Fine-Tuning of Feedback Gain Control for Hover Quad Copter Rotors by Stochastic Optimization Methods

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dc.authoridKavuran, Gurkan/0000-0003-2651-5005
dc.authoridAlagoz, Baris Baykant/0000-0001-5238-6433
dc.authoridATES, Abdullah/0000-0002-4236-6794
dc.authoridYeroglu, Celaleddin/0000-0002-6106-2374
dc.authorwosidYeroglu, Celaleddin/ABG-9572-2020
dc.authorwosidKavuran, Gurkan/S-6935-2016
dc.authorwosidAlagoz, Baris Baykant/ABG-8526-2020
dc.authorwosidATES, Abdullah/V-6929-2018
dc.contributor.authorAtes, Abdullah
dc.contributor.authorAlagoz, Baris Baykant
dc.contributor.authorKavuran, Gurkan
dc.contributor.authorYeroglu, Celaleddin
dc.date.accessioned2024-08-04T20:47:07Z
dc.date.available2024-08-04T20:47:07Z
dc.date.issued2020
dc.departmentİnönü Üniversitesien_US
dc.description.abstractThree degree of freedom (3 DOF) Hover Quad Copter (HQC) platforms are implemented for various missions in diverse scales from the micro to macro platforms. As HQC platforms scale down, micro platform requires rather robust and effective control techniques. This study investigates applicability of some stochastic optimization methods for tuning feedback gain control of HQC rotors and compares optimization results with results of linear quadratic regulator (LQR) method that has been widely used analytical method for optimal feedback gain control of HQCs. This study considers the utilization of two stochastic methods for tuning of HQCs. These methods are stochastic multi-parameter divergence optimization method (SMDO) and discrete stochastic optimization method (DSO). These methods are employed to optimize feedback gain coefficients of an experimental HQC test platform. Simulation and experimental results of SMDO and DSO methods are reported and compared with results of LQR method.en_US
dc.identifier.doi10.1007/s40998-020-00323-7
dc.identifier.endpage1672en_US
dc.identifier.issn2228-6179
dc.identifier.issn2364-1827
dc.identifier.issue4en_US
dc.identifier.scopus2-s2.0-85079175348en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage1663en_US
dc.identifier.urihttps://doi.org/10.1007/s40998-020-00323-7
dc.identifier.urihttps://hdl.handle.net/11616/99175
dc.identifier.volume44en_US
dc.identifier.wosWOS:000515932000002en_US
dc.identifier.wosqualityQ4en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSpringer International Publishing Agen_US
dc.relation.ispartofIranian Journal of Science and Technology-Transactions of Electrical Engineeringen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectQuad coptersen_US
dc.subjectStochastic optimizationen_US
dc.subjectController tuningen_US
dc.subjectFine-tuningen_US
dc.subjectFlight controlen_US
dc.titleFine-Tuning of Feedback Gain Control for Hover Quad Copter Rotors by Stochastic Optimization Methodsen_US
dc.typeArticleen_US

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