| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3E5d |
| Repository | sid.inpe.br/iris@1905/2005/08.03.22.17 (restricted access) |
| Last Update | 2018:01.02.11.26.00 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.03.22.17.40 |
| Metadata Last Update | 2021:02.11.18.09.45 (UTC) administrator |
| Secondary Key | INPE-9217-PRE/4888 |
| Label | 10131 |
| Citation Key | PrasadKuga:2000:StHoCo |
| Title | Study of a homotopy continuation method for station keeping maneuvers  |
| Year | 2000 |
| Secondary Date | 20021004 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LI |
| Number of Files | 1 |
| Size | 159 KiB |
| 2. Context | |
| Author | 1 Prasad, Polamraju Rajendra 2 Kuga, Hélio Koiti |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Prado, Antonio Fernando Bertachini de Almeida |
| Book Title | Advances in Space Dynamics |
| City | São José dos Campos |
| Pages | 204-212 |
| Series Title | Advances in Space Dynamics |
| History (UTC) | 2014-09-29 15:09:01 :: administrator -> marciana :: 2000 2018-01-02 11:26:00 :: marciana -> administrator :: 2000 2021-02-11 18:09:45 :: administrator -> :: 2000 |
| 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 station keeping maneuvers |
| Abstract | The station acquisition and subsequently c for satellites carrying applicat payloads for communications or remote sensing are of great importance. For remote sensing missions with precise applications, the immediate post launch maneuver design task is to achieve operational orbit with specified reference ground track pattern. The maneuvers are to be designed to ensure ground track pattern phasing with minimum number of maneuvers. The station acquisition of geo-stationary satellite consists of bringing it from the initial geo-stationary transfer orbit into station on the geo-stationary orbit. There are several existing operational methods to solve problem concerning the optimal space maneuvers. Typically these methods are solved by one of following two methods. In the so-called indirect method necessary conditions of optimality derived using the calculus of variations and generally result in a two-point boundary value problem. Most of these approaches are difficult to solve and are subject to numerical sensitivity problems. The other hand, direct methods like optimization problems are frequently used for operation purposes. Here an attempt has been made to explore the feasibility of applying the homot continuation method for optimal space maneuvers. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Study of a... |
| 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 | 9217.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 copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress format isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project publisher readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |