| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/GUonN |
| Repository | sid.inpe.br/iris@1905/2005/07.29.05.59.40 (restricted access) |
| Last Update | 2018:04.19.14.03.06 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/07.29.06.00 |
| Metadata Last Update | 2021:07.28.22.17.56 (UTC) administrator |
| Secondary Key | INPE-6729-PRE/2751 |
| ISSN | 0731-5090 1533-3884 |
| Label | 7897 |
| Citation Key | BrouckePrad:1996:OrPlMa |
| Title | Orbital planar maneuvers using two and three-four (through infinity) impulses  |
| Year | 1996 |
| Secondary Date | 19980707 |
| Month | Mar. - Apr. |
| Access Date | 2024, May 08 |
| Secondary Type | PRE PI |
| Number of Files | 1 |
| Size | 1158 KiB |
| 2. Context | |
| Author | 1 Broucke, Roger A. 2 Prado, Antonio Fernando Bertachini de Almeida |
| Group | 1 DMC-INPE-MCT-BR |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 19 |
| Number | 2 |
| Pages | 274-282 |
| History (UTC) | 2014-09-29 15:13:37 :: administrator -> marciana :: 1996 2018-04-19 14:03:07 :: marciana -> administrator :: 1996 2021-07-28 22:17:56 :: administrator -> marciana :: 1996 |
| 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 thrust coplanar |
| Abstract | We consider the problem of minimum time-free impulsive transfers between coplanar Keplerian orbits. We studied two types of maneuvers: the ones performed with two impulses and the ones performed with three or four impulses that go to infinity in the middle of the transfer. For the two-impulse maneuver, we develop optimality conditions that lead to a nonlinear system of three equations and three unknowns. For the three-impulse maneuver, we develop a new maneuver that uses two elliptic transfer orbits that are connected by a negligible impulse applied at an infinite distance from the attracting body. It is an extension of the bi-elliptic transfer, where the two orbits involved in the transfer are not coaxial. We study in detail and show regions of optimality for the most trivial cases of transfers: between two circular orbits, one circular and one elliptic orbit, and two elliptic coaxial orbits. We complete the research by studying a scheme to reduce the total for some of those maneuvers, by adding a second impulse at infinity, and making it a four-impulse maneuver. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital planar maneuvers... |
| 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 | broucke_orbital.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 secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
| 7. Description control | |
| e-Mail (login) | marciana |
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