author = "Ferreira, A. F. S. and Moraes, Rodolfo Vilhena de and Prado, 
                         Antonio Fernando Bertachini de Almeida and Winter, Othon Cabo",
                title = "Trajectory analysis of a spacecraft making a three-dimensional 
                         powered swing-by maneuver",
            booktitle = "Astrodynamics 2018, PTS I-IV",
            publisher = "Univelt",
                 year = "2019",
               editor = "Singla, P. and Weisman, R. M. and Marchand, B. G. and Jones, B. 
                pages = "1107--1126",
                 note = "AAS/AIAA Astrodynamics Specialist Confernece, 2018, 19-23 aug., 
                         Snowbird, UT.",
             keywords = "orbital maneuvers.",
             abstract = "The present paper studies the problem of orbital maneuvers 
                         performed combining the passage of a spacecraft by a celestial 
                         body with an impulse applied to the spacecraft during the close 
                         approach. The motion of the spacecraft is assumed to be in the 
                         three-dimensional space, thus allowing plane change. This type of 
                         maneuver can also send the spacecraft to a point far from the 
                         orbit or to end in capture or collision of the spacecraft by the 
                         celestial body. The effects of the variations in the orbital 
                         plane, energy and the angular momentum of the spacecraft are 
          affiliation = "{Universidade Estadual Paulista (UNESP)} and {Universidade 
                         Estadual Paulista (UNESP)} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)} and {Instituto Nacional de Pesquisas Espaciais 
             language = "en",
          seriestitle = "Advances in the Astronautical Sciences",
               volume = "167",
        urlaccessdate = "17 abr. 2021"