Model identification adaptive control - implementation case studies for a high manoeuvrability aircraft

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dc.contributor.authorÖreg, Zsombor
dc.contributor.authorShin, Hyosang
dc.contributor.authorTsourdos, Antonios
dc.date.accessioned2019-12-18T15:58:52Z
dc.date.available2019-12-18T15:58:52Z
dc.date.issued2019-08-15
dc.description.abstractWith the proliferation of modular Unmanned Aerial Vehicles (UAVs) cheap and scalable control methods are needed to ensure operability. Using adaptive control it seems that these requirements could be met. In this paper applicability of parameter adaptation and control methods are demonstrated within the model identification adaptive control framework, implementing several methods and evaluating their performance. As a plant a non-linear simulation model of an F-16 aircraft is used.en_UK
dc.identifier.citationOreg Z, Shin H-Y, Tsourdos A. (2019) Model identification adaptive control - implementation case studies for a high manoeuvrability aircraft. In: 27th Mediterranean Conference on Control and Automation, 1-4 July 2019, Akko, Israelen_UK
dc.identifier.isbn978-1-7281-2804-7
dc.identifier.urihttps://doi.org/10.1109/MED.2019.8798513
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/14867
dc.language.isoenen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution-NonCommercial 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/*
dc.subjectWireless fidelityen_UK
dc.subject3GPPen_UK
dc.subjectChannel allocationen_UK
dc.subjectComputer architectureen_UK
dc.subject5G mobile communicationen_UK
dc.subjectPrivacyen_UK
dc.titleModel identification adaptive control - implementation case studies for a high manoeuvrability aircraften_UK
dc.typeConference paperen_UK

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