| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/GUKAo |
| Repository | sid.inpe.br/iris@1905/2005/07.29.22.33.54 (restricted access) |
| Last Update | 2018:08.29.12.16.46 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/07.29.22.34 |
| Metadata Last Update | 2021:02.11.18.09.43 (UTC) administrator |
| Secondary Key | INPE-8040-PRE/3856 |
| Label | 8992 |
| Citation Key | SchulzPradMora:2000:OrChUs |
| Title | Orbital changes using atmospheric maneuvers  |
| Format | ISBN:901487-1-8 |
| Year | 2000 |
| Secondary Date | 20010416 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 86 KiB |
| 2. Context | |
| Author | 1 Schulz, Walkiria 2 Prado, Antonio Fernando Bertachini de Almeida 3 Moraes, Rodolpho Vilhena de |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Prado, Antonio Fernando Bertachini de Almeida. |
| Book Title | Colóquio Brasileiro de Dinâmica Orbital, 9 Orbital changes using atmospheric maneuvers |
| Pages | 368-378 |
| Series Title | Orbital changes using atmospheric maneuvers |
| History (UTC) | 2018-06-06 03:53:23 :: administrator -> marciana :: 2000 2018-08-29 12:16:48 :: marciana -> administrator :: 2000 2021-02-11 18:09:43 :: administrator -> :: 2000 |
| 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 | ENGENHARIA E TECNOLOGIA ESPACIAL ASTRODINÂMICA TRAJETÓRIAS ESPACIAIS MECÂNICA CELESTE MANOBRAS ORBITAIS ASTRODYNAMICS SPCECRAFT TRAJECTORIES CELESTIAL MECHANICS ORBITAL MANEUVERS |
| Abstract | The study of atmospheric maneuvers for satellites is an important aspect of the exploration of planets surfaces and atmospheres. To take more advantage of the gains due to atmospheric maneuvers, we need to develop an optimal control law to maneuver the satellite. This control law should minimize the fuel consumption required by the velocity variation due to engines on board the satellite. With this in mind, the aim of the present work is to establish what is the performance gain that can be achieved using aerodynamic forces combined with propulsive ones, with the objective of changing a satellite orbital plane around the Earth. Results of several simulations are presented. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital changes using... |
| 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 | schulz_orbital.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 city 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 publisher readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url volume |