Considering the limitation of the anti-radiation submissile, this paper shows a method by GNSS/SINS integrated guidance to improve the hit accuracy on conditions that radar swiching-off.
文中主要根据反辐射子弹的局限性，采用GNSS/SINS组合制导方案来提高反辐射子弹在雷达关机情况下的命中精度，达到抗雷达关机的能力。
The idea of aerodynamic design for an unguided glider submissile is introduced. Wind tunnel experimental results indicate that the tail raiser plays the role of causing a submissile to glide.
采用理论与实验相结合的方法进行了滑翔子弹的气动外形设计。
应用推荐