@Article{Prado:2006:OrMaTh,
author = "Prado, Antonio Fernando Bertachini de Almeida",
title = "Orbital maneuvers between the Lagrangian points and the primaries
in the Earth-Sun system",
journal = "Journal of the Brazilian Society of Mechanical Sciences and
Engineering",
year = "2006",
volume = "28",
number = "2",
pages = "131--139",
month = "Apr./June",
keywords = "Astrodynamics, lagrangian points, orbital maneuvers, impulsive
transfers.",
abstract = "This paper is concerned with trajectories to transfer a spacecraft
between the Lagrangian points of the Sun-Earth system and the
primaries. The Lagrangian points have important applications in
astronautics, since they are equilibrium points of the equation of
motion and very good candidates to locate a satellite or a space
station. The planar circular restricted three-body problem in two
dimensions is used as the model for the Sun-Earth system, and
Lama{\^{\i}}tre regularization is used to avoid singularities
during the numerical integration required to solve the Lambert's
three-body problem. The results show families of transfer orbits,
parameterized by the transfer time. .",
issn = "0100-7386",
language = "en",
targetfile = "prado1.pdf",
urlaccessdate = "30 abr. 2024"
}