@InProceedings{FormigaPrad:2011:OrChDu,
               author = "Formiga, J. K. S. and Prado, A. F. B. A.",
          affiliation = "{Technology Faculty-FATEC-SJC} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "Orbital Characteristics Due to the Three Dimensional Swing-By in 
                         the Sun-Jupiter System",
            booktitle = "Proceedings...",
                 year = "2011",
                pages = "61--69",
         organization = "10. International Conference on Computational Intelligence 
                         Man-Machine Systems and Cybernetics",
            publisher = "he World Scientific and Engineering Academy and Society Press",
             keywords = "orbital maneuver, three dimensional swing-by, celestial mechanics, 
                         orbital dynamics.",
             abstract = "This paper presents an analytical and numerical study about 
                         orbital characteristics of trajectories due to a three dimensional 
                         swing-by maneuver between a planet and a particle. The model used 
                         has the same hypothesis of the circular restricted three-body 
                         problem. It is assumed that the forces are given by two main 
                         bodies that are in circular orbits around their center of mass and 
                         that the particles are moving under the gravitational attraction 
                         of these two primaries. This method has been under study for a 
                         long time by several authors, most of them used the dynamical 
                         system given by the patched-conics. The technique shown here 
                         generates accurate solutions for interplanetary transfer 
                         description. Two solutions are considered for the Swing- By 
                         (clock-wise and counter-clock-wise orbit). The goal is to study 
                         the orbital change due to the variation of inclination, longitude 
                         of the ascending node and argument of periapsis, considering two 
                         angles of approaches. Finally, numerical simulations are performed 
                         using the Sun-Jupiter system to determine the evolution of the 
                         cloud of particles during the maneuver and to map regions for 
                         optimal maneuvers.",
  conference-location = "Jakarta",
      conference-year = "2011",
                 isbn = "978-1-61804-049-7",
             language = "en",
           targetfile = "CIMISP-09.pdf",
               volume = "1",
        urlaccessdate = "15 jan. 2021"
}