Numerical solution and dispersion analysis for airbornerocket trajectory are studied.
本文研究航空火箭(简称航箭)弹道的数值解法和散布分析。
2
Finally, a certain model of airbornerocket as an example for calculation, the optimum attack condition curve about attack distance and dive Angle of armed helicopter is drawn.
最后，以某型航空火箭弹为例进行计算，得到关于距离和俯冲角的最佳攻击条件曲线。
3
The subsequent analysis results indicate that the rocket kinetic parameters after the air separation phase can be up to the mustard of the airborne launch mission.