@InProceedings{FelipePrad:2000:StInCh,
author = "Felipe, Gislaine de and Prado, Antonio Fernando Bertachini de
Almeida",
title = "Study of the inclination change in three-dimensional swing-by
trajectories",
year = "2000",
pages = "60",
organization = "International Symposium on Space Technology and Science, 22.",
keywords = "ENGENHARIA E TECNOLOGIA ESPACIAL, astrodin{\^a}mica,
trajet{\'o}rias espaciais, mec{\^a}nica celeste, manobra
orbital, t{\'e}cnica {"}swingby{"}, astrodynamics, spacecraft
trajectories, celestial mechanics, orbital maneuvers, swingby
technique.",
abstract = "In the present paper the swing-by maneuvers are studied under the
model given by the three dimensional 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, 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; , 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.",
conference-location = "Morioka, JP",
conference-year = "28 May - 4 June 2000",
label = "9310",
targetfile = "2000_felipe.PDF",
urlaccessdate = "18 jan. 2021"
}