@Article{MasagoPradChiaGome:2016:DePrIn,
               author = "Masago, Bruna Yukiko Pinheiro Lopes and Prado, Antonio Fernando 
                         Bertachini de Almeida and Chiaradia, Ana Paula Marins and Gomes, 
                         Vivian Martins",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Universidade Estadual 
                         Paulista (UNESP)} and {Universidade Estadual Paulista (UNESP)}",
                title = "Developing the {"}Precessing Inclined Bi-Elliptical Four-Body 
                         Problem with Radiation Pressure{"} to search for orbits in the 
                         triple asteroid 2001SN(263)",
              journal = "Advances in Space Research",
                 year = "2016",
               volume = "57",
               number = "4",
                pages = "962--982",
                month = "Feb.",
             keywords = "Astrodynamics, Orbital maneuvers, Close approach trajectories, 
                         Small bodies.",
             abstract = "Space missions to visit small bodies of the Solar System are 
                         important steps to improve our knowledge of the Solar System. 
                         Usually those bodies do not have well known characteristics, as 
                         their gravity field, which make the mission planning a difficult 
                         task. The present paper has the goal of studying orbits around the 
                         triple asteroid 2001SN(263), a Near-Earth Asteroid (NEA). A 
                         mission to this system allows the exploration of three bodies in 
                         the same trip. The distances reached by the spacecraft from those 
                         three bodies have fundamental importance in the quality of their 
                         observations. Therefore, the present research has two main goals: 
                         (i) to develop a semi-analytical mathematical model, which is 
                         simple, but able to represent the main characteristics of that 
                         system; (ii) to use this model to find orbits for a spacecraft 
                         with the goal of remaining the maximum possible time near the 
                         three bodies of the system, without the need of space maneuvers. 
                         This model is called {"}Precessing Inclined Bi-Elliptical Problem 
                         with Radiation Pressure{"} (PIBEPRP). The use of this model allow 
                         us to find important natural orbits for the exploration of one, 
                         two or even the three bodies of the system. These trajectories can 
                         be used individually or combined in two or more parts using 
                         orbital maneuvers.",
                  doi = "10.1016/j.asr.2015.12.007",
                  url = "http://dx.doi.org/10.1016/j.asr.2015.12.007",
                 issn = "0273-1177 and 1879-1948",
             language = "en",
           targetfile = "masago_developing.pdf",
        urlaccessdate = "27 abr. 2024"
}