[D-5] Orbital Dynamics 2

[2022-d-23] Design of low energy transfer trajectories from Earth to Europa with ballistic capture

*Kanta Ikeda¹, Naoki Hiraiwa¹, Mai Bando¹, Shinji Hokamoto¹ (1. Kyushu Univ. Department of Aeronautics and Astronautics)

キーワード：Trajectory Design, Multibody Dynamics, Periapsis Poincaré Map