[D-15] Trajectory Design and Optimization 2

[2022-d-63] Multidisciplinary System Design Optimization on Precise Lunar Landing Trajectories and Spacecraft Systems

*Satoshi Ueda¹, Takahiro Ito¹, Shin-ichiro Sakai² (1. Japan Aerospace Exploration Agency, Research and Development Directorate, 2. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science)

キーワード：Trajectory optimization, Spacecraft system, Lunar landing, MSDO, Precise guidance