Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators

A smart-skin antenna structure is investigated for active flutter control with piezoelectric sensors and actuators. The skin antenna is designed as a multilayer sandwich structure with a dielectric polymer to perform the role of antenna or radar structures. The governing equations are developed acco...

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Main Authors: Chang-Yull Lee, Ji-Hwan Kim
Format: Article
Language:English
Published: MDPI AG 2021-09-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/8/9/257
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spelling doaj-5a50697ee28c4bdc99c9e0543ce9ef612021-09-25T23:33:19ZengMDPI AGAerospace2226-43102021-09-01825725710.3390/aerospace8090257Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and ActuatorsChang-Yull Lee0Ji-Hwan Kim1Department of Aerospace Engineering, Inha University, Incheon 22212, KoreaDepartment of Aerospace Engineering, Institute of Advanced Aerospace Technology, Seoul National University, Seoul 08826, KoreaA smart-skin antenna structure is investigated for active flutter control with piezoelectric sensors and actuators. The skin antenna is designed as a multilayer sandwich structure with a dielectric polymer to perform the role of antenna or radar structures. The governing equations are developed according to the first-order shear deformation theory, and von Karman strain–displacement relationships are used for the moderate geometrical nonlinearity. To consider the supersonic airflow, first-order piston theory is performed for the aerodynamic pressures. The linear quadratic regulator (LQR) method is applied as a control algorithm, and Newmark’s method is studied to obtain the numerical results. In the present study, the effects of placements and shape of piezoelectric patches are discussed on the flutter control of the model in detail. In addition, the numerical results show that the skin antenna model can effectively suppress the panel flutter behaviors of the model, optimal conditions of piezoelectric patches are obtained for skin antenna structures.https://www.mdpi.com/2226-4310/8/9/257smart-skin antenna structureactive flutter controlLQR control algorithmpiezoelectric sensor and actuator
collection DOAJ
language English
format Article
sources DOAJ
author Chang-Yull Lee
Ji-Hwan Kim
spellingShingle Chang-Yull Lee
Ji-Hwan Kim
Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
Aerospace
smart-skin antenna structure
active flutter control
LQR control algorithm
piezoelectric sensor and actuator
author_facet Chang-Yull Lee
Ji-Hwan Kim
author_sort Chang-Yull Lee
title Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
title_short Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
title_full Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
title_fullStr Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
title_full_unstemmed Active Flutter Suppression of Smart-Skin Antenna Structures with Piezoelectric Sensors and Actuators
title_sort active flutter suppression of smart-skin antenna structures with piezoelectric sensors and actuators
publisher MDPI AG
series Aerospace
issn 2226-4310
publishDate 2021-09-01
description A smart-skin antenna structure is investigated for active flutter control with piezoelectric sensors and actuators. The skin antenna is designed as a multilayer sandwich structure with a dielectric polymer to perform the role of antenna or radar structures. The governing equations are developed according to the first-order shear deformation theory, and von Karman strain–displacement relationships are used for the moderate geometrical nonlinearity. To consider the supersonic airflow, first-order piston theory is performed for the aerodynamic pressures. The linear quadratic regulator (LQR) method is applied as a control algorithm, and Newmark’s method is studied to obtain the numerical results. In the present study, the effects of placements and shape of piezoelectric patches are discussed on the flutter control of the model in detail. In addition, the numerical results show that the skin antenna model can effectively suppress the panel flutter behaviors of the model, optimal conditions of piezoelectric patches are obtained for skin antenna structures.
topic smart-skin antenna structure
active flutter control
LQR control algorithm
piezoelectric sensor and actuator
url https://www.mdpi.com/2226-4310/8/9/257
work_keys_str_mv AT changyulllee activefluttersuppressionofsmartskinantennastructureswithpiezoelectricsensorsandactuators
AT jihwankim activefluttersuppressionofsmartskinantennastructureswithpiezoelectricsensorsandactuators
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