NASA NTRS · 20210003344
Optimization of Insertion Cost for Transfer Trajectories to Libration Point Orbits
Abstract
The objective of this work is the development of efficient techniques to optimize the cost associated with transfer trajectories to libration point orbits in the Sun-Earth-Moon four body problem, that may 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/20210003344
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