Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-27217
Full metadata record
DC FieldValueLanguage
dc.contributor.authorCapone, Pierluigi-
dc.contributor.authorPrimatesta, Stefano-
dc.contributor.authorBarra, Federico-
dc.contributor.authorGuglieri, Giorgio-
dc.date.accessioned2023-03-07T16:34:40Z-
dc.date.available2023-03-07T16:34:40Z-
dc.date.issued2022-05-10-
dc.identifier.issn1552-2938de_CH
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/27217-
dc.description.abstractThis paper introduces a tilt-rotor flight simulation platform for research and teaching purposes implementing a real-time simulation of the Bell XV-15 aircraft. The mathematical model of the XV-15 aircraft has been implemented including simplified models for the aerodynamics of the whole aircraft, rotors, and engine dynamics. Hence, the simulation is performed in a graphic environment to reproduce the simulated flight and to interact with it using commands given by the pilot. The simulation platform is implemented using MATLAB/Simulink®, while the input commands are set using USB peripherals, i.e., a flight stick and a pedal board. Instead, the visualization environment is performed using FlightGear, an open-source and cross-platform software that is widely used in research. The result is a portable tilt-rotor simulator to be executed on a commercial pc, while ensuring real-time performance. The tilt-rotor flight simulator is also validated by a licensed helicopter pilot returning positive feedback regarding the flight experience.de_CH
dc.language.isoende_CH
dc.publisherVertical Flight Societyde_CH
dc.rightsLicence according to publishing contractde_CH
dc.subjectReal-time simulationde_CH
dc.subjectTilt-rotorde_CH
dc.subject.ddc629: Luftfahrt- und Fahrzeugtechnikde_CH
dc.titleDesign and integration of a tilt-rotor flight simulation platformde_CH
dc.typeKonferenz: Paperde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
zhaw.publisher.placeFairfax, VAde_CH
dc.identifier.doi10.4050/F-0078-2022-17587de_CH
dc.identifier.doi10.21256/zhaw-27217-
zhaw.conference.details78th Annual Forum and Technology Display, Fort Worth, Texas, 10-12 May 2022de_CH
zhaw.funding.euNode_CH
zhaw.originated.zhawNode_CH
zhaw.publication.statuspublishedVersionde_CH
zhaw.publication.reviewPeer review (Publikation)de_CH
zhaw.title.proceedingsForum 78 Proceedingsde_CH
zhaw.webfeedFlight Mechanics and Flight Control Systemsde_CH
zhaw.author.additionalNode_CH
zhaw.display.portraitYesde_CH
Appears in collections:Publikationen School of Engineering

Files in This Item:
File Description SizeFormat 
2022_Primatesta-etal_Design-integration-tilt-rotor-flight-simulation-platform_VFS-f78.pdf617.6 kBAdobe PDFThumbnail
View/Open
Show simple item record
Capone, P., Primatesta, S., Barra, F., & Guglieri, G. (2022, May 10). Design and integration of a tilt-rotor flight simulation platform. Forum 78 Proceedings. https://doi.org/10.4050/F-0078-2022-17587
Capone, P. et al. (2022) ‘Design and integration of a tilt-rotor flight simulation platform’, in Forum 78 Proceedings. Fairfax, VA: Vertical Flight Society. Available at: https://doi.org/10.4050/F-0078-2022-17587.
P. Capone, S. Primatesta, F. Barra, and G. Guglieri, “Design and integration of a tilt-rotor flight simulation platform,” in Forum 78 Proceedings, May 2022. doi: 10.4050/F-0078-2022-17587.
CAPONE, Pierluigi, Stefano PRIMATESTA, Federico BARRA und Giorgio GUGLIERI, 2022. Design and integration of a tilt-rotor flight simulation platform. In: Forum 78 Proceedings. Conference paper. Fairfax, VA: Vertical Flight Society. 10 Mai 2022
Capone, Pierluigi, Stefano Primatesta, Federico Barra, and Giorgio Guglieri. 2022. “Design and Integration of a Tilt-Rotor Flight Simulation Platform.” Conference paper. In Forum 78 Proceedings. Fairfax, VA: Vertical Flight Society. https://doi.org/10.4050/F-0078-2022-17587.
Capone, Pierluigi, et al. “Design and Integration of a Tilt-Rotor Flight Simulation Platform.” Forum 78 Proceedings, Vertical Flight Society, 2022, https://doi.org/10.4050/F-0078-2022-17587.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.