| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3JUy |
| Repository | sid.inpe.br/iris@1905/2005/08.04.02.07 (restricted access) |
| Last Update | 2019:01.16.16.20.54 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.02.07.27 |
| Metadata Last Update | 2021:02.11.18.10.10 (UTC) administrator |
| Secondary Key | INPE-9538-PRE/5191 |
| Label | 10466 |
| Citation Key | JesusPradSouz:2002:MoAnNo |
| Title | Monte-carlo analysis of nonimpulsive orbital transfer under thrust errors, 3  |
| Format | ISBN 85-17-00006-4 |
| Year | 2002 |
| Secondary Date | 20021213 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 3273 KiB |
| 2. Context | |
| Author | 1 Jesus, Antonio Delson Conceição de 2 Prado, Antonio Fernando Bertachini de Almeida 3 Souza, Marcelo Lopes de Oliveira e |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida |
| Book Title | Colóquio Brasileiro de Dinâmica Orbital, 10 Advances in space dynamics 3: application in astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 397-408 |
| Series Title | Advances in space dynamics 3: application in astronautics |
| History (UTC) | 2008-06-09 21:41:10 :: administrator -> jefferson :: 2012-08-02 17:55:08 :: jefferson -> administrator :: 2019-01-16 16:20:31 :: administrator -> simone :: 2002 2019-01-16 16:20:54 :: simone -> administrator :: 2002 2021-02-11 18:10:10 :: administrator -> :: 2002 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL |
| Abstract | In this paper we studied statistically orbital maneuvers with finite propulsion under thrust errors. We studied two transfer maneuvers: a)a high orbit low thrust coplanar theoretical transfer; and b)a middle orbit high thrust noncoplanar practical transfer (1st transfer of the satellite EUTELSAT II-F2).These transfers were realized with magnitude and direction ("pitch" and "yaw")errors in the thrust applied to the satellite. This errors were modeled as stochastic processes: random-bias and white or pink noise, with zero mean and adjustable variance gaussian probability functions. We also studied the 1st moment (mathematical expectation)of the standard deviation of each thrust error. The general results suggest simple nonlinear relations between the causes (in the initial instant)and effects (in the final instant), and a progressive deformation of the trajectory distribution along the propulsive arc. Finally, we compared and related both results, the gaussian and the uniform results. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Monte-carlo analysis 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 | |
| Target File | INPE-9538.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 contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |