@Article{MouraJúniorCelePrad:2018:DeOpCo,
author = "Moura J{\'u}nior, O. and Celestino, C. C. and Prado, Antonio
Fernando Bertachini de Almeida",
affiliation = "{Universidade Federal do ABC (UFABC)} and {Universidade Federal do
ABC (UFABC)} and {Instituto Nacional de Pesquisas Espaciais
(INPE)}",
title = "Determination of the optimal conditions for inclination maneuvers
using a Swing-by",
journal = "Astrophysics and Space Science",
year = "2018",
volume = "363",
number = "5",
pages = "e91",
month = "may",
keywords = "Swing-by · Orbital maneuvers · Changing of orbital plane ·
Astrodynamics.",
abstract = "The search for methods to reduce the fuel consumption in orbital
transfers is something relevant and always current in
astrodynamics. Therefore, the maneuvers assisted by the gravity,
also called Swing-by maneuvers, can be an advantageous option to
save fuel. The proposal of the present research is to explore the
influence of some parameters in a Swing-by of an artificial
satellite orbiting a planet with one of the moons of this mother
planet, with the goal of changing the inclination of the
artificial satellite around the main body of the system. The fuel
consumption of this maneuver is compared with the required
consumption to perform the same change of inclination using the
classical approach of impulsive maneuvers.",
doi = "10.1007/s10509-018-3308-z",
url = "http://dx.doi.org/10.1007/s10509-018-3308-z",
issn = "0004-640X",
language = "en",
urlaccessdate = "26 abr. 2024"
}