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首页> 外文期刊>北海道工業大学研究紀要 >Experimental study of rendezvous docking mechanism for microsatellite under the microgravity field
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Experimental study of rendezvous docking mechanism for microsatellite under the microgravity field

机译:微重力场下微卫星交会对接机理的实验研究

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摘要

In order to build a small satellite in the mass range of 5-kg (microsatellite), the feasibility study has been begun for the development of microsatellite. Several key technologies are studied such as small reaction wheel, small electric propulsion, docking mechanism, electrical recharging device, and software for three-axes attitude control by using image processing. This paper is described about the experimental test of the original berthing and docking mechanism for microsatellite under the microgravity condition, which was carried out on October 27 to 28, 1999, at Japan Microgravity Center (JAMIC), Kamisunagawa, Rokkaido.
机译:为了建造质量在5公斤(微卫星)范围内的小型卫星,已经开始进行微卫星开发的可行性研究。研究了一些关键技术,例如小反作用轮,小电推进,对接机构,充电装置以及使用图像处理的三轴姿态控制软件。本文介绍了微卫星在微重力条件下的原始靠泊和对接机制的实验测试,该实验于1999年10月27日至28日在北海道神奈川县的日本微重力中心(JAMIC)进行。

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