[F-9] Attitude Determination and Control

[2022-f-37] Experiment/Simulation-Based Assessment of Microvibration-Induced Pointing Error in 6U Class CubeSat Missions

*Takayuki Hosonuma¹, Satoshi Ikari¹, Toshihiro Suzuki¹, Toshio Imamura¹, Masahiro Fujiwara¹, Hirotaka Sekine¹, Naoto Usami¹, Ryohei Takahashi¹, Yoshihide Shimada², Hirokazu Nakamura², Shinichi Yokobori¹, Ryuichi Hirayama¹, Tatsuya Arai¹, Kazuki Toma¹, Akihiro Ishikawa¹, Shuhei Matsushita¹, Ryu Funase¹, Shinichi Nakasuka¹ (1. The University of Tokyo, 2. Seiren Co., Ltd)

キーワード：Microvibration, Ponting Control, Satellite Structure, Reaction Wheels