@Article{DeiennoMergPradSmir:2016:SaDeVi,
author = "Deienno, Rog{\'e}rio and Merguizo Sanchez, Diogo and Prado,
Antonio Fernando Bertachini de Almeida and Smirnov, Georgi",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)} and {University of Minho}",
title = "Satellite de-orbiting via controlled solar radiation pressure",
journal = "Celestial Mechanics and Dynamical Astronomy",
year = "2016",
volume = "126",
number = "4",
pages = "433--459",
month = "Nov.",
keywords = "Astrodynamics, Orbital maneuvers, Satellite de-orbiting, Solar
radiation pressure.",
abstract = "The goal of the present research was to study the use of solar
radiation pressure to place a satellite in an orbit that makes it
to re-enter the atmosphere of the Earth. This phase of the mission
is usual, since the orbital space around the Earth is crowded and
all satellites have to be discarded after the end of their
lifetimes. The technique proposed here is based on a device that
can increase and decrease the area-to-mass ratio of the satellite
when it is intended to reduce its altitude until a re-entry point
is reached. Equations that predict the evolution of the
eccentricity and semi-major axis of the orbit of the satellite are
derived and can be used to allow the evaluation of the time
required for the decay of the satellite. Numerical simulations are
made, and they show the time required for the decay as a function
of the area-to-mass ratio and the evolution of the most important
orbital elements. The results show maps that indicate regions of
fast decays as a function of the area-to-mass ratio and the
initial inclination of the orbit of the satellite. They also
confirmed the applicability of the equations derived here. The
numerical results showed the role played by the evection and the
Sun-synchronous resonances in the de-orbiting time.",
doi = "10.1007/s10569-016-9699-7",
url = "http://dx.doi.org/10.1007/s10569-016-9699-7",
issn = "0923-2958",
language = "en",
targetfile = "Deienno_satellite.pdf",
urlaccessdate = "23 abr. 2024"
}