%0 Conference Proceedings
%4 sid.inpe.br/mtc-m21c/2018/08.20.11.34
%2 sid.inpe.br/mtc-m21c/2018/08.20.11.34.49
%T Trajectory analysis of a spacecraft making a three-dimensional powered swing-by maneuver
%D 2018
%A Ferreira, Alessandra Ferraz da Silva,
%A Moraes, Rodolpho Vilhena de,
%A Prado, Antonio Fernando Bertachini de Almeida,
%A Winter, Othon,
%@affiliation Universidade Estadual Paulista (UNESP)
%@affiliation Universidade Federal de São Paulo (UNIFESP)
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%@affiliation Universidade Estadual Paulista (UNESP)
%@electronicmailaddress
%@electronicmailaddress
%@electronicmailaddress antonio.prado@inpe.br
%B AAS/AIAA Astrodynamics Specialist Conference
%C Snowbird, UT, USA
%8 19-23 aug.
%X This paper proposes to study orbital maneuvers performed by the passage of a spacecraft near of a celestial body with impulsive propulsion, considering the movement of the space vehicle in the three-dimensional space, thus allowing the orbital plane change. This type of maneuver can send the probe to a point far from the orbit or to cause the capture or escape of the spacecraft by the celestial body. The effects of the orbit change on the energy and angular momentum of the spacecraft will be presented, as well as the types of orbits and inclination resulting from this change.
%@language en
%3 FinalPaper_AAS-ale.pdf