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Passification-based robust flight control design. / Fradkov, Alexander L.; Andrievsky, Boris.

In: Automatica, Vol. 47, No. 12, 12.2011, p. 2743-2748.

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Fradkov, Alexander L. ; Andrievsky, Boris. / Passification-based robust flight control design. In: Automatica. 2011 ; Vol. 47, No. 12. pp. 2743-2748.

BibTeX

@article{769d9576680e4ceda078940d546b4273,
title = "Passification-based robust flight control design",
abstract = "A passification-based robust autopilot for attitude control of flexible aircraft under parametric uncertainty is designed. A high gain controller with forced sliding motions is used to secure good performance over a wide range of the aircraft model parameters. The shunting method is applied to ensure closed-loop system stability under lack of aircraft state information. The series reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The simulation results demonstrate the efficiency and high robustness of the suggested control system. (C) 2011 Elsevier Ltd. All rights reserved.",
keywords = "Flight control, Uncertain dynamic systems, Shunt compensation, Robustness, Passification, SIMPLE ADAPTIVE-CONTROL, STABILIZATION, PASSIVITY",
author = "Fradkov, {Alexander L.} and Boris Andrievsky",
year = "2011",
month = dec,
doi = "10.1016/j.automatica.2011.09.004",
language = "Английский",
volume = "47",
pages = "2743--2748",
journal = "Automatica",
issn = "0005-1098",
publisher = "Elsevier",
number = "12",

}

RIS

TY - JOUR

T1 - Passification-based robust flight control design

AU - Fradkov, Alexander L.

AU - Andrievsky, Boris

PY - 2011/12

Y1 - 2011/12

N2 - A passification-based robust autopilot for attitude control of flexible aircraft under parametric uncertainty is designed. A high gain controller with forced sliding motions is used to secure good performance over a wide range of the aircraft model parameters. The shunting method is applied to ensure closed-loop system stability under lack of aircraft state information. The series reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The simulation results demonstrate the efficiency and high robustness of the suggested control system. (C) 2011 Elsevier Ltd. All rights reserved.

AB - A passification-based robust autopilot for attitude control of flexible aircraft under parametric uncertainty is designed. A high gain controller with forced sliding motions is used to secure good performance over a wide range of the aircraft model parameters. The shunting method is applied to ensure closed-loop system stability under lack of aircraft state information. The series reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The simulation results demonstrate the efficiency and high robustness of the suggested control system. (C) 2011 Elsevier Ltd. All rights reserved.

KW - Flight control

KW - Uncertain dynamic systems

KW - Shunt compensation

KW - Robustness

KW - Passification

KW - SIMPLE ADAPTIVE-CONTROL

KW - STABILIZATION

KW - PASSIVITY

U2 - 10.1016/j.automatica.2011.09.004

DO - 10.1016/j.automatica.2011.09.004

M3 - статья

VL - 47

SP - 2743

EP - 2748

JO - Automatica

JF - Automatica

SN - 0005-1098

IS - 12

ER -

ID: 5437050