Article ID: | iaor201530565 |
Volume: | 110 |
Start Page Number: | 341 |
End Page Number: | 353 |
Publication Date: | May 2015 |
Journal: | Acta Astronautica |
Authors: | Howell Kathleen C, Folta David C, Bosanac Natasha, Guzzetti Davide |
Keywords: | control |
As 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.