%0 Book Section
%@nexthigherunit 8JMKD3MGPCW/446AF4B
%3 INPE-9528.pdf
%X In this work we study the problem of orbital station keeping maneuvers of symmetrical constellations of satellites with minimum fuel consumption using impulsive maneuvers with time constraint. This time constraint imposes a new characteristic to the problem, that rules out the majority of the transfer methods available in the literature. Due to the satellites constraints, we have the problem of simultaneously optimizing the maneuver for n satellites. Thus, the goal of this work is to formulate and to study maneuver strategies that, in some way, make it possible to obtain solutions with small fuel consumption and time constraint considering all the satellites in the constellation, thus we have a multi-objective problem.
%@secondarydate 20021213
%E Winter, Othon Cabo,
%E Prado, Antonio Fernando Bertachini de Almeida,
%T Station Keeping of Satellite Constellation with time contraint using optimal bi-impulsive maneuvers
%S Advances in space dynamics 3: applications in astronautics
%@format ISBN 85-17-00006-4
%@secondarytype PRE LN
%K ENGENHARIA E TECNOLOGIA ESPACIAL, orbital maneuvers, constellations of satellites, fuel consumption, impulsive maneuvers, time constraint, stationkeeping.
%B Advances in space dynamics 3: applications in astronautics
%@usergroup administrator
%@group DMC-INPE-MCT-BR
%C São José dos Campos
%@secondarykey INPE-9528-PRE/5181
%F 10457
%2 sid.inpe.br/iris@1905/2005/08.04.01.57.27
%I INPE
%P 238-256
%4 sid.inpe.br/iris@1905/2005/08.04.01.57
%D 2002
%@documentstage not transferred
%A Rocco, Evandro Marconi,
%A Souza, Marcelo Lopes de Oliveira e,
%A Prado, Antonio Fernando Bertachini de Almeida,
%@area ETES
%@holdercode {isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S}