@Article{FerreiraPrad:2023:PeOrRe,
author = "Ferreira, Alessandra F. S. and Prado, Antonio Fernando Bertachini
de Almeida",
affiliation = "{Universidade Estadual Paulista (UNESP)} and {Instituto Nacional
de Pesquisas Espaciais (INPE)}",
title = "Periodic orbits in the restricted three-body problem for
observations of the smaller primary",
journal = "European Physical Journal: Special Topics",
year = "2023",
volume = "23",
pages = "e01020",
abstract = "This work proposes a numerical investigation for periodic orbits
in the restricted three-body problem to observe the smaller
primary of the system. Periodic orbits are very important for
observation missions, because they do not need station-keeping
maneuvers and allow predicted passages by the main bodies. So,
they allow a better observation of the body under study. For this
verification, the grid search method will be used [(Barrio and
Blesa, Chaos Solit Fractals, 41, 560582 (2009)]. For each set of
conditions, the differential equations of the motion of the
spacecraft will be numerically integrated using TIDES [Abad et
al., ACM Trans Math Softw (TOMS) 39, 128 (2012)]. In case of
occurrence of periodic orbits, the characteristics of these orbits
will be analyzed and the families found will be identified and
classified. In particular, it is important to avoid effects from
the close approach with the secondary body (swing-by), because
this effect may destroy the periodicity of the orbit. This can be
done using angle of approaches of 0\◦ or 180\◦ for
the close approach, because they allow passages very close to the
smaller body but with zero variations in energy and angular
momentum. This aspect of the Swing-By maneuver is very important
in the present research.",
doi = "10.1140/epjs/s11734-023-01020-2",
url = "http://dx.doi.org/10.1140/epjs/s11734-023-01020-2",
issn = "1951-6355 and 1951-6401",
language = "en",
targetfile = "s11734-023-01020-2.pdf",
urlaccessdate = "16 jun. 2024"
}