| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/GUomG |
| Repository | sid.inpe.br/iris@1905/2005/07.29.05.58.41 (restricted access) |
| Last Update | 2018:04.19.14.15.03 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/07.29.05.59.01 |
| Metadata Last Update | 2021:07.28.22.17.56 (UTC) administrator |
| Secondary Key | INPE-6731-PRE/2753 |
| ISSN | 0731-5090 1533-3884 |
| Label | 7896 |
| Citation Key | PradoBrou:1994:StHeOr |
| Title | Study of henon's orbit transfer problem using the Lambert algorithm  |
| Year | 1994 |
| Month | Sept. - Oct. |
| Access Date | 2024, May 08 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 893 KiB |
| 2. Context | |
| Author | 1 Prado, Antonio Fernando Bertachini de Almeida 2 Broucke, Roger A. |
| Group | 1 DMC-INPE-MCT-BR |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 17 |
| Number | 5 |
| Pages | 1075-1081 |
| History (UTC) | 2014-09-29 15:13:37 :: administrator -> marciana :: 1994 2018-04-19 14:15:04 :: marciana -> administrator :: 1994 2021-07-28 22:17:56 :: administrator -> marciana :: 1994 |
| 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 MANOBRA DE ORBITA MECANICA ESPACIAL |
| Abstract | The problem of transfer orbits from one body back to the same body (the moon or a planet) is formulated as a Lambert problem and solved by Gooding's Lambert routines . Elliptic and circular orbits are considered for the moon or a planet and any type of orbit (elliptic, parabolic, or hyperbolic) is considered for the spacecraft. The solutions are plotted in terms of the true anomaly (instead of the eccentric anomaly) for several cases. The use of the true anomaly simplifies the solutions in several ways. The problem of transfers from this body to the corresponding L4 and L5 points is also solved. Next, the same problem is studied in terms of the and the time required for the transfer. Among all of the possible transfer orbits, a small family with almost zero was studied in detail. A transfer from the moon to the corresponding Lagrangian equilibrium points L or L is shown, as an example of a practical application of this theory. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Study of henon's... |
| 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 | prado_study.pdf |
| User Group | administrator |
| Visibility | shown |
| 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; COMPENDEX. |
| Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
| 6. Notes | |
| Empty Fields | affiliation alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress format isbn language lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |