@InCollection{Prado:2002:ImTrTo,
               author = "Prado, Antonio Fernando Bertachini de Almeida",
                title = "Impulsive transfer to/from the lagrangian point in the Earth -sun 
                         system",
            booktitle = "Advances in space dynamics 3: applications in astronautics",
            publisher = "INPE",
                 year = "2002",
               editor = "Winter, Othon Cabo and Prado, Antonio Fernando Bertachini de 
                         Almeida.",
                pages = "272--286",
              address = "S{\~a}o Jos{\'e} dos Campos",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, three-body problem, transfer 
                         orbits, lagrange points, Lambert method.",
             abstract = "This paper is concerned with trajectories to transfer a spacecraft 
                         between the Lagrange points of the Sun-Earth system and the Sun. 
                         The Lagrange 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 Sun-Earth system, and Lemaitre 
                         regularization is used to avoid singularities during the numerical 
                         integration required to solve the Lambert's three-body problem. 
                         The results show families of transfer orbits, parameterized by the 
                         transfer time.",
                label = "10459",
                  ibi = "6qtX3pFwXQZ3r59YCT/H3JKv",
                  url = "http://urlib.net/ibi/6qtX3pFwXQZ3r59YCT/H3JKv",
          seriestitle = "Advances in space dynamics 3: applications in astronautics",
           targetfile = "INPE-9531.pdf",
        urlaccessdate = "01 maio 2024"
}