@Article{GonçalvesRoccMora:2015:AnInOr,
author = "Gon{\c{c}}alves, Liana Dias and Rocco, Evandro Marconi and
Moraes, Rodolpho Vilhena de",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Universidade Federal
de S{\~a}o Paulo (UNIFESP)}",
title = "Analysis of the influence of orbital disturbances applied to an
artificial lunar satellite",
journal = "Journal of Physics: Conference Series",
year = "2015",
volume = "641",
pages = "012028",
keywords = "Astrodynamics, Orbit Perturbation, Orbital Motion.",
abstract = "This paper analyzes the influence of the orbital disturbance
forces in the trajectory of lunar satellites. The following
gravitational and non-gravitational orbital disturbances are
considered: the non-homogeneity of the lunar gravitational field;
the gravitational attraction due to the third body, considering
the Earth and the Sun; the lunar albedo; the solar radiation
pressure. Numerical models were developed and implemented in an
orbital trajectory simulator aiming to understand the dynamics of
the orbital motion of an artificial satellite in lunar orbit when
considering the simultaneous effect of all disturbances. Different
orbits were simulated in order to characterize the major and the
minor influence of each disturbing force as function of the
inclination and the right ascension of the ascending node. This
study can be very useful in the space mission analysis and in the
selection of orbits less affected by environmental disturbances.",
doi = "10.1088/1742-6596/641/1/012028",
url = "http://dx.doi.org/10.1088/1742-6596/641/1/012028",
issn = "1742-6588",
label = "lattes: 0088337156908774 2 Gon{\c{c}}alvesRoccMora:2015:AnInOr",
language = "pt",
targetfile = "1_goncalves3.pdf",
urlaccessdate = "15 jun. 2024"
}