Interplanetary trajectories in the restricted three-body problem
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Polo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2761
Reference5 articles.
1. Matched-conic approximation to the two fixed force-center problem
2. SOME NUMERICAL ASPECTS OF EARTH-TO-MOON TRAJECTORIES IN THE RESTRICTED THREE-BODY PROBLEM
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