@Article{Prado:2006:OrMaTh,
               author = "Prado, Antonio Fernando Bertachini de Almeida",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)}",
                title = "Orbital maneuvers between the lagrangian points and the primaries 
                         in the Earth-Sun system",
              journal = "Journal of the Brazilian Society of Mechanical Sciences and 
                         Engineering",
                 year = "2006",
               volume = "28",
               number = "2",
                pages = "131--139",
                month = "Apr.-June",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAIS, astrodynamics, lagrangian 
                         points, orbital maneuvers, impulsive transfers.",
             abstract = "This paper is concerned with trajectories to transfer a spacecraft 
                         between the Lagrangian points of the Sun-Earth system and the 
                         primaries. 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 Sun-Earth system, and 
                         Lama{\^{\i}}tre 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.",
           copyholder = "SID/SCD",
                 issn = "0100-7386",
             language = "en",
           targetfile = "prado-orbital maneuvers.pdf",
        urlaccessdate = "01 maio 2024"
}