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Published in 2021 at "Journal of The Brazilian Society of Mechanical Sciences and Engineering"
DOI: 10.1007/s40430-021-03071-9
Abstract: This paper considers the dynamics of the circular restricted three-body problem (CRTBP) for the Earth–Moon system designing stationkeeping controllers at periodic orbits. Taking into account the $$L_1$$ and $$L_2$$ equilibrium points in this dynamics, it…
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Keywords:
halo orbits;
earth moon;
libration points;
stationkeeping controllers ... See more keywords