摘要
本文研究了三体问题中平衡点附近周期轨道的周期和特证指数与其所在能量面的能量之间的关系,并就这种关系对地—月—人卫系统给出了具体的计算结果。
The periods and characteristic exponents of the periodic orbits in the vicinity of the equilibrium points in the restricted three-body problem have been studied. The relations between the periods, the characteristic exponents and the energy of the energy surfaces where the periodic orbits lie are shown, and some results for the Earth-Moon-satellite system are given.
