"Control System Design for the Powered Ascent of Winged Rocket Based on ..."

Yuto Kitazono et al. (2021)

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DOI: —

access: closed

type: Conference or Workshop Paper

metadata version: 2021-10-20

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  dblp key:
  - conf/sice/KitazonoKYFM21
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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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