State dependent regional pole assignment controller design for a 3-DOF helicopter model

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dc.contributor.authorArıcan, Ahmet Çağrı
dc.contributor.authorÇopur, Engin Hasan
dc.contributor.authorInalhan, Gokhan
dc.contributor.authorSalamci, Metin U.
dc.date.accessioned2023-08-23T08:12:07Z
dc.date.available2023-08-23T08:12:07Z
dc.date.issued2023-06-26
dc.description.abstractFor linear systems, a state feedback control law can be easily designed to keep all closed-loop poles inside a specified disk since the locations of the poles are unique. However, its application to nonlinear systems is not so simple. Therefore, this paper introduces a new pole placement method, named as State Dependent Regional Pole Assignment, for nonlinear systems. This proposed method produces a state dependent feedback control law, enabling the eigenvalues of the closed-loop matrix to be placed in a specified disk to achieve the desired control performance characteristics. The effectiveness of the method is tested on the 3 DOF Helicopter experimental setup. To verify its effectiveness, the experimental results of the nonlinear method are compared with those of the linear method.en_UK
dc.identifier.citationArıcan AC, Çopur EH, Inalhan G, Salamci MU. (2023) State dependent regional pole assignment controller design for a 3-DOF helicopter model. In: 2023 International Conference on Unmanned Aircraft Systems (ICUAS), 6-9 June 2023, Warsaw, Polanden_UK
dc.identifier.eisbn979-8-3503-1037-5
dc.identifier.eissn2575-7296
dc.identifier.isbn979-8-3503-1038-2
dc.identifier.issn2373-6720
dc.identifier.urihttps://doi.org/10.1109/ICUAS57906.2023.10155816
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20127
dc.language.isoenen_UK
dc.publisherIEEEen_UK
dc.rightsAttribution-NonCommercial 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/*
dc.titleState dependent regional pole assignment controller design for a 3-DOF helicopter modelen_UK
dc.typeConference paperen_UK

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