2025 AAS/AIAA Space Flight Mechanics Meeting

2025 年 1 月 19 日から 23 日までアメリカ・ハワイで開催された 2025 AAS/AIAA Space Flight Mechanics Meeting にて、以下の研究発表を行いました。

• Detecting unstable resonant orbits via Keplerian map（Keplerian mapを用いた不安定共鳴軌道の導出）
  • Shohei Morimitsu*, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)
• Station-Keeping for Earth-Moon Periodic Orbit with Solar Sail based on the Orbit-Attitude Coupled Model（軌道・姿勢連成モデルに基づくソーラーセイルを用いた地球-月周回軌道のステーションキーピング）
  • Yuta Hayashi*, Naoki Hiraiwa, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)
• Extending Earth–Moon Transfer Based on Lobe Dynamics into the Restricted Four-Body Problem （ローブダイナミクスに基づく地球-月遷移の円制限4体問題への拡張）
  • Naoki Hiraiwa*, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)

Our laboratory presented our research at the 2025 AAS/AIAA Space Flight Mechanics Meeting held in Hawaii, U.S., from January 19 to 23, 2025.

• Detecting unstable resonant orbits via Keplerian map
  • Shohei Morimitsu*, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)
• Station-Keeping for Earth-Moon Periodic Orbit with Solar Sail based on the Orbit-Attitude Coupled Model
  • Yuta Hayashi*, Naoki Hiraiwa, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)
• Extending Earth–Moon Transfer Based on Lobe Dynamics into the Restricted Four-Body Problem
  • Naoki Hiraiwa*, Mai Bando, Shinji Hokamoto (Kyushu University, Japan)