論文
ランデブ接近軌道の標準的復帰法
2002 年 50 巻 578 号 p. 118
詳細
2002 年 50 巻 578 号 p. 118
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.
