ランデブ接近軌道の標準的復帰法

河野 功, 若林 靖史

doi:10.2322/jjsass.50.95

ランデブ接近軌道の標準的復帰法

DOI DOI 機関リポジトリ機関リポジトリ Web Site Web Site Web Site Web Site ほか3件をすべて表示一部だけ表示被引用文献14件参考文献20件

河野功

宇宙開発事業団
若林靖史

宇宙開発事業団

書誌事項

タイトル別名

Standard Recovery Method to Rendezvous Approach Trajectory.
ランデブセッキンキドウノヒョウジュンテキフッキホウ
ETS-7ランデブ・ドッキング実験の結果
ETS 7 ランデブドッキングジッケンノケッカ
Result of Rendezvous Docking Experiment of ETS-VII.

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抄録

Rendezvous docking technology will be necessary for advanced space activities in the early 21st century, such as logistic support service to the International Space Station, exchange of observation sensors or bus equipments, re-supply of fuel or cryogenic liquid, etc. A chaser vehicle will perform rendezvous along a reference trajectory, which would be pre-planned and well investigated. If the chaser deviate from the reference trajectory for instance because of thruster trouble, it will be required to recover to the reference trajectory as soon as possible. In this paper, we introduce an easy and practical recovery method based on C–W solution of Hill’s equation. We think the recovery method will be applicable for many kinds of rendezvous vehicles.