Attitude Control of Spacecraft with Membrane using Interplanetary Magnetic Field with Consideration of Vibration

講演情報

Oral Session

d) Astrodynamics, Navigation Guidance and Control

2023年6月7日(水) 11:00 〜 12:40 C Box 4F (C Box 4F)

Hirohisa Kojima (Tokyo Metropolitan University), Shinji Hokamoto ( Kyushu University)

12:00 〜 12:20

*Truong An Hoang Xuan¹, Takaya Inamori¹, Kouhei Yamaguchi¹ (1. Department of Aerospace Engineering, Nagoya University)

キーワード：Space membrane structure, Attitude control, vibration analysis