摘要
本文对一般空舰导弹的纵向下滑段弹道优化设计进行了探讨;介绍了利用极小值原理解决优化的数值方法;以某空舰导弹为例对该弹道进行了计算,并得出了较满意的结果,可供该弹道的计算机辅助设计参考。
The optimum longitudinal glide trajectory design for general air-to-ship missile was discussed. An optimum numerical method on basis of minimum principle was proposed. A trajectory for certain air-to-ship missile, as an example, has been calculated. The result obtained can be used for trajectory CAD as reference.
出处
《战术导弹技术》
1990年第1期19-26,共8页
Tactical Missile Technology
关键词
导弹
空对舰
弹道
优化算法
Air-to-ship missile Glide trajectory Trajectory optimization
