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A New Pitch Angle Adaptive Control Design

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dc.contributor.authorViúdez Moreiras. Daniel
dc.contributor.authorMartín, Isaias
dc.contributor.authorMartín Sánchez, Juan M.
dc.coverage.spatialOrlando, FL, USA
dc.coverage.temporal2014-05-27
dc.date.accessioned2025-01-15T11:43:26Z
dc.date.available2025-01-15T11:43:26Z
dc.date.issued2014-06-26
dc.descriptionThe registered version, published in “2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Conference Proceedings", is available online at the publisher's website: https://doi.org/10.1109/ICUAS.2014.6842342
dc.description.abstractThis paper presents a new pitch angle adaptive control design based on the pitch rate following of a desired trajectory that ensures closed loop satisfactory performance. The pitch rate is under adaptive predictive (AP) control, as previously seen in the literature, but its desired trajectory is produced by a guidance block within a global guidance system structure that ensures automatic pitch angle closed loop performance. Additionally, the guidance block presented in this paper allows satisfactory operation of the automatic pilot in a range of high control frequencies suitable for this kind of application, overcoming stability problems that may arise within these high frequencies by direct application of a pitch angle AP controller. Experimental results obtained by flying a simulated aircraft illustrate comparatively the guidance system performance, and show the robustness of the new design with aerodynamic disturbances.en
dc.description.versionversión final
dc.identifier.citationViúdez-Moreiras, D., Martin, I., Martín-Sánchez J.M. (2014) “A New Pitch Angle Adaptive Control Design”. IEEE International Conference on Unmanned Aircraft Systems 2014, Orlando, Florida, USA, May 2014. pp. 928-935, ISBN: 978-1-4799-2376-2. https://doi.org/10.1109/ICUAS.2014.6842342
dc.identifier.doihttps://doi.org/10.1109/ICUAS.2014.6842342
dc.identifier.issn978-1-4799-2376-2
dc.identifier.urihttps://hdl.handle.net/20.500.14468/25310
dc.language.isoen
dc.publisherIEEE
dc.relation.centerFacultades y escuelas::E.T.S. de Ingenieros Industriales
dc.relation.congress2014 International Conference on Unmanned Aircraft Systems (ICUAS)
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-nc-nd/4.0/deed.es
dc.subject33 Ciencias Tecnológicas::3307 Tecnología electrónica
dc.subject.keywordsPitch Angle Controlen
dc.subject.keywordsOptimized Adaptive Controlen
dc.subject.keywordsAdaptive Predictive Controlen
dc.subject.keywordsDerivative Controlen
dc.subject.keywordsGuidance Systemen
dc.titleA New Pitch Angle Adaptive Control Designen
dc.typeactas de congresoes
dc.typeconference proceedingsen
dspace.entity.typePublication
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