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本文分析了对称方法不适合带耗散力的卫星轨道长间隔积分的缺陷和本质原因,并针对这个问题,采用文所介绍的方法,构造并推荐了一组积分公式。
In this paper, we analyze the defect that the symmetry method is unsuitable for the long interval integral of satellite orbits with dissipative forces and propose a set of integral formulas to solve this problem, using the method introduced in this paper.