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介绍了建立在最优控制理论上的导引律的方法,对攻击机动目标的导航比进行了最优化处理,得出导弹在不同攻击条件下的导航比。
The guidance law based on the optimal control theory is introduced. The navigation ratio of the maneuvering target is optimized, and the navigation ratio of the missile under different attack conditions is obtained.