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Adaptive Self-Tuning Flight Control System for ATLANTE UAS.

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dc.contributor.authorViúdez Moreiras. Daniel
dc.contributor.authorMartín Sánchez, Juan
dc.date.accessioned2025-01-15T11:14:29Z
dc.date.available2025-01-15T11:14:29Z
dc.date.issued2016-09
dc.descriptionThe registered version of this article, first published in “Journal of Aerospace Engineering. 29(5). 10.1061/", is available online at the publisher's website: ASCE, https://doi.org/10.1061/(ASCE)AS.1943-5525.0000564
dc.descriptionLa versión registrada de este artículo, publicado por primera vez en “Journal of Aerospace Engineering. 29(5). 10.1061/", está disponible en línea en el sitio web del editor: ASCE, https://doi.org/10.1061/(ASCE)AS.1943-5525.0000564
dc.description.abstractThis paper presents an adaptive self-tuning flight control system (AST-FCS) for a fixed-wing aircraft, applied to a high-fidelity dynamic model of the ATLANTE unmanned aircraft system (UAS). This new adaptive control system is based on adaptive predictive (AP) control methodology and a new guidance system. AP control has been implemented in many complex industrial applications with excellent results, but it has not been applied in the aerospace sector yet. Experimental results obtained in simulation by flying a high-fidelity model of the ATLANTE UAS illustrate excellent control system performance and show the robustness of the AST-FCS, which has been designed without using accurate knowledge of the aircraft dynamics embedded within the model. It is expected that the application of AP control in this field could introduce significant advantages in aircraft control, improving performance in a wide variety of flight conditions and reducing design costs.en
dc.description.versionversión final
dc.identifier.citationiúdez-Moreiras, D. and Martín-Sánchez J.M. (2016) Adaptive Self-Tuning Flight Control System for ATLANTE UAS. Journal of Aerospace Engineering. 29(5). 10.1061/(ASCE)AS.1943-5525.0000564, 04016032. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000564
dc.identifier.doihttps://doi.org/10.1061/(ASCE)AS.1943-5525.0000564
dc.identifier.issn0893-1321 | eISSN 1943-5525
dc.identifier.urihttps://hdl.handle.net/20.500.14468/25306
dc.journal.issue5
dc.journal.titleJournal of Aerospace Engineering
dc.journal.volume29
dc.language.isoen
dc.publisherAmerican Society of Civil Engineers (ASCE)
dc.relation.centerFacultades y escuelas::E.T.S. de Ingenieros Industriales
dc.relation.departmentIngeniería Eléctrica, Electrónica, Control, Telemática y Química Aplicada a la Ingeniería
dc.rightsinfo:eu-repo/semantics/openAccess
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/deed.es
dc.subject33 Ciencias Tecnológicas::3306 Ingeniería y tecnología eléctricas
dc.titleAdaptive Self-Tuning Flight Control System for ATLANTE UAS.en
dc.typeartículoes
dc.typejournal articleen
dspace.entity.typePublication
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