1. Identity statement | |
Reference Type | Conference Paper (Conference Proceedings) |
Site | mtc-m21b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34P/3KH6J52 |
Repository | sid.inpe.br/mtc-m21b/2015/11.04.15.00 |
Last Update | 2015:11.04.15.01.30 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m21b/2015/11.04.15.00.52 |
Metadata Last Update | 2021:02.11.18.19.55 (UTC) administrator |
Secondary Key | INPE--PRE/ |
Citation Key | GonçalvesRoccMora:2015:OrMaLu |
Title | Orbital maneuvers of a lunar artificial satellite, under the action of gravitational and non-gravitational perturbation forces |
Year | 2015 |
Access Date | 2024, May 14 |
Secondary Type | PRE CI |
Number of Files | 1 |
Size | 323 KiB |
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2. Context | |
Author | 1 Gonçalves, Liana Dias 2 Rocco, Evandro Marconi 3 Moraes, Rodolpho Vilhena de |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JH37 |
Group | 1 CMC-ETES-SPG-INPE-MCTI-GOV-BR 2 DMC-ETE-INPE-MCTI-GOV-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Universidade Federal de São Paulo (UNIFESP) |
Author e-Mail Address | 1 lianadgon@gmail.com 2 evandro.rocco@inpe.br 3 rodolpho.vilhena@gmail.com |
Conference Name | International Symposium on Space Flight Dynamics, 25 |
Conference Location | Munich, Germany |
Date | 19-23 Oct. |
Book Title | Proceedings |
History (UTC) | 2015-11-04 15:00:52 :: simone -> administrator :: 2021-02-11 18:19:55 :: administrator -> simone :: 2015 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Version Type | finaldraft |
Keywords | Astrodynamics Orbital Maneuvers Continuous Thrust Perturbations |
Abstract | The objective of this study is to analyze the orbital maneuvers of an artificial satellite around the Moon surface subject to perturbative forces of gravitational and not gravitational origin, such as lunar gravitational potential, gravitational attraction of the Earth and the Sun, lunar albedo and solar radiation pressure. Optimal maneuvers were obtained from the Lambert's problem solution (Two Point Boundary Value Problem) in order that is minimized the fuel consumption. Then a selected maneuver was simulated assuming a more realistic model of the propulsion system. For both cases is analyzed the actions of thrusters, fuel consumption and deviations in the orbital elements that characterize the lunar orbit of artificial satellite. The deviation is obtained by a comparison between the actual state and the reference state of the vehicle at each step of the simulation. The actual state is calculated every step of the simulation and the reference state is determined considering the desired final orbital elements for the trajectory. |
Area | ETES |
Arrangement 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Orbital maneuvers of... |
Arrangement 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital maneuvers of... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
data URL | http://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3KH6J52 |
zipped data URL | http://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3KH6J52 |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Read Permission | allow from all |
Update Permission | not transferred |
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5. Allied materials | |
Mirror Repository | urlib.net/www/2011/03.29.20.55 |
Next Higher Units | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/446AF4B |
Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.14.45.41 6 |
Host Collection | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
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6. Notes | |
Empty Fields | archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn label language lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject targetfile tertiarymark tertiarytype type url volume |
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7. Description control | |
e-Mail (login) | simone |
update | |
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