Please use this identifier to cite or link to this item: http://repositorio.unitau.br/jspui/handle/20.500.11874/2440
Full metadata record
DC FieldValueLanguage
dc.contributor.authorGiacaglia, Giorgio Eugenio Oscarept_BR
dc.contributor.authorSchutz B.E.pt_BR
dc.date.accessioned2019-09-12T16:53:17Z-
dc.date.available2019-09-12T16:53:17Z-
dc.date.issued2009-
dc.citation.volume134pt_BR
dc.citation.spage585-
dc.citation.epage599-
dc.identifier.isbn9780877035541-
dc.identifier.issn653438-
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-80053388817&partnerID=40&md5=d9f58d4b3e0164374af99aa618ef97e9-
dc.identifier.urihttp://repositorio.unitau.br/jspui/handle/20.500.11874/2440-
dc.description.abstractNonsingular differential equations for the variation of variables suggested by Lagrange for the motion of an artificial satellite under the influence of the Earth gravitational field are developed keeping the usual orbital elements. It is shown that no singularities are present in these equations except for the case of a retrograde equatorial orbit. Equations are developed for secular, long period and short period perturbations. The advantage of retaining the usual orbital elements is to avoid a complex and cumbersome form of the equations.en
dc.description.provenanceMade available in DSpace on 2019-09-12T16:53:17Z (GMT). No. of bitstreams: 0 Previous issue date: 2009en
dc.languageInglêspt_BR
dc.publisher.countryEstados Unidospt_BR
dc.relation.ispartofAdvances in the Astronautical Sciences-
dc.relation.haspart19th AAS/AIAA Space Flight Mechanics Meeting-
dc.rightsAcesso Restritopt_BR
dc.sourceScopuspt_BR
dc.subject.otherEarth gravitational fieldsen
dc.subject.otherEquatorial orbitsen
dc.subject.otherLagrangeen
dc.subject.otherNonsingularen
dc.subject.otherOrbital elementen
dc.subject.otherShort periodsen
dc.subject.otherDifferential equationsen
dc.subject.otherMechanicsen
dc.subject.otherSpace flighten
dc.subject.otherEarth (planet)en
dc.titleA nonsingular approach in satellite theoryen
dc.typeTrabalho apresentado em eventopt_BR
dc.description.affiliationGiacaglia, G.E.O., Graduate Program in Mechanical Engineering, University of Taubaté, Brazil-
dc.description.affiliationSchutz, B.E., Aerospace Engineering and Engineering Mechanics, Center for Space Research, University of Texas, Austin, TX 78712, United States-
dc.identifier.scopus2-s2.0-80053388817-
dc.contributor.scopus55175945800pt_BR
dc.contributor.scopus7006936301pt_BR
Appears in Collections:Trabalhos Apresentados em Eventos
Artigos de Periódicos

Files in This Item:
There are no files associated with this item.
Show simple item record Recommend this item


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.