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Optimization of Insertion Cost for Transfer Trajectories to Libration Point OrbitsThe 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.
Document ID
20210003344
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/16861
Authors
Howell, K.
Lo, M.
Wilson, R.
Date Acquired
August 16, 1999
Publication Date
August 16, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Genesis
Halo
Orbit
Libration
Point

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