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dc.contributor.authorCárdenas R., César A.spa
dc.contributor.authorCOLLAZOS MORALES, CARLOS ANDRESspa
dc.contributor.authorP. Ospina, Juanspa
dc.contributor.authorSánchez, Joaquín F.spa
dc.contributor.authorCaro-Ruiz, Claudiaspa
dc.contributor.authorHugo Grisales, Victorspa
dc.contributor.authorAriza Colpas, Paola Patriciaspa
dc.contributor.authorDe-La-Hoz-Franco, Emirospa
dc.contributor.authorR. González, Ramón E.spa
dc.date.accessioned2020-11-19T14:37:57Z
dc.date.available2020-11-19T14:37:57Z
dc.date.issued2020
dc.identifier.urihttps://hdl.handle.net/11323/7355spa
dc.description.abstractMotivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent autonomous flight, a quadrotor dynamical model is presented in this work. The purpose of this study is to get a better understanding of its flight dynamics. It is an underactuated system. So, a simplified and clear model is needed to implement controllers on these kind of unmanned aerial systems. In addition, a computational tool is used for validation purposes. For future works embedded or intelligent control systems can be developed to control them. Gyroscopic and some aerodynamics effects are neglected.spa
dc.format.mimetypeapplication/pdfspa
dc.language.isoeng
dc.publisherCorporación Universidad de la Costaspa
dc.relation.ispartofhttps://link.springer.com/bookseries/558spa
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internationalspa
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/spa
dc.sourceInternational Conference on Computational Science and Its Applicationsspa
dc.subjectQuadrotorspa
dc.subjectVTOLspa
dc.subjectFlight dynamicsspa
dc.subjectUAVspa
dc.titleMathematical Modelling and Identification of a Quadrotorspa
dc.typeArtículo de revistaspa
dc.source.urlhttps://link.springer.com/chapter/10.1007/978-3-030-58799-4_19spa
dc.rights.accessrightsinfo:eu-repo/semantics/openAccessspa
dc.identifier.doihttps://doi.org/10.1007/978-3-030-58799-4_19spa
dc.identifier.instnameCorporación Universidad de la Costaspa
dc.identifier.reponameREDICUC - Repositorio CUCspa
dc.identifier.repourlhttps://repositorio.cuc.edu.co/spa
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dc.relation.references2. Cárdenas Ruiz, C.A.: Performance study of the flight control and path planning for a UAV type Quadrotor. Ingeniería Mecatrónica (2018)spa
dc.relation.references3. Collazos, C., et al.: State estimation of a dehydration process by interval analysis. In: Figueroa-García, J.C., López-Santana, E.R., Rodriguez-Molano, J.I. (eds.) WEA 2018. CCIS, vol. 915, pp. 66–77. Springer, Cham (2018). https://doi.org/10.1007/978-3-030-00350-0_6spa
dc.relation.references4. Cook, M.V.: Flight Dynamics Prıncıples. Elsevıer (2007)spa
dc.relation.references5. Cork, L.R.: Aircraft dynamic navigation for unmanned aerial vehicles. Ph.D. thesis. Queensland University of Technology (2014)spa
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dc.relation.references7. Habib, M.K., Abdelaal, W.G.A., Saad, M.S., et al.: Dynamic modeling and control of a Quadrotor using linear and nonlinear approaches (2014)spa
dc.relation.references8. Huang, H., et al.: Aerodynamics and control of autonomous Quadrotor helicopters in aggressive maneuvering. In: IEEE International Conference on Robotics and Automation, ICRA 2009, pp. 3277–3282. IEEE (2009)spa
dc.relation.references9. Ireland, M.L.: Investigations in multi-resolution modelling of the Quadrotor micro air vehicle. Ph.D. thesis. University of Glasgow (2014)spa
dc.relation.references10. Jiménez-Cabas, J., et al.: Robust control of an evaporator through algebraic Riccati equations and d-K iteration. In: Misra, S., et al. (eds.) ICCSA 2019. LNCS, vol. 11620, pp. 731–742. Springer, Cham (2019). https://doi.org/10.1007/978-3-030-24296-1_58spa
dc.relation.references11. Leishman, G.J.: Principles of Helicopter Aerodynamics with CD Extra. Cambridge University Press, Cambridge (2006)spa
dc.relation.references12. Lugo-Cárdenas, I., et al.: Dubins path generation for a fixed wing UAV. In: 2014 International Conference on Unmanned Aircraft Systems (ICUAS), pp. 339–346. IEEE (2014)spa
dc.relation.references13. Malang, Y.: Design and Control of a Vertical Takeo and Landing Fixed-wing Unmanned Aerial Vehicle. Ph.D. thesis (2016)spa
dc.relation.references14. Mulder, S.: Flight Dynamics (2007)spa
dc.relation.references15. Swartling, J.O.: Circumnavigation with a group of Quadrotor helicopters (2014)spa
dc.relation.references16. Pharpatara, P.: Trajectory planning for aerial vehicles with constraints. Theses. Université Paris-Saclay; Université d’Evry-Val-d’Essonne, September 2015. https://tel.archives-ouvertes.fr/tel-01206423spa
dc.relation.references17. Poyi, G.T.: A novel approach to the control of quad-rotor helicopters using fuzzy-neural networks (2014)spa
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dc.relation.references19. Voos, H.: Nonlinear control of a Quadrotor micro-UAV using feedback linearization. In: International Conference on Mechatronics, ICM 2009, pp. 1–6. IEEE (2009)spa
dc.type.coarhttp://purl.org/coar/resource_type/c_6501spa
dc.type.contentTextspa
dc.type.driverinfo:eu-repo/semantics/articlespa
dc.type.redcolhttp://purl.org/redcol/resource_type/ARTspa
dc.type.versioninfo:eu-repo/semantics/acceptedVersionspa
dc.type.coarversionhttp://purl.org/coar/version/c_ab4af688f83e57aaspa
dc.rights.coarhttp://purl.org/coar/access_right/c_abf2spa


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