@Article{GomesPrad:2008:SwMaCl,
author = "Gomes, Vivian Martins and Prado, Antonio Fernando Bertachini de
Almeida",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Swing-by maneuvers for a cloud of particles with planets of the
solar system",
journal = "WSEAS Transactions on Applied and Theoretical Mechanics",
year = "2008",
volume = "3",
number = "11",
pages = "859--868",
keywords = "Astrodynamics, Orbital maneuvers, Swing-By, Gravity assisted
maneuvers, Orbital motion.",
abstract = "The idea of the present paper is to study the swing-by maneuver
between one of the planets of the Solar System and a cloud of
particles. This is what happens when a fragmented comet crosses
the orbit of a planet like Jupiter, Saturn, etc. We used the
dynamical system that is formed by two main bodies (the Sun and
one of the planets of the Solar System) and we assumed that they
are in circular orbits around their center of mass and a cloud of
particles is moving under the gravitational attraction of these
two primaries. The motion is assumed to be planar for all the
particles and the dynamics given by the patched-conic
approximation is used, which means that a series of two-body
problems are used to generate analytical equations that describe
the problem. The main obejctive is to understand the change of the
orbit of this cloud of particles after the close approach with the
planet. It is assumed that all the particles that belong to the
cloud have semi-major axis a ± da and eccentricity e ± de before
the close approach with the planet. It is desired to known those
values after the close approach. In particular, we will study the
effects of the periapsis distance in this maneuver.",
issn = "1991-8747",
label = "lattes: 7340081273816424 2 GomesPrad:2009:SwMaCl",
language = "en",
targetfile = "29-110vivian.pdf",
urlaccessdate = "17 jan. 2021"
}