摘要
考虑到反舰导弹试验与训练的安全性,引入反舰导弹飞行航区的定义。探讨了4个影响飞行航区划定因素:舰面干扰、风干扰、陀螺漂移干扰、导弹故障干扰,构建了反舰导弹干扰作用下的全弹道模型。进而以设定的导弹参数为例,划定飞行航区,通过与实际靶试对照,验证了该方案的合理性与优越性。
Considering the safety of anti-ship testing and training, this paper introduced the concept of .flight test region, and studied the four factors which affect the design of flight test region, which are ship-deck interference, wind interference, gyro drift interference, fault interference. It constructed the anti-ship whole trajectory model with interferences, then designed the flight test region by setting missile parameters, contrasted the simulation test with the actual range test, and verified the rationality and superiority of the scheme.
出处
《飞行力学》
CSCD
北大核心
2009年第1期55-58,共4页
Flight Dynamics
关键词
反舰导弹
飞行航区
弹道模型
仿真
anti-ship missile
flight test region
trajectory model
simulation
