%0 Journal Article
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%@resumeid
%@resumeid
%@resumeid 8JMKD3MGP5W/3C9JGJA
%X The search for methods to reduce the fuel consumption in orbital transfers is something relevant and always current in astrodynamics. Therefore, the maneuvers assisted by the gravity, also called Swing-by maneuvers, can be an advantageous option to save fuel. The proposal of the present research is to explore the influence of some parameters in a Swing-by of an artificial satellite orbiting a planet with one of the moons of this mother planet, with the goal of changing the inclination of the artificial satellite around the main body of the system. The fuel consumption of this maneuver is compared with the required consumption to perform the same change of inclination using the classical approach of impulsive maneuvers.
%8 may
%N 5
%9 journal article
%T Determination of the optimal conditions for inclination maneuvers using a Swing-by
%@electronicmailaddress osvaldomourajr@hotmail.com
%@electronicmailaddress
%@electronicmailaddress antonio.prado@inpe.br
%@secondarytype PRE PI
%K Swing-by · Orbital maneuvers · Changing of orbital plane · Astrodynamics.
%@archivingpolicy denypublisher denyfinaldraft12
%@usergroup self-uploading-INPE-MCTI-GOV-BR
%@usergroup simone
%@group
%@group
%@group DIDMC-CGETE-INPE-MCTIC-GOV-BR
%@tertiarymark Trabalho não Vinculado à Tese/Dissertação
%@secondarymark B1_GEOCIÊNCIAS B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B3_ASTRONOMIA_/_FÍSICA
%@issn 0004-640X
%2 sid.inpe.br/mtc-m21c/2018/05.04.19.41.12
%@affiliation Universidade Federal do ABC (UFABC)
%@affiliation Universidade Federal do ABC (UFABC)
%@affiliation Instituto Nacional de Pesquisas Espaciais (INPE)
%B Astrophysics and Space Science
%@versiontype publisher
%P e91
%4 sid.inpe.br/mtc-m21c/2018/05.04.19.41
%@documentstage not transferred
%D 2018
%V 363
%@doi 10.1007/s10509-018-3308-z
%A Moura Júnior, O.,
%A Celestino, C. C.,
%A Prado, Antonio Fernando Bertachini de Almeida,
%@dissemination WEBSCI; PORTALCAPES.
%@area ETES
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}