This project concerns closed trajectories of a spacecraft under the gravitational attraction of the Earth and of the Moon. Our approach uses both analytical and numerical methods in order to find proper initial conditions and closed orbits in the vicinity of Lagrangian points, in the Earth-Moon system. All computations are performed with Maple 15.
|Presenter:||Jessica Friedman (SUNY Brockport) -- email@example.com
|Topic:||Math and Sciences - Poster Session|
|Location:||Edwards Hall Lobby|
|Time:||9 am (Session I)|