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dc.contributor.author | Herrero Debón, Alicia | es_ES |
dc.contributor.author | Moll López, Santiago Emmanuel | es_ES |
dc.contributor.author | Moraño Fernández, José Antonio | es_ES |
dc.contributor.author | Vázquez, David | es_ES |
dc.contributor.author | Vega, Erika | es_ES |
dc.date.accessioned | 2022-05-24T18:05:07Z | |
dc.date.available | 2022-05-24T18:05:07Z | |
dc.date.issued | 2021-12 | es_ES |
dc.identifier.uri | http://hdl.handle.net/10251/182876 | |
dc.description.abstract | [EN] Interception of extrasolar objects is one of the major current astrophysical objectives since it allows gathering information on the formation and composition of other planetary systems. This paper develops a tool to design optimal orbits for the interception of these bodies considering the effects of different perturbation sources. The optimal trajectory is obtained by solving a Lambert's problem that gives the required initial impulse. A numerical integration of a perturbed orbital model is calculated. This model considers the perturbations of the joint action of the gravitational potentials of the Solar System planets and the solar radiation pressure. These effects cause a deviation in the orbit that prevents the interception from taking place, so an iterative correction scheme of the initial estimated impulse is presented, capable of modifying the orbit and achieving a successful interception in a more realistic environment. | es_ES |
dc.description.sponsorship | This research has been partially supported by the Spanish Ministerio de Ciencia, Innovacion y Universidades and the Fondo Europeo de Desarrollo Regional, Project PID2019-109753GB-C22. | es_ES |
dc.language | Inglés | es_ES |
dc.publisher | MDPI AG | es_ES |
dc.relation.ispartof | Aerospace | es_ES |
dc.rights | Reconocimiento (by) | es_ES |
dc.subject | Interception | es_ES |
dc.subject | Extrasolar bodies | es_ES |
dc.subject | Lambert's problem | es_ES |
dc.subject | Perturbations | es_ES |
dc.subject | Orbit propagation | es_ES |
dc.subject.classification | MATEMATICA APLICADA | es_ES |
dc.title | Iterative Lambert's Trajectory Optimization for Extrasolar Bodies Interception | es_ES |
dc.type | Artículo | es_ES |
dc.identifier.doi | 10.3390/aerospace8120366 | es_ES |
dc.relation.projectID | info:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020/PID2019-109753GB-C22/ES/TEORIA DE CAMPOS Y GRAVITACION/ | es_ES |
dc.rights.accessRights | Abierto | es_ES |
dc.contributor.affiliation | Universitat Politècnica de València. Instituto de Diseño para la Fabricación y Producción Automatizada - Institut de Disseny per a la Fabricació i Producció Automatitzada | es_ES |
dc.contributor.affiliation | Universitat Politècnica de València. Departamento de Matemática Aplicada - Departament de Matemàtica Aplicada | es_ES |
dc.description.bibliographicCitation | Herrero Debón, A.; Moll López, SE.; Moraño Fernández, JA.; Vázquez, D.; Vega, E. (2021). Iterative Lambert's Trajectory Optimization for Extrasolar Bodies Interception. Aerospace. 8(12):1-16. https://doi.org/10.3390/aerospace8120366 | es_ES |
dc.description.accrualMethod | S | es_ES |
dc.relation.publisherversion | https://doi.org/10.3390/aerospace8120366 | es_ES |
dc.description.upvformatpinicio | 1 | es_ES |
dc.description.upvformatpfin | 16 | es_ES |
dc.type.version | info:eu-repo/semantics/publishedVersion | es_ES |
dc.description.volume | 8 | es_ES |
dc.description.issue | 12 | es_ES |
dc.identifier.eissn | 2226-4310 | es_ES |
dc.relation.pasarela | S\453757 | es_ES |
dc.contributor.funder | Agencia Estatal de Investigación | es_ES |
dc.contributor.funder | European Regional Development Fund | es_ES |
dc.subject.ods | 03.- Garantizar una vida saludable y promover el bienestar para todos y todas en todas las edades | es_ES |