Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3MPQGU5
Repositorysid.inpe.br/mtc-m21b/2016/11.11.18.32   (restricted access)
Last Update2016:11.11.18.32.25 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/11.11.18.32.25
Metadata Last Update2021:07.28.22.52.22 (UTC) administrator
DOI10.1007/s40314-015-0256-x
ISSN2238-3603
Citation KeyGomesMurcPradGole:2016:AtClAp
TitleAtmospheric close approaches with the Earth considering drag and lift forces
Year2016
MonthOct.
Access Date2024, Apr. 20
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1147 KiB
2. Context
Author1 Gomes, Vivian Martins
2 Murcia Pineros, Jhonathan Orlando
3 Prado, Antonio Fernando Bertachini de Almeida
4 Golebiewska, Justyna
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1
2 CMC-ETES-SPG-INPE-MCTI-GOV-BR
3 DSE-ETE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Adam Mickiewicz University
Author e-Mail Address1 vivianmartinsgomes@gmail.com
2 jhonathan.pineros@inpe.br
3 antonio.prado@inpe.br
4 jg@amu.edu.pl
JournalComputational and Applied Mathematics
Volume35
Number3
Pages817-833
History (UTC)2016-11-11 18:33:12 :: simone -> administrator :: 2016
2021-07-28 22:52:22 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodynamics
Swing-by
Orbital maneuvers
Aero-gravity maneuver
Close approach
AbstractA maneuver called "Aero-Gravity Assisted" is known in the literature to increase the energy gains given by a close approach between a spacecraft and a planet using the atmosphere of the planet. In a sequence of studies related to this problem, the present paper studies close approaches between a spacecraft and the Earth, in situations where the passage is close enough to the surface of the Earth such that the spacecraft crosses its atmosphere. The dynamical model considers the atmosphere of the Earth, in terms of drag and lift, the gravitational fields of the Earth and the Sun, assumed to be points of mass, and the spacecraft. The Earth and the Sun are assumed to be in circular coplanar orbits around their common center of mass. The equations of motion are the ones given by the circular planar restricted three-body problem with the addition of the forces generated by the atmospheric drag and lift. The primary objective is to map the variations of energy of the orbits of the spacecraft due to this close approach. The results show how the atmosphere affects the trajectory of the spacecraft, generating situations where the variation of energy changes sign with respect to the gravity part of the maneuver or where they have a zero net result, based in the equilibrium between atmospheric and gravity forces. This result opens the possibility of changing only the eccentricity of the orbit, keeping fixed its semi-major axis.
AreaETES
Arrangement 1urlib.net > Produção pgr ATUAIS > CMC > Atmospheric close approaches...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDSE > Atmospheric close approaches...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 11/11/2016 16:32 1.0 KiB 
4. Conditions of access and use
Languageen
Target Filegomes_atmospheric.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AUSL
Citing Item Listsid.inpe.br/bibdigital/2013/10.14.00.13 2
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1
sid.inpe.br/bibdigital/2021/02.11.20.54 1
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
e-Mail (login)simone
update 


Close