| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16b.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZGivnK2Y/NqFsE |
| Repository | sid.inpe.br/mtc-m17@80/2006/12.11.12.12 (restricted access) |
| Last Update | 2006:12.11.12.12.09 (UTC) administrator |
| Metadata Repository | sid.inpe.br/mtc-m17@80/2006/12.11.12.12.10 |
| Metadata Last Update | 2021:02.11.18.11.44 (UTC) administrator |
| Secondary Key | INPE-14435-PRE/9515 |
| ISSN | 1024-123X 1563-5147 |
| Citation Key | TorresPrad:2006:ChInEa |
| Title | Changing inclination of earth satellites using the gravity of the moon  |
| Project | Dinâmica Órbital |
| Year | 2006 |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 1461 KiB |
| 2. Context | |
| Author | 1 Torres, K. S. 2 Prado, Antonio Fernando Bertachini de Almeida |
| Resume Identifier | 1 2 8JMKD3MGP5W/3C9JGJA |
| Group | 1 DMC-INPE-MCT-BR 2 DMC-INPE-MCT-BR |
| Affiliation | 1 2 Instituto Nacional de Pesquisas Espaciais (INPE) |
| Author e-Mail Address | 1 2 prado@dem.inpe.br |
| Journal | Mathematical Problems in Engineering |
| Volume | ID 13690 |
| Pages | 1-13 |
| History (UTC) | 2007-03-20 12:48:48 :: vinicius -> administrator :: 2008-06-29 02:29:54 :: administrator -> vinicius :: 2011-12-19 13:32:25 :: vinicius -> administrator :: 2012-11-24 01:39:42 :: administrator -> vinicius :: 2006 2013-02-20 16:29:36 :: vinicius -> administrator :: 2006 2021-02-11 18:11:44 :: administrator -> marciana :: 2006 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Version Type | publisher |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL controle de órbita orbital control gravity field Moon |
| Abstract | We analyze the problem of the orbital control of an Earth's satellite using the gravity of the Moon. The main objective is to study a technique to decrease the fuel consumption of a plane change maneuver to be performed in a satellite that is in orbit around the Earth. The main idea of this approach is to send the satellite to the Moon using a single-impulsive maneuver, use the gravity field of the Moon to make the desired plane change of the trajectory, and then return the satellite to its nominal semimajor axis and eccentricity using a bi-impulsive Hohmann-type maneuver. The satellite is assumed to start in a Keplerian orbit in the plane of the lunar orbit around the Earth and the goal is to put it in a similar orbit that differs from the initial orbit only by the inclination. A description of the close-approach maneuver is made in the three-dimensional space. Analytical equations based on the patched conics approach are used to calculate the variation in velocity, angular momentum, energy, and inclination of the satellite. Then, several simulations are made to evaluate the savings involved. The time required by those transfers is also calculated and shown. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Changing inclination 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 | |
| Language | en |
| Target File | torres-changing.pdf |
| User Group | administrator vinicius |
| Visibility | shown |
| Copy Holder | SID/SCD |
| Archiving Policy | denypublisher allowfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Dissemination | WEBSCI; PORTALCAPES; COMPENDEX. |
| Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
| 6. Notes | |
| Empty Fields | alternatejournal archivist callnumber copyright creatorhistory descriptionlevel doi e-mailaddress format isbn label lineage mark mirrorrepository month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |