1. Identificação | |
Tipo de Referência | Artigo em Evento (Conference Proceedings) |
Site | mtc-m21d.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34T/47LCLMS |
Repositório | sid.inpe.br/mtc-m21d/2022/09.19.14.19 |
Última Atualização | 2022:09.19.14.19.59 (UTC) simone |
Repositório de Metadados | sid.inpe.br/mtc-m21d/2022/09.19.14.19.59 |
Última Atualização dos Metadados | 2023:01.03.16.46.16 (UTC) administrator |
Chave Secundária | INPE--PRE/ |
Chave de Citação | NegriPradChagMora:2022:SiDoAn |
Título | Six dof analysis for asteroid autonomous exploration |
Ano | 2022 |
Data de Acesso | 12 maio 2024 |
Tipo Secundário | PRE CI |
Número de Arquivos | 1 |
Tamanho | 36 KiB |
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2. Contextualização | |
Autor | 1 Negri, Rodolfo Batista 2 Prado, Antonio Fernando Bertachini de Almeida 3 Chagas, Ronan Arraes Jardim 4 Moraes, Rodolpho |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JGJA |
Grupo | 1 2 DIMEC-CGCE-INPE-MCTI-GOV-BR 3 DISEP-CGCE-INPE-MCTI-GOV-BR |
Afiliação | 1 Universidade Estadual Paulista (UNESP) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) |
Endereço de e-Mail do Autor | 1 rodolfobnegri@yahoo.com.br 2 antonio.prado@inpe.br 3 ronan.arraes@inpe.br |
Nome do Evento | International Astronautical Congress, 73 |
Localização do Evento | Paris, France |
Data | 18-22 Sept. 2022 |
Editora (Publisher) | IAF |
Histórico (UTC) | 2022-09-19 14:19:59 :: simone -> administrator :: 2023-01-03 16:46:16 :: administrator -> simone :: 2022 |
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3. Conteúdo e estrutura | |
É a matriz ou uma cópia? | é a matriz |
Estágio do Conteúdo | concluido |
Transferível | 1 |
Tipo do Conteúdo | External Contribution |
Resumo | The autonomy in asteroid missions has gained particular attention in the last years. Reference [1] shows that a bolder approach, taking full advantage of the spacecraft autonomy, is possible by using a robust guidance to deal with the uncertain asteroid environment, with no need to maintain the same conservative approach applied in other works. Although the time constants in an asteroid environment are usually large, allowing the spacecraft to make sparse measurements in hours, with plenty of time to execute other required maneuvers, it is worth investigating the coupling between attitude and guidance to assess if any undesired behavior derives from it. That investigation is especially needed in an operational profile such as the proposed by Reference [1], which might present frequent control activity for trajectory correction and orbital maintenance. This work makes a six degree of freedom (DOF) analysis for the GNC approach proposed in Reference [1]. For that sake, we consider a spacecraft equipped with a LIDAR and two optical navigation cameras on its -z body-fixed frame panel, twelve thrusters are used for attitude control and guidance (similar to Hayabusa 2), and four reaction wheels. A fixed solar panel is considered, which simplifies the spacecraft design and removes points for failure, increasing the robustness of the mission. Uncertainties in the attitude are modeled accordingly to the noise level of the IMU LN-200S of the Northrop Grumman, the same used in the OSIRIS-REx mission. The attitude control algorithm aims to point the solar panels towards the Sun to recharge the batteries while executing the required guidance maneuvers. The orbital maintenance in close proximity to the asteroid is made using the control proposed by Reference [2]. The spacecraft also needs to point its LIDAR and optical cameras to the asteroid once every hour for the measurement used in the trajectory estimation. Preliminary considerations and specificities in operating about binary asteroids are also made. Reaction wheels desaturation maneuvers are planned and investigated. The results draw guidelines for further developments in the autonomous exploration of the challenging environments of small bodies. |
Área | ETES |
Arranjo | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Six dof analysis... |
Conteúdo da Pasta doc | acessar |
Conteúdo da Pasta source | não têm arquivos |
Conteúdo da Pasta agreement | |
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4. Condições de acesso e uso | |
URL dos dados | http://urlib.net/ibi/8JMKD3MGP3W34T/47LCLMS |
URL dos dados zipados | http://urlib.net/zip/8JMKD3MGP3W34T/47LCLMS |
Idioma | en |
Arquivo Alvo | IAC-22,C1,IPB,36,x67873.brief.pdf |
Grupo de Usuários | simone |
Visibilidade | shown |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/46KTFK8 |
Lista de Itens Citando | sid.inpe.br/mtc-m21/2012/07.13.14.40.20 3 |
Acervo Hospedeiro | urlib.net/www/2021/06.04.03.40 |
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6. Notas | |
Campos Vazios | archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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