and vertical landing is a major challenge when the control system must be designed. In this sense, there are different effects that alter its dynamics. In this paper, an experimental method based on pseudo-random bit signals (PRBS) is proposed to identify the transfer function of a vertical take-off and landing (VTOL) system. According to the results, an equation for the system response is proposed to describe the performance of the mechanism. The modeling of the whole VTOL system is studied under the ground effect. Matlab and LabVIEW software were used to perform the research.

AB - © 2016 IEEE. Change from a resting state to a full launch on any device that has the characteristic of flight and vertical landing is a major challenge when the control system must be designed. In this sense, there are different effects that alter its dynamics. In this paper, an experimental method based on pseudo-random bit signals (PRBS) is proposed to identify the transfer function of a vertical take-off and landing (VTOL) system. According to the results, an equation for the system response is proposed to describe the performance of the mechanism. The modeling of the whole VTOL system is studied under the ground effect. Matlab and LabVIEW software were used to perform the research.

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U2 - 10.1109/ICA-ACCA.2016.7778464

DO - 10.1109/ICA-ACCA.2016.7778464

M3 - Paper

T2 - 2016 IEEE International Conference on Automatica, ICA-ACCA 2016

Y2 - 19 October 2016 through 21 October 2016

ER -

Experimental identification of the transfer function model of a scale VTOL system by PRBS signals under ground effect

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