@InProceedings{CavalcaPradFormGome:2016:StOrAr,
               author = "Cavalca, Marina Pires de Oliveira and Prado, Ant{\^o}nio Fernando 
                         Bertachini de Almeida and Formiga, Jorge Kennety Silva and Gomes, 
                         Vivian Martins",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)}",
                title = "Study of Orbits Around the Asteroid 2001 SN263",
            booktitle = "Anais...",
                 year = "2016",
               editor = "Cerqueira, Christopher Shneider and Souza, Alain Giacobini de and 
                         Oliveira Junior, Eloy Martins de and Bertoldo Junior, Jorge and 
                         Yassuda, Irineu dos Santos and Lima, Jeanne Samara dos Santos and 
                         Morais, Marcelo Henrique Essado de and Oliveira, M{\^o}nica 
                         Elizabeth Rocha de and Gondo, Suely Mitsuko Hirakawa and Fornari, 
                         Celso Israel and Toledo, Rafael Cardoso and Fischer, Gustavo 
                         Alexandre Achilles",
         organization = "Workshop em Engenharia e Tecnologias Espaciais, 7. (WETE)",
            publisher = "Instituto Nacional de Pesquisas Espaciais (INPE)",
              address = "S{\~a}o Jos{\'e} dos Campos",
             keywords = "Aster Mission, Restricted Three-Body Problem, Spacecraft 
                         Trajectories.",
             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.",
  conference-location = "S{\~a}o Jos{\'e} dos Campos",
      conference-year = "23-25 ago. 2016",
                 issn = "2177-3114",
             language = "en",
         organisation = "Instituto Nacional de Pesquisas Espaciais (INPE)",
                  ibi = "8JMKD3MGPDW34R/3M5JQ2B",
                  url = "http://urlib.net/ibi/8JMKD3MGPDW34R/3M5JQ2B",
           targetfile = "template_wete.pdf",
                 type = "Mec{\^a}nica Espacial e Controle",
        urlaccessdate = "28 abr. 2024"
}