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

Research output: Contribution to conference › Paper

Abstract

© 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.

Original language	English
DOIs	https://doi.org/10.1109/ICA-ACCA.2016.7778464
State	Published - 8 Dec 2016
Event	2016 IEEE International Conference on Automatica, ICA-ACCA 2016 - University of Talca, Curicó, Chile Duration: 19 Oct 2016 → 21 Oct 2016

Conference

Conference	2016 IEEE International Conference on Automatica, ICA-ACCA 2016
Abbreviated title	ICA-ACCA 2016
Country/Territory	Chile
City	Curicó
Period	19/10/16 → 21/10/16

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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}",

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

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T1 - Experimental identification of the transfer function model of a scale VTOL system by PRBS signals under ground effect

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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ER -

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

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