日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
超小型衛星用ドッキング機構によるスラスタ搭載衛星の進入把持3次元微小重力実験
宇井 恭一占部 智之松永 三郎石川 智浩佐鳥 新
著者情報
ジャーナル フリー

2005 年 53 巻 620 号 p. 419-425

詳細
抄録
This paper describes 3-dimensional microgravity experiments of a new docking mechanism for nano-satellite at Japan Microgravity Center (JAMIC). The proposed docking sequence is divided between approaching/grasping phase and guiding phase. In the approaching/grasping phase, the docking mechanism grasps the nano-satellite even though the nano-satellite has some control errors in a docking space. In the guiding phase, the docking mechanism guides the nano-satellite to a docking port while adjusting its attitude in order to transfer electrical power and fuel to the nano-satellite. We design and fabricate an experimental model of the docking mechanism which has the grasping and guiding functions for each phase. The objective of the experiments is to verify the grasping function because 3-dimensional microgravity environment is very important in the approaching/grasping phase. In this paper, we introduce the docking mechanism and the daughtership satellite model and explain the microgravity experimental setup and its results.
著者関連情報
© 2005 The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top