Mathematical modeling of a V-stack piezoelectric aileron actuation

The article presents a mathematical modeling of aileron actuation that uses piezo V-shaped stacks. The aim of the actuation is the increasing of flutter speed in the context of a control law, in order to widen the flight envelope. In this way the main advantage of such a piezo actuator, the bandwidt...

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Main Authors:	Ioan URSU, Dragos Daniel ION GUTA, Daniela ENCIU, Adrian TOADER, Mircea DAN1, Cristiana DONCIU, Vasile TURCAN
Format:	Article
Language:	English
Published:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2016-12-01
Series:	INCAS Bulletin
Subjects:	piezoelectric stack actuators flutter counteracting kinematic scheme mathematical modeling numerical simulations
Online Access:	http://bulletin.incas.ro/files/ursu__ion-guta__enciu__toader__dan__donciu__turcan.pdf

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spelling	doaj-3c02cf8c4e154066aa0f87308613ba2e2020-11-24T23:41:22ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282016-12-018414115510.13111/2066-8201.2016.8.4.12Mathematical modeling of a V-stack piezoelectric aileron actuationIoan URSU0Dragos Daniel ION GUTA1Daniela ENCIU2Adrian TOADER3Mircea DAN14Cristiana DONCIU5Vasile TURCAN6INCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, ursu.ioan@incas.ro*INCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, guta.dragos@incas.roINCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, enciu.daniela@incas.roINCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, toader.adrian@incas.roINCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, dan.mircea@incas.roINCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania,donciu.cristina@incas.roINCAS ‒ National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, RomaniaThe article presents a mathematical modeling of aileron actuation that uses piezo V-shaped stacks. The aim of the actuation is the increasing of flutter speed in the context of a control law, in order to widen the flight envelope. In this way the main advantage of such a piezo actuator, the bandwidth is exploited. The mathematical model is obtained based on free body diagrams, and the numerical simulations allow a preliminary sizing of the actuator.http://bulletin.incas.ro/files/ursu__ion-guta__enciu__toader__dan__donciu__turcan.pdfpiezoelectric stack actuatorsflutter counteractingkinematic schememathematical modelingnumerical simulations
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	Ioan URSU Dragos Daniel ION GUTA Daniela ENCIU Adrian TOADER Mircea DAN1 Cristiana DONCIU Vasile TURCAN
spellingShingle	Ioan URSU Dragos Daniel ION GUTA Daniela ENCIU Adrian TOADER Mircea DAN1 Cristiana DONCIU Vasile TURCAN Mathematical modeling of a V-stack piezoelectric aileron actuation INCAS Bulletin piezoelectric stack actuators flutter counteracting kinematic scheme mathematical modeling numerical simulations
author_facet	Ioan URSU Dragos Daniel ION GUTA Daniela ENCIU Adrian TOADER Mircea DAN1 Cristiana DONCIU Vasile TURCAN
author_sort	Ioan URSU
title	Mathematical modeling of a V-stack piezoelectric aileron actuation
title_short	Mathematical modeling of a V-stack piezoelectric aileron actuation
title_full	Mathematical modeling of a V-stack piezoelectric aileron actuation
title_fullStr	Mathematical modeling of a V-stack piezoelectric aileron actuation
title_full_unstemmed	Mathematical modeling of a V-stack piezoelectric aileron actuation
title_sort	mathematical modeling of a v-stack piezoelectric aileron actuation
publisher	National Institute for Aerospace Research “Elie Carafoli” - INCAS
series	INCAS Bulletin
issn	2066-8201 2247-4528
publishDate	2016-12-01
description	The article presents a mathematical modeling of aileron actuation that uses piezo V-shaped stacks. The aim of the actuation is the increasing of flutter speed in the context of a control law, in order to widen the flight envelope. In this way the main advantage of such a piezo actuator, the bandwidth is exploited. The mathematical model is obtained based on free body diagrams, and the numerical simulations allow a preliminary sizing of the actuator.
topic	piezoelectric stack actuators flutter counteracting kinematic scheme mathematical modeling numerical simulations
url	http://bulletin.incas.ro/files/ursu__ion-guta__enciu__toader__dan__donciu__turcan.pdf
work_keys_str_mv	AT ioanursu mathematicalmodelingofavstackpiezoelectricaileronactuation AT dragosdanielionguta mathematicalmodelingofavstackpiezoelectricaileronactuation AT danielaenciu mathematicalmodelingofavstackpiezoelectricaileronactuation AT adriantoader mathematicalmodelingofavstackpiezoelectricaileronactuation AT mirceadan1 mathematicalmodelingofavstackpiezoelectricaileronactuation AT cristianadonciu mathematicalmodelingofavstackpiezoelectricaileronactuation AT vasileturcan mathematicalmodelingofavstackpiezoelectricaileronactuation
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Mathematical modeling of a V-stack piezoelectric aileron actuation

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