摘要
文中根据末制导炮弹的飞行特点,提出了利用捷联惯导系统中的陀螺信息,确定末制导炮弹初始滚转角的方法,并通过半实物仿真试验,验证了初始滚转角确定方法的正确性。
In this paper,based on the trajectory character of the projectile,a method to determine the terminal guided projectile initial roll angle with the information got from the gyros in the SINS system is put forward.And a hardware- inothe-Ioop is done to test the method.The result proves that the method is right and effective.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第S4期356-358,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
末制导炮弹
初始滚转角确定
Terminal guided projectile
Initial roll angle determination
