| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3JHg |
| Repository | sid.inpe.br/iris@1905/2005/08.04.01.57 (restricted access) |
| Last Update | 2019:01.16.16.09.40 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.01.57.27 |
| Metadata Last Update | 2021:02.11.18.10.06 (UTC) administrator |
| Secondary Key | INPE-9528-PRE/5181 |
| Label | 10457 |
| Citation Key | RoccoSouzPrad:2002:StKeSa |
| Title | Station Keeping of Satellite Constellation with time contraint using optimal bi-impulsive maneuvers  |
| Format | ISBN 85-17-00006-4 |
| Year | 2002 |
| Secondary Date | 20021213 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 5815 KiB |
| 2. Context | |
| Author | 1 Rocco, Evandro Marconi 2 Souza, Marcelo Lopes de Oliveira e 3 Prado, Antonio Fernando Bertachini de Almeida |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida |
| Book Title | Advances in space dynamics 3: applications in astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 238-256 |
| Series Title | Advances in space dynamics 3: applications in astronautics |
| History (UTC) | 2008-06-09 21:40:46 :: administrator -> jefferson :: 2012-08-02 17:55:01 :: jefferson -> administrator :: 2019-01-16 16:08:59 :: administrator -> simone :: 2002 2019-01-16 16:09:41 :: simone -> administrator :: 2002 2021-02-11 18:10:06 :: administrator -> :: 2002 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL orbital maneuvers constellations of satellites fuel consumption impulsive maneuvers time constraint stationkeeping |
| Abstract | In this work we study the problem of orbital station keeping maneuvers of symmetrical constellations of satellites with minimum fuel consumption using impulsive maneuvers with time constraint. This time constraint imposes a new characteristic to the problem, that rules out the majority of the transfer methods available in the literature. Due to the satellites constraints, we have the problem of simultaneously optimizing the maneuver for n satellites. Thus, the goal of this work is to formulate and to study maneuver strategies that, in some way, make it possible to obtain solutions with small fuel consumption and time constraint considering all the satellites in the constellation, thus we have a multi-objective problem. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Station Keeping of... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Target File | INPE-9528.pdf |
| User Group | administrator |
| Visibility | shown |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
| 6. Notes | |
| Empty Fields | affiliation archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |