自由飞行轨道解析解的中间轨道方法

本文给出了一组不仅能用于卫星轨道计算，同时也能用于导弹自由飞行轨道的中间轨道计算公式。引组公式的解与二体问题解有很好的可比性。由于导弹轨道与卫星轨道有很大不同，故计算中的各使用常数的取值范围也有很大不同。

Intermediate Orbital Method Of Analytic Solution of Free Flight Trajectory

This paper derives a group of computing formulas of intermediate orbit which can be applied not only to satelhte trajactories but also to missile free flight trajectories. The solutions of the formulas are very comparable with the solutions of 2-body problem. Due to the essential difference between ballistic trajectory and satellite trajectory, the values of the constant coefficients in ballistic trajectory may have great difference from those in satellite trajectory.