%0 Journal Article
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}
%@archivingpolicy denypublisher denyfinaldraft
%3 4.pdf
%X In this paper we present the first part of an extensive study of nonimpulsive orbital transfers under thrust errors. We emphasize the first part of the numerical implementation (Monte-Carlo) of the study but mention the first algebraic explanation for some of the numerical results. Its main results suggest and partially characterize the progressive deformation of the trajectory distribution along the propulsive arc, turning 3sigma ellipsoids into banana shaped volumes curved to th6 center of attraction (we call them "bananoids") due to the loss of optimality of the actual (with errors) trajectories with respect to the nominal (no errors) trajectory.
%N 2
%T Statistical analysis of nonimpulsive orbital transfers under thrust errors, 1
%K orbits, transfer, nonimpulsive, thrust errors, Monte-Carlo analysis.
%@secondarytype PRE PI
%@usergroup administrator
%@usergroup banon
%@usergroup marciana
%@group
%@group
%@group DMC-INPE-MCT-BR
%@copyholder SID/SCD
%@secondarykey INPE-9657-PRE/5265
%@issn 1562-8353
%@issn 1813-7385
%2 sid.inpe.br/marciana/2003/05.28.11.10.40
%@affiliation Departamento de Física, Universidade Estadual de Feira de Santana (UEFS)
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%B Nonlinear Dynamics and Systems Theory
%@versiontype publisher
%P 157-172
%4 sid.inpe.br/marciana/2003/05.28.11.10
%@documentstage not transferred
%D 2002
%V 2
%A Jesus, Antônio Delson Conceição de,
%A Souza, Marcelo Lopes de Oliveira e,
%A Prado, Antonio Fernando Bertachini de Almeida,
%@dissemination WEBSCI; PORTALCAPES.
%@area ETES