摘要
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计算的中间轨道计算公式。此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。
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.
出处
《导弹与航天运载技术》
1993年第5期16-26,共11页
Missiles and Space Vehicles
关键词
轨道
计算
弹道
势
Orbit calculation
Trajectory calculation
Potential function
