Adaptive Control of a 3 DoF Helicopter with Linear and Nonlinear Reference Models

Basit Öğe Kaydı
dc.contributor.authorKocagil, Bedrettin Mahmut
dc.contributor.authorOzcan, Sinan
dc.contributor.authorArican, Ahmet Cagri
dc.contributor.authorGuzey, Umit Mufit
dc.contributor.authorCopur, Engin Hasan
dc.contributor.authorSalamci, Metin U.
dc.date.accessioned2024-02-23T14:45:20Z
dc.date.available2024-02-23T14:45:20Z
dc.date.issued2018
dc.departmentNEÜen_US
dc.description6th International Conference on Control Engineering and Information Technology (CEIT) -- OCT 25-27, 2018 -- Istanbul, TURKEYen_US
dc.description.abstractAdaptive control methods are widely used for the control of both linear and nonlinear dynamical systems. Among the adaptive control approaches, Model Reference Adaptive Control (MRAC) method has a systematic design feature in which response of a stable reference model is targeted to be followed by the dynamical system. In general, Linear Time Invariant (LTI) Reference Models are considered in the MRAC design and the adaptation rule is formulated accordingly. In this paper, the linear reference model is altered with a stable nonlinear one and the adaptation rule is re-formulated to cope with the nonlinearity. The stable nonlinear reference model is generated by using the State Dependent Riccati Equation (SDRE) approach and the adaptation rule is also updated by using the same SDRE idea. The effects of altering the linear reference model to the nonlinear counterpart are shown in the MRAC formulations. In addition to the new MRAC formulations, the proposed MRAC algorithm is applied to a 3 DoF helicopter test bed to reveal the advantages of the nonlinear reference model.en_US
dc.description.sponsorshipYildiz Tech Univen_US
dc.description.sponsorshipTUSAS-Turkish Aerospace Industries (TAI) [DKTM/2015/07]en_US
dc.description.sponsorshipThis work is supported by the TUSAS-Turkish Aerospace Industries (TAI) under the Project No: DKTM/2015/07.en_US
dc.identifier.isbn978-1-5386-7641-7
dc.identifier.scopus2-s2.0-85069178259en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12452/17365
dc.identifier.wosWOS:000491282100056en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherIEEEen_US
dc.relation.ispartof2018 6th International Conference On Control Engineering & Information Technology (Ceit)en_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectMracen_US
dc.subjectSdreen_US
dc.subjectNonlinear Systemsen_US
dc.subjectReal Time Controlen_US
dc.subject3 Dof Helicopteren_US
dc.titleAdaptive Control of a 3 DoF Helicopter with Linear and Nonlinear Reference Modelsen_US
dc.typeConference Objecten_US

Dosyalar

Koleksiyon

WoS İndeksli Yayınlar Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu