| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3JLC |
| Repository | sid.inpe.br/iris@1905/2005/08.04.02.00 (restricted access) |
| Last Update | 2015:11.19.15.12.14 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.02.00.24 |
| Metadata Last Update | 2021:02.11.18.10.07 (UTC) administrator |
| Secondary Key | INPE-9532-PRE/5185 |
| Label | 10460 |
| Citation Key | ChiaradiaPradKuga:2002:AuCoOr |
| Title | Autonomous coplanar orbital maneuver using GPS systems  |
| Format | ISBN 85-17-00006-4 |
| Year | 2002 |
| Secondary Date | 20021213 |
| Access Date | 2024, May 05 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 68 KiB |
| 2. Context | |
| Author | 1 Chiaradia, Ana Paula Marins 2 Prado, Antonio Fernando Bertachini de Almeida 3 Kuga, Hélio Koiti |
| 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 | 286-279 |
| Series Title | Advances in space dynamics 3: applications in astronautics |
| History (UTC) | 2008-06-09 21:40:53 :: administrator -> jefferson :: 2012-08-02 17:55:04 :: jefferson -> administrator :: 2015-11-19 15:11:46 :: administrator -> simone :: 2002 2015-11-19 15:12:14 :: simone -> administrator :: 2002 2021-02-11 18:10:07 :: 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 autonomou Lambert method artificial satellite real time Kalaman Filtering artificial satellite |
| Abstract | Three algorithms are tested to calculate and perform autonomous orbital maneuvers in satellite. One of them is implemented and tested numerically. Some of in this algorithm are performed for use in real-time onboard applications. First of all, a simplified and compact algorithm is used to estimate in real-time and on board the artificial satellite orbit, using the GPS measurements. By using the, estimated orbit as the initial one and the information of the final orbit, a coplanar bi-impulsive maneuver is calculated. This maneuver searches for the minimum fuel consumption. To solve this problem, the "Minimum Delta-V Lambert Problem" is used. Two kinds of maneuvers are performed, one varying the semimajor axis and the other varying the semimajor axis and the eccentricity, simultaneously. The obtained results are always according to the expected results. The possibilities of restrictions in the locations to apply the impulses are included, as well as the possibility to control the relation between the processing time and the solution accuracy. They are the two main reasons to recommend this method for use in the proposed application. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Autonomous coplanar orbital... |
| 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 | chiaradia.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 |