摘要
本文应用数值积分法构造了卫星运动方程中各摄动力模型,分别给出了轨道计算中所需的实用公式及各相关的偏微分。
This article, through numerical integral method, Constructs the perturbation force model of satellite move-ment eguation, and gives the practical formulas and every relative partial differential needed in orbit Calculating.
关键词
摄动力
引力场
潮汐力
太阳辐射压
Perturbation Force
Gravitation field
Tidal force
Solar radiation pressure
