空舰(地)导弹下滑弹道优化设计研究

STUDY OF GLIDE TRAJECTORY OPTIMIZATION FOR AIR-TO-SHIP MISSILES

对一般空舰导弹的纵向下滑弹道进行了设计研究,提出用样条函数作为导弹的纵向下滑基准弹道。实例计算结果表明,设计的下滑基准弹道可以满足载机不同发射速度、不同发射高度条件下弹道的技术要求。提供的方法可供弹道的计算机辅助设计参考。

The longitudinal glide trajectory design for general air-to-ship missile is studied.Using spline function as glide standard trajectory of missile is presented.The calculation result of example shows that glide standard trajectory designed can meet the trajectory tactical requirements when missile is launched in different velocity and altitude.The method in the paper can be used in trajectory CAD as reference.