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1. Identity statement
Reference TypeBook Section
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/GUKBB
Repositorysid.inpe.br/iris@1905/2005/07.29.22.35   (restricted access)
Last Update2015:11.18.11.30.58 (UTC) marciana
Metadata Repositorysid.inpe.br/iris@1905/2005/07.29.22.35.18
Metadata Last Update2021:02.11.18.09.44 (UTC) administrator
Secondary KeyINPE-8041-PRE/3857
Label8995
Citation KeyJesusSouzPrad:2000:StEfTh
TitleStudy of the effects of thrust vector erroRs on nonimpulsive orbital transfers
FormatISBN:901487-1-8
Year2000
Secondary Date20010416
Access Date2024, May 08
Secondary TypePRE LN
Number of Files1
Size71 KiB
2. Context
Author1 Jesus, Antonio Delson Canceição
2 Souza, Marcelo Lopes Oliveira
3 Prado, Antonio Fernando Bertachini de Almeida
Group1 DMC-INPE-MCT-BR
EditorPrado, Antonio Fernando Bertachini de Almeida.
Book TitleColóquio brasileiro de Dinâmica Orbital, 9 Advances in space Dynamics
Pages424-436
Series TitleAdvances in space Dynamics
History (UTC)2014-09-29 15:08:58 :: administrator -> marciana :: 2000
2015-11-18 11:30:58 :: marciana -> administrator :: 2000
2021-02-11 18:09:44 :: administrator -> :: 2000
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
astrodinâmica
trajetórias espaciais
mecânica celeste
manobras orbitais transferência de orbitas
astrodynamics
spacecraft trajectories
celestial mechanics
orbital maneuvers
transfer orbits (orbital transfer)
AbstractIn this paper we present the first part of a Monte-Carlo analysis of nonimpulsive orbital transfers under thrust errors. This was done as part of an extensive study conducted in three phases. The first phase was the numerical implementation and numerical tests of a nonimpulsive trajectory optimization method. The second phase was an extensive Monte-Carlo analysis on nonimpulsive orbital transfers under thrust errors. The third phase was a first algebraic explanation for some of the numerical relations found in the second phase. This paper emphasizes the first (uniform) part of the second phase. Its main results suggest and partially characterizes the progressive deformation of the trajectory distribution along the propulsive arc, turning 3sigma ellipsoids into banana shaped volumes curved to the center of atraction (we call them "bananoids") due to the loss of optimality of the actual (with errors) trajectories with respect to the nominal (no errors) trajectory. Such deformations can not be anticipated by covariance analysis on linearized models with zero mean errors which propagate ellipsoids into ellipsoids always centered in the nominal (no errors) trajectory. The results also characterize how close or how far are Monte-Carlo analysis and covariance analysis for those examples.
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4. Conditions of access and use
Target File2000_jesus.pdf
User Groupadministrator
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
Empty Fieldsaffiliation archivingpolicy archivist callnumber city 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 publisher readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url volume


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