Based on linear quadratic Gaussian (LQG) theory, this paper shows a study of a LQG optimal guidance law that minimizes the terminal miss distance and control energy consumption within the intercepting period.

• 以线性二次型高斯 (LQG)理论为基础 ,研究一种最小化末端脱靶量和拦截周期内控制能量消耗的具有可变有效导航比的LQG最优制导规律。