[F-9] Attitude Determination and Control

[2022-f-39] Flight Model Development and Ground Tests of Variable-Shape Attitude Control Demonstration MicroSatellite HIBARI

*Kei Watanabe¹, Hiroyuki Kobayashi¹, Yuki Amaki¹, Naoki Kawaguchi¹, Soichi Sato¹, Kenichiro Takahashi¹, Fumitaka Sagawa¹, Shogo Nerome¹, Kiyona Miyamoto¹, Yuta Sasagawa¹, Yoichi Yatsu¹, Toshihiro Chujo¹, Saburo Matunaga¹, HIBARI Development Team¹ (1. Tokyo Institute of Technology)

キーワード：Microsatellite, Attitude Control, Variable Shape, Hardware in the Loop Simulation