[F-9] Attitude Determination and Control

[2022-f-41] Development of Compact and Highly Capable Integrated AOCS Module for CubeSats

*Satoshi Ikari^1,4, Takayuki Hosonuma¹, Toshio Imamura¹, Toshihiro Suzuki¹, Masahiro Fujiwara¹, Hirotaka Sekine¹, Naoto Usami¹, Ryohei Takahashi^1,4, Hajime Arai², Yoshihide Shimada², Hirokazu Nakamura², Ryo Suzumoto^1,4, Toshihiro Shibukawa^1,4, Shuhei Matsushita^1,4, Akihiro Ishikawa¹, Takayoshi Fukuyo⁴, Ryu Funase^1,3, Shinichi Nakasuka¹ (1. The University of Tokyo, 2. Seiren Co., Ltd., 3. ISAS, JAXA, 4. ArkEdge Space Inc.)

キーワード：CubeSats, Attitude Control, Orbit Determination