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Kazuki Kishiwada

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2021
[c1]
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Yuto Kitazono, Kazuki Kishiwada, Koichi Yonemoto, Takahiro Fujikawa, Takahiro Matsukami:
Control System Design for the Powered Ascent of Winged Rocket Based on Dynamic Inversion Theory. SICE 2021: 767-772

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