<?xml version="1.0" encoding="ISO-8859-1"?>
<metadatalist>
	<metadata ReferenceType="Journal Article">
		<site>plutao.sid.inpe.br 800</site>
		<holdercode>{isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}</holdercode>
		<identifier>J8LNKAN8RW/3D53AB5</identifier>
		<repository>dpi.inpe.br/plutao/2012/11.28.14.42.30</repository>
		<lastupdate>2013:02.20.12.37.56 dpi.inpe.br/plutao@80/2008/08.19.15.01 administrator</lastupdate>
		<metadatarepository>dpi.inpe.br/plutao/2012/11.28.14.42.31</metadatarepository>
		<metadatalastupdate>2018:06.05.00.01.57 dpi.inpe.br/plutao@80/2008/08.19.15.01 administrator {D 2012}</metadatalastupdate>
		<secondarykey>INPE--PRE/</secondarykey>
		<doi>10.1007/s10569-012-9426-y</doi>
		<issn>0923-2958</issn>
		<label>lattes: 0793627832164040 3 SalazarMeloMacaWint:2012:ThPrLa</label>
		<citationkey>SalazarMeloMacaWint:2012:ThPrLa</citationkey>
		<title>Three-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5</title>
		<year>2012</year>
		<month>Oct.</month>
		<secondarytype>PRE PI</secondarytype>
		<numberoffiles>1</numberoffiles>
		<size>713 KiB</size>
		<author>Salazar, F. J. T.,</author>
		<author>Melo, Cristiano Fiorilo de,</author>
		<author>Macau, Elbert Einstein Nehrer,</author>
		<author>Winter, Othon Cabo,</author>
		<resumeid></resumeid>
		<resumeid></resumeid>
		<resumeid>8JMKD3MGP5W/3C9JGUT</resumeid>
		<group>LAC-CTE-INPE-MCTI-GOV-BR</group>
		<group></group>
		<group>LAC-CTE-INPE-MCTI-GOV-BR</group>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Universidade Federal do ABC, Rua Santa Adélia 166, Santo André, SP, 09210-170, Brazil O. C. Winter</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Univ Estadual Paulista—UNESP, Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá, SP 12516-410, Brazil</affiliation>
		<electronicmailaddress></electronicmailaddress>
		<electronicmailaddress></electronicmailaddress>
		<electronicmailaddress>elbert@lac.inpe.br</electronicmailaddress>
		<e-mailaddress>elbert@lac.inpe.br</e-mailaddress>
		<journal>Celestial Mechanics and Dynamical Astronomy</journal>
		<volume>114</volume>
		<number>1-2</number>
		<pages>201-213</pages>
		<transferableflag>1</transferableflag>
		<contenttype>External Contribution</contenttype>
		<versiontype>publisher</versiontype>
		<keywords>alternative transfers, stable Lagrangian points, L4, L5, three-body problem, trajectories-G, controle de caos, dinamica nao linear, astrodinâmica, dinâmica orbital.</keywords>
		<abstract>An alternative transfer strategy to send spacecraft to stable orbits around the Lagrangian equilibrium points L4 and L5 based in trajectories derived from the periodic orbits around L1 is presented in this work. The trajectories derived, called Trajectories G, are described and studied in terms of the initial generation requirements and their energy variations relative to the Earth through the passage by the lunar sphere of influence. Missions for insertion of spacecraft in elliptic orbits around L4 and L5 are analysed considering the restricted three-body problem Earth-Moon-particle and the results are discussed starting from the thrust, time of flight and energy variation relative to the Earth.</abstract>
		<area>COMP</area>
		<language>en</language>
		<targetfile>macaulac.pdf</targetfile>
		<usergroup>administrator</usergroup>
		<usergroup>banon</usergroup>
		<usergroup>lattes</usergroup>
		<usergroup>marciana</usergroup>
		<visibility>shown</visibility>
		<archivingpolicy>denypublisher denyfinaldraft12</archivingpolicy>
		<readpermission>deny from all and allow from 150.163</readpermission>
		<documentstage>not transferred</documentstage>
		<nexthigherunit>8JMKD3MGPCW/3ESGTTP</nexthigherunit>
		<url>http://link.springer.com/article/10.1007/s10569-012-9426-y?null</url>
		<dissemination>WEBSCI; PORTALCAPES.</dissemination>
		<hostcollection>dpi.inpe.br/plutao@80/2008/08.19.15.01</hostcollection>
		<notes>Setores de Atividade: Pesquisa e desenvolvimento científico.</notes>
		<username>marciana</username>
		<lasthostcollection>dpi.inpe.br/plutao@80/2008/08.19.15.01</lasthostcollection>
		<url>http://plutao.sid.inpe.br/rep-/dpi.inpe.br/plutao/2012/11.28.14.42.30</url>
	</metadata>
</metadatalist>