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ORCID: https://orcid.org/0000-0001-8773-7184, Ragab, Ahmed Refaat
ORCID: https://orcid.org/0000-0002-6897-6048, Luna Aguirre, Marco
ORCID: https://orcid.org/0000-0003-1036-7538, Ale Eshagh Khoeini, Mohammad Mehdi
ORCID: https://orcid.org/0000-0003-3936-332X and Campoy Cervera, Pascual
ORCID: https://orcid.org/0000-0002-9894-2009
(2023).
Thrust Vectoring Control for Heavy UAVs, Employing a Redundant Communication System.
"Sensors", v. 23
(n. 12);
p. 5561.
ISSN 1424-8220.
https://doi.org/10.3390/s23125561.
| Título: | Thrust Vectoring Control for Heavy UAVs, Employing a Redundant Communication System |
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| Autor/es: |
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| Tipo de Documento: | Artículo |
| Título de Revista/Publicación: | Sensors |
| Fecha: | 14 Junio 2023 |
| ISSN: | 1424-8220 |
| Volumen: | 23 |
| Número: | 12 |
| Materias: | |
| Palabras Clave Informales: | sommunication; thrust vectoring control; UAV; Algorithms; Communication; Sliding mode; Sports; Unmanned Aerial Devices |
| Escuela: | E.T.S.I. Industriales (UPM) |
| Departamento: | Automática, Ingeniería Eléctrica y Electrónica e Informática Industrial |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
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Recently, various research studies have been developed to address communication sensors for Unmanned Aerial Systems (UASs). In particular, when pondering control difficulties, communication is a crucial component. To this end, strengthening a control algorithm with redundant linking sensors ensures the overall system works accurately, even if some components fail. This paper proposes a novel approach to integrate several sensors and actuators for a heavy Unmanned Aerial Vehicle (UAV). Additionally, a cutting-edge Robust Thrust Vectoring Control (RTVC) technique is designed to control various communicative modules during a flying mission and converge the attitude system to stability. The results of the study demonstrate that even though RTVC is not frequently utilized, it works as well as cascade PID controllers, particularly for multi-rotors with mounted flaps, and could be perfectly functional in UAVs powered by thermal engines to increase the autonomy since the propellers cannot be used as controller surfaces.
| ID de Registro: | 85376 |
|---|---|
| Identificador DC: | https://oa.upm.es/85376/ |
| Identificador OAI: | oai:oa.upm.es:85376 |
| URL Portal Científico: | https://portalcientifico.upm.es/es/ipublic/item/10090240 |
| Identificador DOI: | 10.3390/s23125561 |
| URL Oficial: | https://www.mdpi.com/1424-8220/23/12/5561 |
| Depositado por: | iMarina Portal Científico |
| Depositado el: | 18 Dic 2024 11:57 |
| Ultima Modificación: | 18 Dic 2024 11:57 |
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