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采用了被动雷达寻的加捷联惯性制导做为反辐射导弹抗雷达关机的具体措施,采用了广义卡尔曼滤波方法解决了惯性制导的基准轴指向误差的修正问题.并根据导弹的运动方程组对导弹从发射点开始至雷达关机点,直至导弹落地的飞行全过程进行了全弹道仿真。
The passive radar seeks to add strapdown inertial guidance as anti-radiation missile anti-radar shutdown specific measures, the use of generalized Kalman filtering method to solve the inertial guidance of the reference axis pointing error correction problem.According to the missile equations of motion The whole ballistic simulation was carried out on the missile from the launching point to the radar off point until the entire flight of the missile landed.