Effects of the eccentricity on the primaries in the gravitational capture phenomenon

Página do item simplificado
dc.contributor.authorNeto, E. V.
dc.contributor.authorPrado, AFBD
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T15:28:31Z
dc.date.available2014-05-20T15:28:31Z
dc.date.issued2006-01-01
dc.description.abstractGravitational capture is a characteristic of some dynamical systems in celestial mechanics, as in the elliptic restricted three-body problem that is considered in this paper. The basic idea is that a spacecraft (or any particle with negligible mass) can change a hyperbolic orbit with a small positive energy around a celestial body into an elliptic orbit with a small negative energy without the use of any propulsive system. The force responsible for this modification in the orbit of the spacecraft is the gravitational force of the third body involved in the dynamics. In this way, this force is used as a zero cost control, equivalent to a continuous thrust applied in the spacecraft. One of the most important applications of this property is the construction of trajectories to the Moon. The objective of the present paper is to study in some detail the effects of the eccentricity of the primaries in this maneuver.en
dc.description.affiliationUNESP, Fac Engn Guaratingueta, Guaratingueta, Brazil
dc.description.affiliationUnespUNESP, Fac Engn Guaratingueta, Guaratingueta, Brazil
dc.format.extent429-446
dc.identifier.citationMalcolm D. Shuster Astronautics Symposium. San Diego: Univelt Inc., v. 122, p. 429-446, 2006.
dc.identifier.issn1081-6003
dc.identifier.urihttp://hdl.handle.net/11449/38314
dc.identifier.wosWOS:000236528100025
dc.language.isoeng
dc.publisherUnivelt Inc
dc.relation.ispartofMalcolm D. Shuster Astronautics Symposium
dc.rights.accessRightsAcesso aberto
dc.sourceWeb of Science
dc.titleEffects of the eccentricity on the primaries in the gravitational capture phenomenonen
dc.typeTrabalho apresentado em evento
dcterms.rightsHolderUnivelt Inc
unesp.author.orcid0000-0002-7966-3231[2]
unesp.author.orcid0000-0002-7589-0998[1]

Arquivos

Licença do Pacote
Agora exibindo 1 - 1 de 1
Nenhuma Miniatura disponível
Nome:
license.txt
Tamanho:
1.71 KB
Formato:
Item-specific license agreed upon to submission
Descrição:

Coleções

Artigos