@Article{GonçalvesRoccMora:2017:OrTrDe,
               author = "Gon{\c{c}}alves, Liana Dias and Rocco, Evandro Marconi and 
                         Moraes, R. V. de",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Universidade Federal 
                         de S{\~a}o Paulo (UNIFESP)}",
                title = "Orbital trajectories in deimos vicinity considering perturbations 
                         of gravitational origin",
              journal = "Journal of Physics: Conference Series",
                 year = "2017",
               volume = "911",
                pages = "012022",
             abstract = "The present work studies the possibility of maintaining an 
                         artificial satellite near to the Deimos surface, even when 
                         considering the intense Mars gravitational attraction. For this, a 
                         strategy is used in which the spacecraft orbits Mars, but with the 
                         same orbital period of Deimos and similar orbital elements. Using 
                         this strategy, the deviations in the keplerian elements that 
                         characterize the artificial satellite orbit, the magnitude of the 
                         main disturbing forces capable of altering the movement of the 
                         spacecraft and the variation of the distance between the 
                         spacecraft and Deimos are presented.",
                  doi = "10.1088/1742-6596/911/1/012022",
                  url = "http://dx.doi.org/10.1088/1742-6596/911/1/012022",
                 issn = "1742-6588",
             language = "en",
           targetfile = "goncalves_orbital.pdf",
        urlaccessdate = "27 abr. 2024"
}