@Article{GonçalvesRoccMora:2019:TrSpAi,
               author = "Gon{\c{c}}alves, Liana Dias and Rocco, Evandro Marconi and 
                         Moraes, Rodolfo Vilhena de",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "Trajectories of a spacecraft aiming to approach at a near-regular 
                         cadence of the Enceladus and Dione moons",
              journal = "Journal of Physics: Conference Series",
                 year = "2019",
               volume = "1365",
                pages = "012018",
                 note = "{XIX Brazilian Colloquium on Orbital Dynamics 2018}",
             keywords = "Astrodynamics, Orbital Motion, Orbital Perturbation.",
             abstract = "Saturn currently has about 62 moons already discovered. This 
                         number is uncertain due to the numerous of objects that orbit the 
                         planet, but it guarantees the placement of the second planet with 
                         the highest number of moons in the Solar System, each one with 
                         diverse physical and orbital characteristics. Among all the large 
                         moons of Saturn, Dione and Enceladus are the subject of the 
                         present work, whose objective is to evaluate strategic 
                         trajectories aiming to approach an artificial satellite to these 
                         moons, in a near-regular cadence. In the vicinity of Dione and 
                         Enceladus, the artificial satellite is significantly perturbed by 
                         the gravitational potential of Saturn, which in this work is 
                         expanded in spherical harmonics (\𝐽2), and also by the 
                         gravitational field of the 13 largest moons. All simulations were 
                         done using the Spacecraft Trajectory Simulator, an orbital 
                         simulator capable to consider continuous propulsion, and 
                         trajectory control in closed loop.",
                  doi = "10.1088/1742-6596/1365/1/012018",
                  url = "http://dx.doi.org/10.1088/1742-6596/1365/1/012018",
                 issn = "1742-6588",
                label = "lattes: 0088337156908774 2 Gon{\c{c}}alvesRoccMora:2019:TrSpAi",
             language = "en",
           targetfile = "goncalves_trajectories.pdf",
        urlaccessdate = "21 maio 2024"
}