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		<citationkey>CavalcaPradFormGome:2016:StOrAr</citationkey>
		<title>Study of Orbits Around the Asteroid 2001 SN263</title>
		<format>On-line.</format>
		<year>2016</year>
		<secondarytype>PRE CN</secondarytype>
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		<author>Cavalca, Marina Pires de Oliveira,</author>
		<author>Prado, Antônio Fernando Bertachini de Almeida,</author>
		<author>Formiga, Jorge Kennety Silva,</author>
		<author>Gomes, Vivian Martins,</author>
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		<group>CMC-ETES-SPG-INPE-MCTI-GOV-BR</group>
		<group>DMC-ETE-INPE-MCTI-GOV-BR</group>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<electronicmailaddress>mpocavalca@hotmail.com</electronicmailaddress>
		<electronicmailaddress>antonio.prado@inpe.br</electronicmailaddress>
		<editor>Cerqueira, Christopher Shneider,</editor>
		<editor>Souza, Alain Giacobini de,</editor>
		<editor>Oliveira Junior, Eloy Martins de,</editor>
		<editor>Bertoldo Junior, Jorge,</editor>
		<editor>Yassuda, Irineu dos Santos,</editor>
		<editor>Lima, Jeanne Samara dos Santos,</editor>
		<editor>Morais, Marcelo Henrique Essado de,</editor>
		<editor>Oliveira, Mônica Elizabeth Rocha de,</editor>
		<editor>Gondo, Suely Mitsuko Hirakawa,</editor>
		<editor>Fornari, Celso Israel,</editor>
		<editor>Toledo, Rafael Cardoso,</editor>
		<editor>Fischer, Gustavo Alexandre Achilles,</editor>
		<e-mailaddress>mpocavalca@hotmail.com</e-mailaddress>
		<conferencename>Workshop em Engenharia e Tecnologias Espaciais, 7 (WETE)</conferencename>
		<conferencelocation>São José dos Campos</conferencelocation>
		<date>23-25 ago. 2016</date>
		<publisher>Instituto Nacional de Pesquisas Espaciais (INPE)</publisher>
		<publisheraddress>São José dos Campos</publisheraddress>
		<booktitle>Anais</booktitle>
		<organization>Instituto Nacional de Pesquisas Espaciais (INPE)</organization>
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		<keywords>Aster Mission, Restricted Three-Body Problem, Spacecraft Trajectories.</keywords>
		<abstract>The asteroid 2001 SN263 is one of the possible targets of a proposed mission that would be the first Brazilian exploration in deep space, the Aster Mission. This asteroid is composed of three bodies: Alpha, Beta, and Gamma, in decreasing order of mass. For this study, it is proposed to split this triple system in two double systems: Alpha-Beta-spacecraft and Alpha-Gamma-spacecraft, such that it can be used the circular plane restricted three-body problem as mathematical model. The goal is to find orbits that can be used by a spacecraft around Beta and Gamma bodies. Each orbit can be identified by the initial conditions of the spacecraft relative to Beta or Gamma, position and velocity, and between its angle relative to a reference frame. These orbits are classified by the criterion of minimize the average distance spacecraft-celestial body, and the results showed stable orbits around Beta and Gamma with an average distance below 1 km.</abstract>
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		<type>Mecânica Espacial e Controle</type>
		<language>en</language>
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		<readergroup>mpocavalca@hotmail.com</readergroup>
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