宮﨑海杜 氏
2022年12月15日(木) 15時00分
総合研究10号館317号室 / Zoom会議 (ハイブリッド)
The L1 and L2 points of Sun-Earth system have an advantage in observations and communications because the relative positions with these bodies do not change. These equilibria are unstable so that we need to control the attitude and regular course of a satellite which orbits around these points. Hill’s equations are used to model the dynamics of that space crafts. In this talk, Firstly I explain about orbits around these equilibria and Introduce some control methods that can be applied in this situation. Finally, I state my plan for the future work.