NASA NTRS · 20210003342
Optimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits
Abstract
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.
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Howell, K., Lo, M., Wilson, R.. 1999-08-16. Optimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits. https://ntrs.nasa.gov/citations/20210003342
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