@Article{SalazarMasGómMacWin:2014:ZeMiMa,
author = "Salazar, F. J. T. and Masdemont, J. J. and G{\'o}mez, G. and
Macau, Elbert Einstein Nehrer and Winter, O. C.",
affiliation = "{Universidade Estadual Paulista (UNESP)} and ETSEIB-UPC and
Departament de Matem{\`a}tica Aplicada i An{\`a}lisi, UB and
{Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Universidade Estadual Paulista (UNESP)}",
title = "Zero, minimum and maximum relative radial acceleration for planar
formation flight dynamics near triangular libration points in the
Earth-Moon system",
journal = "Advances in Space Research",
year = "2014",
volume = "54",
number = "9",
pages = "1838--1857",
abstract = "Assume a constellation of satellites is flying near a given
nominal trajectory around L4 or L5 in the Earth-Moon system in
such a way that there is some freedom in the selection of the
geometry of the constellation. We are interested in avoiding large
variations of the mutual distances between spacecraft. In this
case, the existence of regions of zero and minimum relative radial
acceleration with respect to the nominal trajectory will prevent
from the expansion or contraction of the constellation. In the
other case, the existence of regions of maximum relative radial
acceleration with respect to the nominal trajectory will produce a
larger expansion and contraction of the constellation. The goal of
this paper is to study these regions in the scenario of the
Circular Restricted Three Body Problem by means of a linearization
of the equations of motion relative to the periodic orbits around
L4 or L5. This study corresponds to a preliminar planar formation
flight dynamics about triangular libration points in the
Earth-Moon system. Additionally, the cost estimate to maintain the
constellation in the regions of zero and minimum relative radial
acceleration or keeping a rigid configuration is computed with the
use of the residual acceleration concept. At the end, the results
are compared with the dynamical behavior of the deviation of the
constellation from a periodic orbit.",
doi = "10.1016/j.asr.2014.07.018",
url = "http://dx.doi.org/10.1016/j.asr.2014.07.018",
issn = "0273-1177 and 1879-1948",
label = "scopus 2014-11 SalazarMasG{\'o}mMacWin:2014:ZeMiMa",
language = "en",
urlaccessdate = "11 maio 2024"
}