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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m21d.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34T/475T7LL
Repositóriosid.inpe.br/mtc-m21d/2022/06.22.15.21
Repositório de Metadadossid.inpe.br/mtc-m21d/2022/06.22.15.21.26
Última Atualização dos Metadados2023:01.03.16.46.08 (UTC) administrator
Chave SecundáriaINPE--PRE/
Chave de CitaçãoSantosSantPrad:2022:StFoFl
TítuloStudy of Formation Flying Topologies for a Geolocation Space Mission Composed of Three CubeSats Satellites
Ano2022
Data de Acesso29 jun. 2024
Tipo SecundárioPRE CI
2. Contextualização
Autor1 Santos, leonardo Moreira dos
2 Santos, Willer
3 Prado, Antonio Fernando Bertachini de Almeida
Identificador de Curriculo1
2
3 8JMKD3MGP5W/3C9JGJA
Grupo1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
2
3 DIMEC-CGCE-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Tecnológico da Aeronáutica (ITA)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 leonardo.msantos16@gmail.com
2
3 antonio.prado@inpe.br
Nome do EventoInternational Workshop on Satellite Constellations and Forming Flying (IWSCFF), 11
Localização do EventoMilano, Italy
Data7-10 June 2022
Histórico (UTC)2022-06-22 15:21:26 :: simone -> administrator ::
2023-01-03 16:46:08 :: administrator -> simone :: 2022
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Palavras-ChaveFormation Flying missions
Constellation missions
Earth-bounded Missions
ResumoA 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.
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4. Condições de acesso e uso
Idiomaen
Grupo de Usuáriossimone
Visibilidadeshown
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/46KTFK8
Acervo Hospedeirourlib.net/www/2021/06.04.03.40
6. Notas
Campos Vaziosarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn label lineage mark mirrorrepository nextedition notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark tertiarytype type url versiontype volume
7. Controle da descrição
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