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Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration.
2022
Naoya Shiraishi
Yuji Sato
Yoshihiko Shibuya
Shinya Fujita
Toshinori Kuwahara
Daisuke Suzuki
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