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Calibration of a 3-Component External Balance for MAVs Wind Tunnel Research
Cita
Bardera Mora, Rafael 
ORCID: https://orcid.org/0000-0002-5157-9935, Rodríguez Sevillano, Ángel Antonio ORCID: https://orcid.org/0000-0003-0685-3875, Barroso Barderas, Estela ORCID: https://orcid.org/0000-0001-6694-3990, Sor, Suthyvann ORCID: https://orcid.org/0000-0002-6972-8601 and Matías García, Juan Carlos ORCID: https://orcid.org/0000-0001-6049-6421
(2024).
Calibration of a 3-Component External Balance for MAVs Wind Tunnel Research.
"Applied Sciences", v. 14
;
ISSN 20763417.
https://doi.org/10.3390/app142311236.
ORCID: https://orcid.org/0000-0002-5157-9935, Rodríguez Sevillano, Ángel Antonio ORCID: https://orcid.org/0000-0003-0685-3875, Barroso Barderas, Estela ORCID: https://orcid.org/0000-0001-6694-3990, Sor, Suthyvann ORCID: https://orcid.org/0000-0002-6972-8601 and Matías García, Juan Carlos ORCID: https://orcid.org/0000-0001-6049-6421
(2024).
Calibration of a 3-Component External Balance for MAVs Wind Tunnel Research.
"Applied Sciences", v. 14
;
ISSN 20763417.
https://doi.org/10.3390/app142311236.
Descripción
| Título: | Calibration of a 3-Component External Balance for MAVs Wind Tunnel Research |
|---|---|
| Autor/es: |
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| Tipo de Documento: | Artículo |
| Título de Revista/Publicación: | Applied Sciences |
| Fecha: | 1 Diciembre 2024 |
| ISSN: | 20763417 |
| Volumen: | 14 |
| Materias: | |
| ODS: | |
| Palabras Clave Informales: | Calibration; external balance; Measuremen |
| Escuela: | E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM) |
| Departamento: | Aeronaves y Vehículos Espaciales |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
Resumen
This paper presents a 3-component external balance, specifically designed, built, and calibrated at the National Institute for Aerospace Technology (INTA) for measuring aerodynamic forces on Micro Aerial Vehicles in the wind tunnel. The balance employs high-precision strain gauge cells as its load-sensing elements, strategically positioned in a metallic structure to measure lift force, aerodynamic drag force, and pitching moment. The entire calibration process of the balance, including the mathematical formulation to derive the calibration matrix and the calibration bench designed and manufactured for this purpose, is detailed in this paper. Moreover, the complete analysis of component interferences of the aerodynamic components and an assessment of the uncertainties inherent in the system are presented.
Más información
| ID de Registro: | 88923 |
|---|---|
| Identificador DC: | https://oa.upm.es/88923/ |
| Identificador OAI: | oai:oa.upm.es:88923 |
| URL Portal Científico: | https://portalcientifico.upm.es/es/ipublic/item/10306866 |
| Identificador DOI: | 10.3390/app142311236 |
| URL Oficial: | https://www.mdpi.com/2076-3417/14/23/11236 |
| Depositado por: | iMarina Portal Científico |
| Depositado el: | 07 May 2025 09:21 |
| Ultima Modificación: | 07 May 2025 09:21 |
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