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ORCID: https://orcid.org/0000-0001-5605-919X, Bardera Mora, Rafael
ORCID: https://orcid.org/0000-0002-5157-9935, Rodríguez Sevillano, Ángel Antonio
ORCID: https://orcid.org/0000-0003-0685-3875 and Cobo González, Álvaro
ORCID: https://orcid.org/0000-0003-3567-0269
(2023).
Performance enhancement of a bioinspired micro air vehicle by integrating a smart composite in its morphing wing.
"Composite Structures", v. 311
;
p. 116794.
ISSN 02638223.
https://doi.org/10.1016/j.compstruct.2023.116794.
| Título: | Performance enhancement of a bioinspired micro air vehicle by integrating a smart composite in its morphing wing |
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| Autor/es: |
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| Tipo de Documento: | Artículo |
| Título de Revista/Publicación: | Composite Structures |
| Fecha: | 1 Mayo 2023 |
| ISSN: | 02638223 |
| Volumen: | 311 |
| Materias: | |
| ODS: | |
| Palabras Clave Informales: | ACTUATION; design; Finite element method; Micro air vehicle; Morphing; Optimization; piezoelectric; Fiber; Finite Element Method; Macro fiber composite; micro air vehicle; Morphing; Piezoelectric |
| Escuela: | E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM) |
| Departamento: | Sistemas Aeroespaciales, Transporte Aéreo y Aeropuertos |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
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The purpose of this paper is to show the advantages of using a smart composite in a micro air vehicle (MAV) equipped with morphing wing technology. A Macro Fiber Composite (MFC) actuator is attached to the wing's bottom surface to modify the wing camber during the mission. This material allows the MAV to be optimized according to each flight, thus making it more versatile and attractive to the market. The elongation of the lower surface when a positive voltage is applied to the actuator is translated to an increment in camber, which results in an increment in the maximum lift coefficient, thus enabling the vehicle to fly slower to adapt to any payload. Besides, a reduction in camber results in an increase in aerodynamic efficiency, which improves range and endurance. Several tests of the MAV at prototype level have been carried out at INTA, so as to demonstrate the feasibility of implementing MFC actuators to control and manoeuvre these vehicles. The use of this material in aerospace industry opens up various fields of research in aerospace engineering, such as new features in flight mechanics and aerodynamic performance and new strategies in the design of flight stability and control laws.
| ID de Registro: | 80971 |
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| Identificador DC: | https://oa.upm.es/80971/ |
| Identificador OAI: | oai:oa.upm.es:80971 |
| URL Portal Científico: | https://portalcientifico.upm.es/es/ipublic/item/10023027 |
| Identificador DOI: | 10.1016/j.compstruct.2023.116794 |
| URL Oficial: | https://www.sciencedirect.com/science/article/pii/... |
| Depositado por: | Portal Científico UPM |
| Depositado el: | 08 Abr 2024 08:52 |
| Ultima Modificación: | 06 Feb 2025 16:44 |
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