[D-14] Trajectory Design and Optimization 1

[2022-d-58] Halo-to-Halo Low-Thrust Transfer via Successive Convex Optimization with Intermediate Orbit Design

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

キーワード：Low-Thrust Trajectory, Three-Body Problem, Convex Optimization