[D-14] Trajectory Design and Optimization 1

[2022-d-60] Design of Multi-Lunar-Flyby Trajectories using Collision Orbits in a Bicircular Restricted Four-Body Model

*Ferran Gonzalez Franquesa¹, Diogene Alessandro Dei Tos², Yasuhiro Kawakatsu² (1. The Graduate University for Advanced Studies, SOKENDAI, 2. JAXA)

キーワード：lunar flyby, collision orbits, four-body models