[D-6] Attitude Determination & Control 2

[2022-d-25] Semi-Optimal Control Law for Minimum-Time Maneuver of Satellite with Pyramid-Type VSCMG

*Kohei Oikawa¹, Takehiro Higuchi², Motoharu Fujii¹, Naoto Hoshika¹, So Kaieda³, Ohmi Fuchiwaki⁴ (1. Yokohama National University Graduate School of Engineering Science, 2. Yokohama National University Faculty of Environment and Information Science, 3. Yokohama National University College of Engineering Science, 4. Yokohama National University Faculty of Engineering)

Keywords:VSCMG, Optimal Control, Semi-Optimal Control