| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3KbR |
| Repository | sid.inpe.br/iris@1905/2005/08.04.02.17 (restricted access) |
| Last Update | 2015:11.18.11.57.34 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.02.17.42 |
| Metadata Last Update | 2021:02.11.18.10.11 (UTC) administrator |
| Secondary Key | INPE-8061-PRE/3877 |
| Label | 9007 |
| Citation Key | CostaPrad:2000:OrEvSa |
| Title | Orbital evolution of a satellite perturbed third-body  |
| Format | ISBN:85-901487-1-8 |
| Year | 2000 |
| Secondary Date | 20010416 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LI |
| Number of Files | 1 |
| Size | 131 KiB |
| 2. Context | |
| Author | 1 Costa, Ione Vicente 2 Prado, Antonio Fernando Bertachini de Almeida |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Prado, Antonio Fernando Bertachini de Almeida, ED. |
| Book Title | Colóquio Brasileiro de Dinâmica Orbital, 9 Advances in Space Dynamics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 176-194 |
| Series Title | Advances in Space Dynamics |
| History (UTC) | 2014-09-29 15:09:03 :: administrator -> marciana :: 2000 2015-11-18 11:57:34 :: marciana -> administrator :: 2000 2021-02-11 18:10:11 :: administrator -> :: 2000 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL astrodinâmica trajetórias espaciais mecânica celeste manobras de orbitas astrodynamics space mechanics spacecraft trajectories orbital maneuvers |
| Abstract | This paper has the goal of developing a semi-analytical study of the perturbation caused in a spacecraft by a third body involved in the dynamics. One of the important applications of the present research is to calculate the effect of Lunar and Solar perturbations on high-altitude Earth satellites. There is a special interest to see under which conditions a near-circular orbit remains near-circular. The so called "critical angle of the third-body perturbation," that is a value for the inclination such that any near-circular orbit with inclination below this value remains near-circular, is discussed in detail. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital evolution 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 | 2000_costa.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 |