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1. Identity statement
Reference TypeBook Section
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/H3J4R
Repositorysid.inpe.br/iris@1905/2005/08.04.01.24   (restricted access)
Last Update2018:01.10.16.29.06 (UTC) marciana
Metadata Repositorysid.inpe.br/iris@1905/2005/08.04.01.24.29
Metadata Last Update2021:02.11.18.09.54 (UTC) administrator
Secondary KeyINPE-9490-PRE/5143
Label10421
Citation KeyJesusSouzPrad:2002:MoAnNo
TitleMonte-Carlos analysis of nonimpulsive orbital transfer under thrust errors, 2
FormatISBN:85-900351-4-X
Year2002
Secondary Date20021011
Access Date2024, May 08
Secondary TypePRE LN
Number of Files1
Size186 KiB
2. Context
Author1 Jesus, Antônio Delson Canceiçã
2 Souza, Marcelo Lopes Oliveira e
3 Prado, Antônio Fernando Bertachini de Almeida
Group1 DMC-INPE-MCT-BR
EditorBalthazar, José Manoel
Gonçalves, Paulo Batista
Brasil, Reyolando M. F. L. R. F.
Caldas, Iberê
Rizatto, Felipe B.
Book TitleNonlinear dynamics, chaos, control and their applications to engineering sciences
PublisherABCM/AAM/SBMAC/SIMAC
Pagescap. 10, 379-389
Series TitleNonlinear dynamics, chaos, control and their applications to engineering sciences
History (UTC)2014-09-29 15:09:03 :: administrator -> marciana :: 2002
2018-01-10 16:29:07 :: marciana -> administrator :: 2002
2021-02-11 18:09:54 :: administrator -> :: 2002
3. Content and structure
Is the master or a copy?is the master
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Transferable1
Content TypeExternal Contribution
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
orbital maneuvers
thrust errors
Monte-Carlo Analysis
orbital transfer
AbstractIn this paper we studied statically orbital maneuvers with finite propulsion under thrust errors. We studied two transfer maneuvers: a)a high orbit low thrust coplanar transfer; and b)a middle orbit high thrust noncoplanar transfer (the 1§ transfer of the satellite EUTELSAT II-F2). These transfers were done with magnitude and direction ("pitch" and "yaw")errors in the thrust applied to the satellite. This errors were modeled as random-bias or white noise stochastic processes, with zero mean and unit variance gaussian probability density functions. We studied many cause-effects relations. Among them The general results, suggest the thrust magnitude errors do not cause appreciable mean final deviations, but that the standard deviation of each thrust direction error holds a nonlinear (almost parabolic)relation with the mean deviation in the final semi-major axis and with the final eccentricity. They suggest and partially characterizes the progressive deformation of the trajectory distribution along the propulsive are , turning 3sigma ellipsoids into banana shaped volumes curved to the center of attraction (we call them "bananoids")due to the nominal (no errors)trajectory. A Similar deformation but due to initial condition gaussian errors was shown by Junkins. As his plots also suggest, such deformations can not be anticipated by covariance analysis on linearized models with zero mean errors wich propagate ellipsoids into ellipsoids always centered in the nominal (no errors)trajectory. Our results also characterize how close or how far are Monte-Carlo Analysis and covariance analysis for those examples.
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Target File9490.pdf
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5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
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