%0 Book Section
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}
%3 9236.pdf
%X The objective of this paper is to study the problem of gravitational capture in the regularized restricted three-body problem. A gravitational capture occurs when a massless particle changes its two-body energy around one celestial body from positive to negative without the use of non-gravitational forces. We studied the importance of several of the parameters involved for a capture in the Earth -Moon system, including the time required for the capture and the effects of the periapse distance. Then, we generalize those results for other binary systems, like the Sun-Earth, Sun-Mars and Sun-Jupiter systems. Next, we cover the whole interval of the mass parameter micro (the mass ratio of the two primaries)and we study the gravitational capture in the interval 0.0 < micro< 0.5. The elliptical restricted problem is also considered as an option for the model.
%@secondarydate 20020511
%E Balthazar, José Manoel,
%E  Gonçalves, Paulo Batista,
%E  Brasil, Reyolando M. F. L. R. F. .,
%T Orbital maneuvers using gravitational capture
%S Nonlinear dynamics, chaos, control and their applications to engineering sciences
%@format ISBN:85-900351-3-1
%@secondarytype PRE LN
%K ENGENHARIA E TECNOLOGIA ESPACIAL, gravitational, capture, three-body problem.
%B Nonlinear dynamics, chaos, control and their applications to engineering sciences
%@usergroup administrator
%@group DMC-INPE-MCT-BR
%@secondarykey INPE-9236-PRE/4908
%F 10158
%2 sid.inpe.br/iris@1905/2005/08.03.22.37.26
%I ABCM;SBMAC
%P cap. 8, 109-128
%4 sid.inpe.br/iris@1905/2005/08.03.22.37
%D 2002
%@documentstage not transferred
%A Prado, Antonio fernando Bertachini de Almeida,
%A Vieira, Ernesto,
%@area ETES