Design of Transfers Trajectories Between Resonant Orbits in the Restricted Problem with Application to the Earth-Moon System (IAA-AAS-DyCoSS1-05-09 - AAS 12-333)
Conference, Dynamics and Control of Space Systems; proceedings of the 1st International Academy of Astronautics Conference ; 2012 ; Porto, Portugal
2012-01-01
20 pages
Includes bibliographical references and indexes; ALSO HELD ON CD-ROM
Conference paper
English
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