@Article{Prado:1996:TrThLa,
               author = "Prado, Antonio Fernando Bertachini de Almeida",
                title = "Traveling between the lagrangian points and the earth",
              journal = "Acta Astronautica",
                 year = "1996",
               volume = "39",
               number = "7",
                pages = "483--486",
                month = "Oct.",
                 note = "International Symposium on Space Fligth Dynamics, 22-28 May, 1994, 
                         Sao Petesburgo, Russia.",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL.",
             abstract = "This paper is concerned with trajectories to transfer a spacecraft 
                         between the Lagrangian points and the Earth. The Lagrangian points 
                         have important applications in astronautics, since they are 
                         equilibrium points of the equation of motion and very good 
                         candidates to locate a satellite or a space station. The planar 
                         circular restricted three-body problem in two dimensions is used 
                         as the model for the Earth-Moon system, and Lama{\^{\i}}tre 
                         regularization is used to avoid singularities during numerical 
                         integration required to solve the Lambert's three-body problem. 
                         Relations with previous results are shown, specially with: i) 
                         Transfers between the Lagrangian points and the Moon; ii) Search 
                         for the absolute minimum V transfer between the Earth and the 
                         Moon; iii) Use of L, as a node for lunar exploration.",
                  doi = "10.1016/S0094-5765(97)85428-8",
                  url = "http://dx.doi.org/10.1016/S0094-5765(97)85428-8",
                 issn = "0094-5765",
                label = "6995",
             language = "en",
        urlaccessdate = "30 abr. 2024"
}