@Article{SantosForm:2015:ApGeAl,
author = "Santos, Denilson Paulo Souza dos and Formiga, Jorge Kennety da
Silva",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Faculdade
de Tecnologia (FATEC)}",
title = "Application of a genetic algorithm in orbital maneuvers",
journal = "Computational and Applied Mathematics",
year = "2015",
volume = "34",
number = "2",
pages = "437--450",
month = "July",
keywords = "Orbital mechanics, Orbital transfers, Genetic algorithm, Space
maneuvers.",
abstract = "This paper has the goal of calculating transfer trajectories
between two coplanar orbits using several impulses, trying to find
solutions that reduce the costs related to the fuel consumption
required to apply these impulses. The number of impulses is given
a priori, and a genetic algorithm is used to find the maneuvers
that spent less fuel to be completed. Several types of maneuvers
are simulated, including constrained maneuvers, where the
spacecraft is forced to pass by intermediate orbits, and maneuvers
that transfer a spacecraft from one body back to the same body.
The method worked in all the situations and the maneuvers were
found in all the situations.",
doi = "10.1007/s40314-014-0151-x",
url = "http://dx.doi.org/10.1007/s40314-014-0151-x",
issn = "2238-3603",
language = "en",
targetfile = "santos_application.pdf",
urlaccessdate = "27 abr. 2024"
}