@Article{MacêdoRocc:2019:EvOrDe,
author = "Mac{\^e}do, Carlos Frederico de Carvalho and Rocco, Evandro
Marconi",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Evaluation of orbital decay of a satellite at low altitude due to
atmospheric drag as a function of solar activity",
journal = "Journal of Physics: Conference Series",
year = "2019",
volume = "1365",
pages = "012027",
note = "{XIX Brazilian Colloquium on Orbital Dynamics 2018}",
keywords = "Astrodynamics, Orbital Motion, Spaceflight Dynamics, Aeroassisted
Maneuvers, Orbital Perturbation.",
abstract = "Artificial satellites in low Earth orbit have as main disturbance
the atmospheric drag, which is a non-conservative disturbance that
causes the satellite to lose orbital energy due to the friction
with the air. Basically, the drag force is a function of the
velocity, the local air density and the satellites constructive
parameters. The air density is a function of altitude, longitude,
latitude, geomagnetic index and solar activity. Solar storms are
responsible for a wide range of terrestrial effects, especially in
damage to telecommunications systems. Another relevant effect of
solar activity is the variation in the volume of the atmosphere
and consequently in the value of the air density for a given
altitude, longitude and latitude. This work provides an initial
approach, through simulation, in the engineering effort to deal
with this disturbance.",
doi = "10.1088/1742-6596/1365/1/012027",
url = "http://dx.doi.org/10.1088/1742-6596/1365/1/012027",
issn = "1742-6588",
label = "lattes: 0088337156908774 2 Mac{\^e}doRocc:2019:EvOrDe",
language = "en",
targetfile = "macedo_evaluation.pdf",
urlaccessdate = "27 abr. 2024"
}