@InCollection{FelipePrad:2002:GrCoSp,
               author = "Felipe, Gislaine and Prado, Antonio Fernando Bertachini de 
                         Almeida",
                title = "Gravitational control of a spacecraft passing by a planet in the 
                         three-dimensional space",
            booktitle = "Nonlinear dynamics, chaos, control and their applications to 
                         engineering sciences",
            publisher = "ABCM;SBMAC",
                 year = "2002",
               editor = "Balthazar, Jos{\'e} Manoel and Gon{\c{c}}alves, Paulo Batista 
                         and Brasil, Reyolando M. F. L. R. F. .",
                pages = "Cap. 12, 159--168",
             keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, swing-by, maneuvers, three-body 
                         problem.",
             abstract = "In the present paper the swing-by maneuvers are studied under the 
                         model given by the threedimensional circular restricted three-body 
                         problem. This maneuver can be identified by five independent 
                         parameters: Vp, the magnitude of the velocity of the spacecraft at 
                         periapsis; y, the angle between the velocity vector at periapsis 
                         and the intersection between the horizontal plane that passes by 
                         the periapsis and the plane perpendicular to the periapsis that 
                         holds Vp;rp; r, the distance between the spacecraft and the 
                         celestial body during the closest approach; a, the angle between 
                         the projection of the periapsis line in the x-y plane and the line 
                         that connects the two primaries; {\'a}, the angle between the 
                         periapsis line and the x-y plane. A numerical algorithm to study 
                         this problem was build and used to generate several results. Based 
                         in those results, it is possible to control the orbit of the 
                         spacecraft with the use of the gravitational forces.",
                label = "10155",
          seriestitle = "Nonlinear dynamics, chaos, control and their applications to 
                         engineering sciences",
           targetfile = "9233.pdf",
        urlaccessdate = "26 abr. 2024"
}