@InCollection{SolórzanoPrad:2004:ThPeUs,
author = "Sol{\'o}rzano, Carlos Renato Huaura and Prado, Antonio Fernando
Bertachini de Almeida",
title = "Third-body perturbation using a single averaged model.",
booktitle = "Advances in space dynamics 4: celestial mechanics and
astronautics",
publisher = "INPE",
year = "2004",
editor = "Kuga, H{\'e}lio Koiti",
pages = "47--56",
address = "S{\~a}o Jos{\'e} dos Campos",
keywords = "SPACE MECHANICS AND CONTROL, Three body problem, Spacecraft,
Perturbation, Lunar effects, Satellites, MEC{\^A}NICA ESPACIAL E
CONTROLE, Problema dos tr{\^e}s corpos, Nave espacial,
Perturba{\c{c}}{\~a}o, Efeitos lunares, Sat{\'e}lites.",
abstract = "Several papers studied the effect of the third body perturbation
in a spacecrafts, usually working with the Hamiltonian of the
system or with the disturbing function expressed in an analytic
manner. The present paper has the goal of developing a
semi-analytical study of the perturbation caused in a spacecraft
by a third body with a single averaged model to eliminate the
terms due to the short time periodic motion of the spacecraft.
Several plots will show the time histories of the Keplerian
elements of the orbits involved. One of the most important
applications is to calculate the effect of Lunar and Solar
perturbations on high-altitude Earth satellites.",
affiliation = "{Instituto Nacional de Pesquisas Espaciais. Divis{\~a}o de
Mec{\^a}nica Espacial e Controle (INPE.DMC)}",
copyholder = "SID/SCD",
language = "en",
ibi = "sid.inpe.br/marciana/2004/09.13.16.32",
url = "http://urlib.net/ibi/sid.inpe.br/marciana/2004/09.13.16.32",
targetfile = "Third-Body.pdf",
urlaccessdate = "21 maio 2024"
}