@Article{AlmeidaJśniorPrad:2022:CoThCi,
author = "Almeida J{\'u}nior, Allan Kardec de and Prado, Antonio Fernando
Bertachini de Almeida",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Comparisons between the circular restricted three-body and
bi-circular four body problems for transfers between the two
smaller primaries",
journal = "Scientific Reports",
year = "2022",
volume = "12",
number = "1",
pages = "e4148",
month = "Mar.",
abstract = "Important properties of the dynamics of a spacecraft can be
obtained from the Circular Restricted Three Body Problem and the
Bi-Circular Bi-planar Four Body Problem. In this work, both
systems are compared under the perspective of the costs involved
in a transfer between the smaller primaries. An analytical
approach shows several properties of the perturbation due to the
gravity of the Sun and the motion of the smaller primaries around
it over a spacecraft in the region of interest, like its behavior
at and around the barycenter or at any point in a circle around
the Sun. The costs involved in transfers between the smaller
primaries are numerically evaluated and analyzed using the newly
developed Theory of Functional Connections. The results show that
the influence of this perturbation over the costs is significant
for systems like the Sun-Earth-Moon or Sun-Mars-Phobos. On the
other hand, it is also shown that this influence may be negligible
for other very different systems, like the Sun-Saturn-Titan or
Sun-Ida-Dactyl. Maps of perturbation are drawn in the region of
interest, which can be used for mission designers. Finally, a new
approach to describe the influence of the Sun over the tides of
the smaller primaries is proposed under the Four Body Problem
model.",
doi = "10.1038/s41598-022-08046-x",
url = "http://dx.doi.org/10.1038/s41598-022-08046-x",
issn = "2045-2322",
language = "en",
targetfile = "almeida jr_2022_comparisons.pdf",
urlaccessdate = "25 jun. 2024"
}