[2023-f-04]On-Orbit Performance Evaluation of Agile and Large-Angle Attitude Control of Spacecraft with Variable Shape Function
*Kei Watanabe1, Hiroyuki Kobayashi1, Yuki Amaki1, Toshihiro Chujo1, Saburo Matunaga1(1. Tokyo Institute of Technology, Department of Mechanical)
Keywords:
Variable Shape,HIBARI,Attitude Control,Non-Holonomic Constraint
