Close

1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/47LCLMS
Repositorysid.inpe.br/mtc-m21d/2022/09.19.14.19
Last Update2022:09.19.14.19.59 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/09.19.14.19.59
Metadata Last Update2023:01.03.16.46.16 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyNegriPradChagMora:2022:SiDoAn
TitleSix dof analysis for asteroid autonomous exploration
Year2022
Access Date2024, May 13
Secondary TypePRE CI
Number of Files1
Size36 KiB
2. Context
Author1 Negri, Rodolfo Batista
2 Prado, Antonio Fernando Bertachini de Almeida
3 Chagas, Ronan Arraes Jardim
4 Moraes, Rodolpho
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1
2 DIMEC-CGCE-INPE-MCTI-GOV-BR
3 DISEP-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 rodolfobnegri@yahoo.com.br
2 antonio.prado@inpe.br
3 ronan.arraes@inpe.br
Conference NameInternational Astronautical Congress, 73
Conference LocationParis, France
Date18-22 Sept. 2022
PublisherIAF
History (UTC)2022-09-19 14:19:59 :: simone -> administrator ::
2023-01-03 16:46:16 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractThe 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.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Six dof analysis...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 19/09/2022 11:19 1.0 KiB 
4. Conditions of access and use
data URLhttp://mtc-m21d.sid.inpe.br/ibi/8JMKD3MGP3W34T/47LCLMS
zipped data URLhttp://mtc-m21d.sid.inpe.br/zip/8JMKD3MGP3W34T/47LCLMS
Languageen
Target FileIAC-22,C1,IPB,36,x67873.brief.pdf
User Groupsimone
Visibilityshown
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/46KTFK8
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.40.20 3
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
Empty Fieldsarchivingpolicy 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
7. Description control
e-Mail (login)simone
update 


Close