@Article{FerreiraKugaPradWint:2015:EsTrSp,
author = "Ferreira, A. Ferraz Silva and Kuga, H{\'e}lio Koiti and Prado,
Antonio Fernando Bertachini de Almeida and Winter, O. C.",
affiliation = "{} and {Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Universidade Estadual Paulista (UNESP)}",
title = "Estimating the trajectory of a space vehicle passing by the Moon
using Kalman Filter",
journal = "Journal of Physics: Conference Series",
year = "2015",
volume = "641",
pages = "012002",
keywords = "Astrodin{\^a}mica.",
abstract = "The trajectory of a spacecraft going to the periapsis of its orbit
around the smaller body of a binary system is estimated from the
observed data using a Kalman Filter. Simulations of the
trajectories will be made to generate the data of the spacecraft
position. When observed from the Earth, using a fixed star as a
reference, we have the spacecraft position as an angle function
\ϕ. This is the angle between spacecraft position vector and
the star position vector. The result shows that Kalman Filter can
be used successfully for trajectory estimation, if adequate
accuracy is available for the angle observations.",
doi = "10.1088/1742-6596/641/1/012002",
url = "http://dx.doi.org/10.1088/1742-6596/641/1/012002",
issn = "1742-6588",
label = "lattes: 7340081273816424 3 FerreiraKugaPradWint:2015:EsTrSp",
language = "pt",
targetfile = "1_ferreira3.pdf",
urlaccessdate = "02 maio 2024"
}