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		<citationkey>SantosPradMoraCarv:2016:StPeIn</citationkey>
		<title>Study of perturbation integrals applied to the dynamics of spacecrafts around Galilean moons</title>
		<year>2016</year>
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		<author>Santos, Josué Cardoso dos,</author>
		<author>Prado, Antonio Fernando Bertachini de Almeida,</author>
		<author>Moraes, Rodolpho Vilhena de,</author>
		<author>Carvalho, Jean Paulo S.,</author>
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		<group>DMC-ETE-INPE-MCTI-GOV-BR</group>
		<affiliation>Universidade Estadual Paulista (UNESP)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Universidade Federal de São Paulo (UNIFESP)</affiliation>
		<affiliation>Universidade Federal do Estado de São Paulo (UNIFESP)</affiliation>
		<electronicmailaddress></electronicmailaddress>
		<electronicmailaddress>antonio.prado@inpe.br</electronicmailaddress>
		<conferencename>AAS/AIAA Space Flight Mechanics Meeting, 26</conferencename>
		<conferencelocation>Napa, CA</conferencelocation>
		<date>14-18 Feb.</date>
		<secondarytype>PRE CI</secondarytype>
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		<abstract>Several scientific missions have been proposed for a deeper exploration of planetary systems. These missions require a lot of specialized techniques in order to reach a better understanding of the dynamics involved in their planning. In order to help to get important features about each system under study, the present study proposes to use different definitions of integrals of the perturbing forces received by spacecrafts for a specific system. These computations present important information about the energy given and/or removed from the spacecraft due to the effects of each perturbation considered in the system and they also help to understand.</abstract>
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