The objective of this work is the development of efficient techniques for preliminary optimization of the cost associated with transfer trajectories to libration point orbits in the Sun-Earth-Moon four body problem; such transfers may also include lunar gravity assists.
Optimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits
1999-08-16
Miscellaneous
No indication
English
genesis , halo , optimization , orbit
Optimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits (AAS 99-401)
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