Relative Estimation and Control for Loyal Wingman MUM-T

This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). This article belongs to the Special Issue Advances in UAV Technology: Dynamics, Guidance, Navigation, and Control of T...

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Autores: Martín Sánchez, Jesús, Esteban Roncero, Sergio
Tipo de recurso: artículo
Estado:Versión publicada
Fecha de publicación:2025
País:España
Institución:Universidad de Sevilla (US)
Repositorio:idUS. Depósito de Investigación de la Universidad de Sevilla
OAI Identifier:oai:idus.us.es:11441/176339
Acceso en línea:https://hdl.handle.net/11441/176339
https://doi.org/10.3390/aerospace12080680
Access Level:acceso abierto
Palabra clave:Swarming
UAVs
Formation flight
Manned-unmanned teaming
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spelling Relative Estimation and Control for Loyal Wingman MUM-TMartín Sánchez, JesúsEsteban Roncero, SergioSwarmingUAVsFormation flightManned-unmanned teamingThis article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). This article belongs to the Special Issue Advances in UAV Technology: Dynamics, Guidance, Navigation, and Control of Transformative Aerial Vehicles.The gradual integration of Manned–Unmanned Teaming (MUM-T) is gaining increasing significance. An intriguing feature is the ability to do relative estimation solely through the use of the INS/GPS system. However, in certain environments, such as GNSS-denied areas, this method may lack the necessary accuracy and reliability to successfully execute autonomous formation flight. In order to achieve autonomous formation flight, we are conducting an initial investigation into the development of a relative estimator and control laws for MUM-T. Our proposal involves the use of a quaternion-based relative state estimator to combine GPS and INS sensor data from each UAV with vision pose estimation of the remote carrier obtained from the fighter. The technique has been validated through simulated findings, which paved the way for the experiments explained in the paper.Multidisciplinary Digital Publishing Institute (MDPI)Ingeniería Aeroespacial y Mecánica de FluidosTEP945: Ingeniería Aeroespacial2025info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfapplication/pdfhttps://hdl.handle.net/11441/176339https://doi.org/10.3390/aerospace12080680reponame:idUS. Depósito de Investigación de la Universidad de Sevillainstname:Universidad de Sevilla (US)InglésAerospace, 12 (8), 680.https://www.mdpi.com/2226-4310/12/8/680info:eu-repo/semantics/openAccessoai:idus.us.es:11441/1763392026-06-17T12:51:07Z
dc.title.none.fl_str_mv Relative Estimation and Control for Loyal Wingman MUM-T
title Relative Estimation and Control for Loyal Wingman MUM-T
spellingShingle Relative Estimation and Control for Loyal Wingman MUM-T
Martín Sánchez, Jesús
Swarming
UAVs
Formation flight
Manned-unmanned teaming
title_short Relative Estimation and Control for Loyal Wingman MUM-T
title_full Relative Estimation and Control for Loyal Wingman MUM-T
title_fullStr Relative Estimation and Control for Loyal Wingman MUM-T
title_full_unstemmed Relative Estimation and Control for Loyal Wingman MUM-T
title_sort Relative Estimation and Control for Loyal Wingman MUM-T
dc.creator.none.fl_str_mv Martín Sánchez, Jesús
Esteban Roncero, Sergio
author Martín Sánchez, Jesús
author_facet Martín Sánchez, Jesús
Esteban Roncero, Sergio
author_role author
author2 Esteban Roncero, Sergio
author2_role author
dc.contributor.none.fl_str_mv Ingeniería Aeroespacial y Mecánica de Fluidos
TEP945: Ingeniería Aeroespacial
dc.subject.none.fl_str_mv Swarming
UAVs
Formation flight
Manned-unmanned teaming
topic Swarming
UAVs
Formation flight
Manned-unmanned teaming
description This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). This article belongs to the Special Issue Advances in UAV Technology: Dynamics, Guidance, Navigation, and Control of Transformative Aerial Vehicles.
publishDate 2025
dc.date.none.fl_str_mv 2025
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.none.fl_str_mv https://hdl.handle.net/11441/176339
https://doi.org/10.3390/aerospace12080680
url https://hdl.handle.net/11441/176339
https://doi.org/10.3390/aerospace12080680
dc.language.none.fl_str_mv Inglés
language_invalid_str_mv Inglés
dc.relation.none.fl_str_mv Aerospace, 12 (8), 680.
https://www.mdpi.com/2226-4310/12/8/680
dc.rights.none.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
application/pdf
dc.publisher.none.fl_str_mv Multidisciplinary Digital Publishing Institute (MDPI)
publisher.none.fl_str_mv Multidisciplinary Digital Publishing Institute (MDPI)
dc.source.none.fl_str_mv reponame:idUS. Depósito de Investigación de la Universidad de Sevilla
instname:Universidad de Sevilla (US)
instname_str Universidad de Sevilla (US)
reponame_str idUS. Depósito de Investigación de la Universidad de Sevilla
collection idUS. Depósito de Investigación de la Universidad de Sevilla
repository.name.fl_str_mv
repository.mail.fl_str_mv
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score 15,812455

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