@InProceedings{MarquesMoniKuga:2005:AnCoMo,
author = "Marques, Haroldo Antonio and Monico, Jo{\~a}o Francisco Galera
and Kuga, H{\'e}lio Koiti",
title = "An{\'a}lise comparativa dos modelos de press{\~a}o de
radia{\c{c}}{\~a}o solar nos sat{\'e}lites GPS",
booktitle = "Anais...",
year = "2005",
pages = "6",
organization = "Col{\'o}quio Brasileiro de Ci{\^e}ncias Geod{\'e}sicas, 4.
(CBCG).",
keywords = "GPS, {\'o}rbitas dos sat{\'e}lites, press{\~a}o de
radia{\c{c}}{\~a}o solar, IGS (international GPS service),
satellites orbits, solar radiation pressure.",
abstract = "A determina{\c{c}}{\~a}o das {\'o}rbitas dos sat{\'e}lites
artificiais {\'e} fundamental para a Geod{\'e}sia. Para a
realiza{\c{c}}{\~a}o deste processo {\'e} necess{\'a}rio,
primeiramente, fazer uma modelagem precisa das v{\'a}rias
for{\c{c}}as ou perturba{\c{c}}{\~o}es que atuam nos
sat{\'e}lites. Estas for{\c{c}}as incluem as gravitacionais e as
n{\~a}o-gravitacionais, que reunidas num vetor
acelera{\c{c}}{\~a}o total, deve ser integrado numericamente em
um sistema de refer{\^e}ncia inercial, uma vez para obter a
velocidade e duas, para obter a posi{\c{c}}{\~a}o dos
sat{\'e}lites. No caso das for{\c{c}}as gravitacionais
t{\^e}m-se as perturba{\c{c}}{\~o}es causadas pela
arra{\c{c}}{\~a}o gravitacional da Terra, Lua e Sol, al{\'e}m
das mar{\'e}s oce{\^a}nicas e terrestres, enquanto que nas
n{\~a}o-gravitacionais est{\~a}o inclu{\'{\i}}das as
for{\c{c}}as de superf{\'{\i}}cie (atrito do ar, press{\~a}o
de radia{\c{c}}{\~a}o solar e radia{\c{c}}{\~a}o
infravermelha), al{\'e}m de outras for{\c{c}}as perturbadoras.
Na Faculdade de Ci{\^e}ncias e Tecnologia - FCT/UNESP, est{\'a}
dispon{\'{\i}}vel o G{\'A}S (GPS Analysis Software) (Monico,
1995 e Stewart et ai., 1994), o qual disp{\~o}e do aplicativo
GPSORBIT para integra{\c{c}}{\~a}o de {\'o}rbitas. Este
aplicativo est{\'a} em fase de atualiza{\c{c}}{\~o}es, sendo
uma delas a implementa{\c{c}}{\~a}o de modelos de press{\~a}o
de radia{\c{c}}{\~a}o solar e, neste trabalho foi analisada a
influ{\^e}ncia dessa perturba{\c{c}}{\~a}o na
integra{\c{c}}{\~a}o das {\'o}rbitas dos sat{\'e}lites GPS,
al{\'e}m de uma an{\'a}lise comparativa do modelo conhecido como
Bola de Canh{\~a}o (Cannon Bali) com o modelo ROCK 42. -->
ABSTRACT: The artificial satellites orbit determination is
fundamental to Geodesy. For realization of this process it is
needed, first, a precise modeling of the many forces and
perturbations acting on the satellite. These forces include the
gravitational and non-gravitational ones that considered in the
resulting acceleration vector, must be integrated by a numerical
process in the inertial reference system, once to obtain the
velocity and twice for the satellite positions. In the cases of
the gravitational force the perturbations are had caused by the
gravitational attraction of the Earth, Moon and Sun, besides the
oceanic and terrestrial tides, while in the non-gravitational ones
the surface force are included (attrition of the air, solar
radiation pressure and infrared radiation), besides other
perturbation forces. In the Faculdade de Ci{\^e}ncias e
Tecnologia -FCT/UNESP, is available the G{\'A}S (GPS Analysis
Software) (Monico, 1995 and Stewart et ai., 1994), that h{\'a}s
the GPSORBIT application module for orbit integration. This module
is being updated with the radiation pressure models implementation
and in this paper it was analyzed the influence of such
perturbation in the GPS satellites orbits integration, besides a
comparative analysis of the model known by {"}Cannon Bali{"} with
the ROCK 42 model.",
conference-location = "Curitiba",
conference-year = "16 a 20 de maio",
copyholder = "SID/SCD",
language = "pt",
targetfile = "42tmarquesmk.pdf",
urlaccessdate = "19 abr. 2024"
}