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Title: Electro-Mechanical Control Loading System For Rotary Wing Aircraft Simulators
Authors: Aygün, Mehmet Murat
Taşcıoğlu, Yiğit
Genç, Gürsoy
Altunay, Mustafa
Issue Date: 2014
Publisher: Amer Soc Mechanical Engineers
Source: Aygün, 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.
Abstract: The 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.
ISBN: 978-0-7918-4585-1
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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