Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-20444
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dc.contributor.authorAbà, Anna-
dc.contributor.authorBarra, Federico-
dc.contributor.authorCapone, Pierluigi-
dc.contributor.authorGuglieri, Giorgio-
dc.date.accessioned2020-09-10T16:00:03Z-
dc.date.available2020-09-10T16:00:03Z-
dc.date.issued2020-08-28-
dc.identifier.issn2226-4310de_CH
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/20444-
dc.description.abstractThis paper introduces a novel gimballed rotor mathematical model for real-time flight simulation of tilt-rotor aircraft and other vertical take-off and landing (VTOL) concepts, which improves the previous version of a multi-purpose rotor mathematical model developed by ZHAW and Politecnico di Torino as part of a comprehensive flight simulation model of a tilt-rotor aircraft currently implemented in the Research and Didactics Simulator of ZHAW and used for research activities such as handling qualities studies and flight control systems development. In the novel model, a new formulation of the flapping dynamics is indroduced to account for the gimballed rotor and better suit current tilt-rotor designs (XV-15, V-22, AW-609). This paper describes the mathematical model and provides a generic formulation as well as a specific one for 3-blades proprotors. The method expresses the gimbal attitude but also considers the variation of each blade’s flapping due to the elasticity of the blades, so that the rotor coning angle can be represented. A validation of the mathematical model is performed against the available literature on the XV-15 Tilt-rotor aircraft and a comparison between the previous model is provided to show the improvements achieved. The results show a good correlation between the model and the reference data and the registered performance allow real-time flight simulation with pilot and hardware in the loop.de_CH
dc.language.isoende_CH
dc.publisherMDPIde_CH
dc.relation.ispartofAerospacede_CH
dc.rightshttp://creativecommons.org/licenses/by/4.0/de_CH
dc.subjectTilt-rotorde_CH
dc.subjectReal-time flight simulationde_CH
dc.subjectRotor dynamicsde_CH
dc.subjectMathematical modellingde_CH
dc.subjectAerodynamicsde_CH
dc.subjectVTOLde_CH
dc.subjectAir taxide_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleMathematical modelling of gimballed tilt-rotors for real-time flight simulationde_CH
dc.typeBeitrag in wissenschaftlicher Zeitschriftde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
dc.identifier.doi10.3390/aerospace7090124de_CH
dc.identifier.doi10.21256/zhaw-20444-
zhaw.funding.euNode_CH
zhaw.issue9de_CH
zhaw.originated.zhawYesde_CH
zhaw.pages.start124de_CH
zhaw.publication.statuspublishedVersionde_CH
zhaw.volume7de_CH
zhaw.publication.reviewPeer review (Publikation)de_CH
zhaw.webfeedAerodynamicsde_CH
zhaw.author.additionalNode_CH
zhaw.display.portraitYesde_CH
Appears in collections:Publikationen School of Engineering

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Abà, A., Barra, F., Capone, P., & Guglieri, G. (2020). Mathematical modelling of gimballed tilt-rotors for real-time flight simulation. Aerospace, 7(9), 124. https://doi.org/10.3390/aerospace7090124
Abà, A. et al. (2020) ‘Mathematical modelling of gimballed tilt-rotors for real-time flight simulation’, Aerospace, 7(9), p. 124. Available at: https://doi.org/10.3390/aerospace7090124.
A. Abà, F. Barra, P. Capone, and G. Guglieri, “Mathematical modelling of gimballed tilt-rotors for real-time flight simulation,” Aerospace, vol. 7, no. 9, p. 124, Aug. 2020, doi: 10.3390/aerospace7090124.
ABÀ, Anna, Federico BARRA, Pierluigi CAPONE und Giorgio GUGLIERI, 2020. Mathematical modelling of gimballed tilt-rotors for real-time flight simulation. Aerospace. 28 August 2020. Bd. 7, Nr. 9, S. 124. DOI 10.3390/aerospace7090124
Abà, Anna, Federico Barra, Pierluigi Capone, and Giorgio Guglieri. 2020. “Mathematical Modelling of Gimballed Tilt-Rotors for Real-Time Flight Simulation.” Aerospace 7 (9): 124. https://doi.org/10.3390/aerospace7090124.
Abà, Anna, et al. “Mathematical Modelling of Gimballed Tilt-Rotors for Real-Time Flight Simulation.” Aerospace, vol. 7, no. 9, Aug. 2020, p. 124, https://doi.org/10.3390/aerospace7090124.


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