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Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-19753
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dc.contributor.authorBarra, Federico-
dc.contributor.authorCapone, Pierluigi-
dc.contributor.authorMonstein, Raphael-
dc.contributor.authorGodio, Simone-
dc.contributor.authorGuglieri, Giorgio-
dc.date.accessioned2020-03-12T16:09:04Z-
dc.date.available2020-03-12T16:09:04Z-
dc.date.issued2019-09-17-
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/19753-
dc.description.abstractThis paper aims at describing the effort performed by the joint research group of Politecnico di Torino and ZHAW (Zurich University of Applied Sciences) in achieving a novel implementation of a mathematical model for real-time flight simulation of tilt-rotors and tilt-wings aircraft. The focus is on the description of the current stage of the project, the achievements of the first version of the model, on-going improvements and future developments. The first part of the work describes the initial development of the overall simulation model: relying on several NASA reports on the Generic Tilt Rotor Simulator (GTRS), the mathematical model is revised and the rotor dynamic model is improved in order to enhance computational performance. In particular, the model uses the conventional mathematical formulation for non-dynamic inflow modelling based on Blade Element Momentum Theory. A novel but simple numerical method is used to ensure the convergence of the non-linear equation in every tested condition. The resulting simulation model and its development and implementation in the MATLAB/Simulink® environment is described. The second part of the work deals with the integration of the model in the ZHAW Research and Didactics Simulator (ReDSim), the replacement of the pilot controls by the introduction of a center stick and the corresponding adjustment of the force-feel system to suitable values for the tilt-rotor model. Subsequently, several pilot tests are carried out and preliminary feedbacks about the overall behaviour of the system are collected. Limits and weaknesses of the first release of the model are investigated and future necessary improvements are assessed, such as the development of a novel generic prop-rotor mathematical model. The third part introduces the novel multi-purpose rotor mathematical model which was developed to improve the overall tilt-rotor simulation model. The multi-purpose rotor model implements non-approximated flapping dynamics and inflow dynamic based on Pitt-Peters formulation. The validation of the nover rotor model is carried out with available data of both the XV-15 Research Aircraft and the UH-60 Helicopter.de_CH
dc.language.isoende_CH
dc.publisherZHAW Zürcher Hochschule für Angewandte Wissenschaftende_CH
dc.rightshttp://creativecommons.org/licenses/by/4.0/de_CH
dc.subjectTilt-rotor flight simulationde_CH
dc.subjectRotocraft flight simulationde_CH
dc.subjectFlight mechanicsde_CH
dc.subjectFlight dynamicsde_CH
dc.subjectRotor dynamicsde_CH
dc.subjectRotor modellingde_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleImplementation of a comprehensive mathematical model for tilt-rotor real-time flight simulationde_CH
dc.typeKonferenz: Paperde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
dc.identifier.doi10.21256/zhaw-19753-
zhaw.conference.details45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019de_CH
zhaw.funding.euNode_CH
zhaw.originated.zhawYesde_CH
zhaw.publication.statuspublishedVersionde_CH
zhaw.publication.reviewPeer review (Publikation)de_CH
zhaw.webfeedFlight Mechanics and Flight Control Systemsde_CH
zhaw.author.additionalNode_CH
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Barra, F., Capone, P., Monstein, R., Godio, S., & Guglieri, G. (2019, September 17). Implementation of a comprehensive mathematical model for tilt-rotor real-time flight simulation. 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019. https://doi.org/10.21256/zhaw-19753
Barra, F. et al. (2019) ‘Implementation of a comprehensive mathematical model for tilt-rotor real-time flight simulation’, in 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019. ZHAW Zürcher Hochschule für Angewandte Wissenschaften. Available at: https://doi.org/10.21256/zhaw-19753.
F. Barra, P. Capone, R. Monstein, S. Godio, and G. Guglieri, “Implementation of a comprehensive mathematical model for tilt-rotor real-time flight simulation,” in 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019, Sep. 2019. doi: 10.21256/zhaw-19753.
BARRA, Federico, Pierluigi CAPONE, Raphael MONSTEIN, Simone GODIO und Giorgio GUGLIERI, 2019. Implementation of a comprehensive mathematical model for tilt-rotor real-time flight simulation. In: 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019. Conference paper. ZHAW Zürcher Hochschule für Angewandte Wissenschaften. 17 September 2019
Barra, Federico, Pierluigi Capone, Raphael Monstein, Simone Godio, and Giorgio Guglieri. 2019. “Implementation of a Comprehensive Mathematical Model for Tilt-Rotor Real-Time Flight Simulation.” Conference paper. In 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019. ZHAW Zürcher Hochschule für Angewandte Wissenschaften. https://doi.org/10.21256/zhaw-19753.
Barra, Federico, et al. “Implementation of a Comprehensive Mathematical Model for Tilt-Rotor Real-Time Flight Simulation.” 45th European Rotorcraft Forum, Warsaw, Poland, 17-20 September 2019, ZHAW Zürcher Hochschule für Angewandte Wissenschaften, 2019, https://doi.org/10.21256/zhaw-19753.


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