| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16b.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZGivnK2Y/NqLiw |
| Repository | sid.inpe.br/mtc-m17@80/2006/12.11.15.58 (restricted access) |
| Last Update | 2006:12.11.15.58.24 (UTC) administrator |
| Metadata Repository | sid.inpe.br/mtc-m17@80/2006/12.11.15.58.25 |
| Metadata Last Update | 2021:02.11.18.11.50 (UTC) administrator |
| Secondary Key | INPE-14438-PRE/9518 |
| ISSN | 0100-7386 |
| Citation Key | Prado:2006:OrCoSa |
| Title | Orbital control of a satellite using the gravity of the Moon  |
| Project | Dinâmica Órbital |
| Year | 2006 |
| Month | Jan.- Mar. |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 158 KiB |
| 2. Context | |
| Author | Prado, Antonio Fernando Bertachini de Almeida |
| Resume Identifier | 8JMKD3MGP5W/3C9JGJA |
| Group | DMC-INPE-MCT-BR |
| Affiliation | Instituto Nacional de Pesquisas Espaciais (INPE) |
| Author e-Mail Address | prado@dem.inpe.br |
| Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
| Volume | 28 |
| Number | 1 |
| Pages | 105-110 |
| History (UTC) | 2007-03-20 12:57:58 :: vinicius -> administrator :: 2008-06-29 02:30:01 :: administrator -> vinicius :: 2011-05-29 09:26:50 :: vinicius -> administrator :: 2012-11-24 01:39:52 :: administrator -> vinicius :: 2006 2013-02-20 16:29:36 :: vinicius -> administrator :: 2006 2021-02-11 18:11:50 :: 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 |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL controle de órbita manobras orbitais Astrodynamics orbital maneuver swing-by |
| Abstract | In this paper, a study is made in 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 spacecraft 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 spacecraft to its nominal semi-major axis and eccentricity using a bi-impulsive Hohmann type maneuver. The spacecraft is assumed to start in a circular 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 threedimensional space. Analytical equations based in the patched conics approximation are used to calculate the variation in velocity, angular momentum, energy and inclination of the spacecraft that realizes this maneuver. Then, several simulations are made to evaluate the savings involved. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital control 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 | prado-orbital control.pdf |
| User Group | administrator vinicius |
| Visibility | shown |
| Copy Holder | SID/SCD |
| Archiving Policy | denypublisher denyfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Dissemination | WEBSCI; PORTALCAPES. |
| 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 documentstage doi e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |