Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
Resource URI: https://dblp.l3s.de/d2r/resource/publications/conf/sii/ShiraishiSSFKS22
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Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
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Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
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