@InProceedings{SantosSantPrad:2022:StFoFl,
author = "Santos, leonardo Moreira dos and Santos, Willer and Prado, Antonio
Fernando Bertachini de Almeida",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Tecnol{\'o}gico da Aeron{\'a}utica (ITA)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Study of Formation Flying Topologies for a Geolocation Space
Mission Composed of Three CubeSats Satellites",
year = "2022",
organization = "International Workshop on Satellite Constellations and Forming
Flying (IWSCFF), 11.",
keywords = "Formation Flying missions, Constellation missions, Earth-bounded
Missions.",
abstract = "A major motivation for the development of this study is the
ITASAT-2 mission of the Aeronautics Institute of Technology, whose
one of the main objectives is to be able to geolocate an
electromagnetic emitting source on the Earth's surface. For this,
the mission will have a formation flying of three CubeSats. The
topology and configuration must be chosen such that the
geolocation system presents the necessary precision, while the
other objectives of the mission are fulfilled. Thus, this study
intends to simulate various topologies by using the dynamics of
orbital motion and a geolocation algorithm based on combined
measurements of TDOA and FDOA. It is expected to obtain a base of
results that will assist the development team of the ITASAT-2
mission and related missions in choosing the best topology and
configurations for the formation flying. Therefore, this study
proves to be important as it demonstrates great potential of
contributions to the scientific and technical community of the
aerospace area. This scenario, therefore, serves as a motivation
for the development of the study presented here, which is also
based on the current development of the ITASAT-2 mission, by the
Technological Institute of Aeronautics (ITA) in collaboration, in
terms of research, with the National Institute of Space Research
(INPE) and researchers from Brazilian public universities. The
ITASAT-2 mission is designed to be composed of a formation flying
of three identical CubeSats 8U or even 12U. The main objectives of
the mission are: to conduct scientific and technological
investigations around the appearance and growth of irregularities
in the plasma structure of the ionosphere; and propose a specific
formation flying for the CubeSats so that they are able to locate
an electromagnetic emitting source on the Earth's surface. To
achieve the necessary requirements of the ITASAT-2 mission, it is
necessary to evaluate the possible topologies and configurations
for the formation that enable, at the same time, the study of the
space climate and the geolocation process.",
conference-location = "Milano, Italy",
conference-year = "7-10 June 2022",
language = "en",
urlaccessdate = "01 jun. 2024"
}