Multiloop State-Dependent Nonlinear Time-Varying Sliding Mode Control of Unmanned Small-Scale Helicopter

dc.authoridSalamci, Metin Uymaz/0000-0002-6150-8014
dc.authorscopusid55846118800
dc.authorscopusid6506327033
dc.authorscopusid6506329918
dc.authorwosidSalamci, Metin Uymaz/AAB-5826-2021
dc.contributor.authorOzcan, Sinan
dc.contributor.authorSalamci, Metin U.
dc.contributor.authorNalbantoglu, Volkan
dc.contributor.otherAirframe and Powerplant Maintenance
dc.date.accessioned2024-07-05T15:40:15Z
dc.date.available2024-07-05T15:40:15Z
dc.date.issued2020
dc.departmentAtılım Universityen_US
dc.department-temp[Ozcan, Sinan] Turkish Aerosp Ind, Helicopter Div, TR-06980 Ankara, Turkey; [Salamci, Metin U.] Gazi Univ, Dept Mech Engn, Ankara, Turkey; [Nalbantoglu, Volkan] Atilim Univ, Sch Civil Aviat, Ankara, Turkeyen_US
dc.descriptionSalamci, Metin Uymaz/0000-0002-6150-8014en_US
dc.description.abstractTime delays, parameter uncertainties, and disturbances are the fundamental problems that hinder the stability and reduce dramatically the tracking performance of dynamical systems. In this paper, a new state-dependent nonlinear time-varying sliding mode control autopilot structure is proposed to cope with these dynamical and environmental complexities for an unmanned helicopter. The presented technique is based on freezing the nonlinear system equations on each time step and designing a controller using the frozen system model at this time step. The proposed method offers an improved performance in the presence of major disturbances and parameter uncertainties by adapting itself to possible dynamical varieties without a need of trimming the system on different operating conditions. Unlike the existing linear cascade autopilot structure, this study also proposes a nonlinear cascade state-dependent coefficient helicopter autopilot structure consisting of four separate nonlinear sub-systems. The proposed method is tested through the real time and PC-based simulations. To show the performance of the proposed robust method, it is also bench-marked against a linear sliding control control in PC-based simulations.en_US
dc.description.sponsorshipTurkish Aerospace Industries, Inc. (TAI) [DKTM/2015/07]en_US
dc.description.sponsorshipThe author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by the Turkish Aerospace Industries, Inc. (TAI) under project no: DKTM/2015/07.en_US
dc.identifier.citationcount4
dc.identifier.doi10.1177/0954410019872116
dc.identifier.endpage606en_US
dc.identifier.issn0954-4100
dc.identifier.issn2041-3025
dc.identifier.issue3en_US
dc.identifier.scopus2-s2.0-85073801877
dc.identifier.startpage585en_US
dc.identifier.urihttps://doi.org/10.1177/0954410019872116
dc.identifier.urihttps://hdl.handle.net/20.500.14411/3321
dc.identifier.volume234en_US
dc.identifier.wosWOS:000485274800001
dc.identifier.wosqualityQ4
dc.institutionauthorNalbantoğlu, Volkan
dc.language.isoenen_US
dc.publisherSage Publications Ltden_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.scopus.citedbyCount4
dc.subjectSliding mode controlen_US
dc.subjectstate-dependent Riccati equationen_US
dc.subjectflight controlen_US
dc.subjectflight dynamicsen_US
dc.subjectnonlinear controlen_US
dc.titleMultiloop State-Dependent Nonlinear Time-Varying Sliding Mode Control of Unmanned Small-Scale Helicopteren_US
dc.typeArticleen_US
dc.wos.citedbyCount4
dspace.entity.typePublication
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