dc.creator | Pérez-Sánchez, Vicente | es |
dc.creator | Gómez-Tamm, Alejandro E. | es |
dc.creator | García Rubiales, Francisco Javier | es |
dc.creator | Arrue Ullés, Begoña C. | es |
dc.creator | Ollero Baturone, Aníbal | es |
dc.date.accessioned | 2022-11-10T17:27:10Z | |
dc.date.available | 2022-11-10T17:27:10Z | |
dc.date.issued | 2021 | |
dc.identifier.citation | Pérez-Sánchez, V., Gómez-Tamm, A.E., García Rubiales, F.J., Arrue Ullés, B.C. y Ollero Baturone, A. (2021). Analysis of Forces Involved in the Perching Maneuver of Flapping-Wing Aerial Systems and Development of an Ultra-Lightweight Perching System. En International Conference on Unmanned Aircraft Systems, ICUAS 2021 (1284-1290), Atenas: Institute of Electrical and Electronics Engineers Inc.. | |
dc.identifier.isbn | 978-073813115-3 | es |
dc.identifier.uri | https://hdl.handle.net/11441/139269 | |
dc.description.abstract | Trying to optimize the design of aerial robotics
systems, this work presents an optimized low-weight landing
system for flapping-wing aerial robots. The design, based on the
use of low-sized neodymium magnets, intends to provide that
these aerial robots have the capability of landing in restricted
areas by using the presented solution. This capacity will increase
the application range of these robots. A study of this situation
has been done to analyze the perching maneuver forces and
evaluate the system. The solution presented is low-weight, lowsized, and also relatively inexpensive. Therefore, this solution
may apply to most ornithopter robots. Design, analysis of
the implied forces, development and experimental validation
of the idea are presented in this work, demonstrating that
the developed solution can overcome the ornithopter’s payload
limitation providing an efficient and reliable solution | es |
dc.description.sponsorship | Unión Europea SI-1867/23/2018 ERC-ADG | es |
dc.format | application/pdf | es |
dc.format.extent | 7 p. | es |
dc.language.iso | eng | es |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | es |
dc.relation.ispartof | International Conference on Unmanned Aircraft Systems, ICUAS 2021 (2021), pp. 1284-1290. | |
dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
dc.subject | Aerial Robotics | es |
dc.subject | UAS | es |
dc.subject | Flapping-Wings | es |
dc.subject | Magnetic End-Effectors | es |
dc.title | Analysis of Forces Involved in the Perching Maneuver of Flapping-Wing Aerial Systems and Development of an Ultra-Lightweight Perching System | es |
dc.type | info:eu-repo/semantics/conferenceObject | es |
dcterms.identifier | https://ror.org/03yxnpp24 | |
dc.type.version | info:eu-repo/semantics/submittedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/openAccess | es |
dc.contributor.affiliation | Universidad de Sevilla. Departamento de Ingeniería de Sistemas y Automática | es |
dc.relation.projectID | SI-1867/23/2018 ERC-ADG | es |
dc.relation.publisherversion | https://ieeexplore.ieee.org/abstract/document/9476754 | es |
dc.identifier.doi | 10.1109/ICUAS51884.2021.9476754 | es |
dc.publication.initialPage | 1284 | es |
dc.publication.endPage | 1290 | es |
dc.eventtitle | International Conference on Unmanned Aircraft Systems, ICUAS 2021 | es |
dc.eventinstitution | Atenas | es |
dc.contributor.funder | Unión Europea | es |