Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/1560
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dc.contributor.authorAygün, Mehmet Murat-
dc.contributor.authorTaşcıoğlu, Yiğit-
dc.contributor.authorGenç, Gürsoy-
dc.contributor.authorAltunay, Mustafa-
dc.date.accessioned2019-06-26T08:07:06Z
dc.date.available2019-06-26T08:07:06Z
dc.date.issued2014
dc.identifier.citationAygün, M. M., Tascıoğlu, Y., Genç, G., & Altunay, M. (2014, July). Electro-Mechanical Control Loading System for Rotary Wing Aircraft Simulators. In ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis (pp. V003T15A019-V003T15A019). American Society of Mechanical Engineers.en_US
dc.identifier.isbn978-0-7918-4585-1
dc.identifier.urihttps://proceedings.asmedigitalcollection.asme.org/proceeding.aspx?articleid=1920179-
dc.identifier.urihttps://hdl.handle.net/20.500.11851/1560-
dc.description.abstractThe focus of this paper is on the development of a high-fidelity electro-mechanical Control Loading System (CLS) for a rotary wing aircraft simulator. CLS is one of the major components of a flight simulator. It is used for providing realistic force feedback to pilots. The pilot in a real aircraft feels the forces acting on control surfaces through cockpit controls. During simulation, these forces are produced by CLS actuators. For this reason, CLS must behave exactly like the aircraft control hardware, statically and dynamically. The fidelity of the force feel simulation is a key criterion for flight simulation certification. It is also important that a CLS design is reconfigurable and modular such that it conforms easily to different simulator models and simulations of different aircrafts. The work also includes system integration of a research simulator for testing purposes. Design and selection of hardware and software components of the CLS and the simulator are presented along with the overall system architecture.en_US
dc.language.isoenen_US
dc.publisherAmer Soc Mechanical Engineersen_US
dc.relation.ispartofProceedings Of The ASME 12Th Biennial Conference On Engineering Systems Design And Analysis - 2014, Vol 3en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleElectro-Mechanical Control Loading System For Rotary Wing Aircraft Simulatorsen_US
dc.typeConference Objecten_US
dc.departmentFaculties, Faculty of Engineering, Department of Mechanical Engineeringen_US
dc.departmentFakülteler, Mühendislik Fakültesi, Makine Mühendisliği Bölümütr_TR
dc.authorid0000-0002-3000-7057-
dc.identifier.wosWOS:000361407000074en_US
dc.identifier.scopus2-s2.0-84916898400en_US
dc.institutionauthorTaşcıoğlu, Yiğit-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairetypeConference Object-
item.cerifentitytypePublications-
item.languageiso639-1en-
crisitem.author.dept02.7. Department of Mechanical Engineering-
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection
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