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An Earth-Moon System Trajectory Design Reference CatalogAs demonstrated by ongoing concept designs and the recent ARTEMIS mission, there is, currently, significant interest in exploiting three-body dynamics in the design of trajectories for both robotic and human missions within the Earth-Moon system. The concept of an interactive and 'dynamic' catalog of potential solutions in the Earth-Moon system is explored within this paper and analyzed as a framework to guide trajectory design. Characterizing and compiling periodic and quasi-periodic solutions that exist in the circular restricted three-body problem may offer faster and more efficient strategies for orbit design, while also delivering innovative mission design parameters for further examination.
Document ID
20140010042
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Folta, David
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Bosanac, Natasha
(Purdue Univ. West Lafayette, IN, United States)
Guzzetti, Davide
(Purdue Univ. West Lafayette, IN, United States)
Howell, Kathleen C.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
July 23, 2014
Publication Date
March 24, 2014
Subject Category
Astrodynamics
Report/Patent Number
IAA-DyCoSS2-ID-37
GSFC-E-DAA-TN13580
Meeting Information
Meeting: IAA Conference on Dynamics and Control of Space Systems
Location: Roma
Country: Italy
Start Date: March 24, 2014
End Date: March 26, 2014
Sponsors: American Astronautical Society, International Academy of Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX13AM17G
CONTRACT_GRANT: NNX13AH02G
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Libration Orbits
Robotic & Human missions
Dynamical Systems
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