[d-10] Trajectory Design and Optimization 1

[2023-ｄ-41] Orbital Configuration Control for Space-based Gravitational Wave Observatory in the Three-body Problem

*Zhengxu Pan^1,2, Zhanxia Zhu², Mai Bando¹, Shinji Hokamoto¹ (1. Kyushu University. Department of Aeronautics and Astronautics, 2. Northwestern Polytechnical University. School of Astronautics)

キーワード：gravitational wave observatory, circular restricted three-body problem, the two-layer optimization, “Taiji” mission