建立了再入机动弹道数学模型，给出了气动力系数为速度、迎角、高度的函数拟合式，进行了最佳再入机动弹道设计和仿真计算。
The mathematical model of reentry maneuvering trajectory is established. The fitting expression of aerodynamic coefficient function on velocity, attack of Angle and altitude is presented.
目的 研究底排火箭复合增程弹最佳外弹道参数匹配方案。
This paper presents numerical investigations of influence of base bleed on increasing range of base bleed projectile.
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