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...
| Main Authors: | , , , , , , |
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2016-12-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/ursu__ion-guta__enciu__toader__dan__donciu__turcan.pdf |
| _version_ | 1818130373799837696 |
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| author | Ioan URSU Dragos Daniel ION GUTA Daniela ENCIU Adrian TOADER Mircea DAN1 Cristiana DONCIU Vasile TURCAN |
| author_facet | Ioan URSU Dragos Daniel ION GUTA Daniela ENCIU Adrian TOADER Mircea DAN1 Cristiana DONCIU Vasile TURCAN |
| author_sort | Ioan URSU |
| collection | DOAJ |
| 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. |
| first_indexed | 2024-12-11T08:04:01Z |
| format | Article |
| id | doaj.art-3c02cf8c4e154066aa0f87308613ba2e |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-12-11T08:04:01Z |
| publishDate | 2016-12-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-3c02cf8c4e154066aa0f87308613ba2e2022-12-22T01:15:03ZengNational 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 |
| 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 |
| title | 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_short | Mathematical modeling of a V-stack piezoelectric aileron actuation |
| title_sort | mathematical modeling of a v stack piezoelectric aileron actuation |
| 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 |
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