Halo orbit determination and control for the elliptic restricted three-body system
Author:
Affiliation:
1. Arizona State Univ., Tempe
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3729
Reference13 articles.
1. Quasi-periodic orbits about the translunar libration point
2. Trajectories and Orbital Maneuvers for the First Libration-Point Satellite
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