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推导了空对地导弹的三维导引律模型,并设计了针对机动目标的变结构导引律,分析了其制导特性。设计的导引律由于需要的目标信息少,可以便利地应用于实际工程中,数字仿真结果证实了设计的导引律的可行性。
The three-dimensional guided law model of air-to-ground missiles was deduced and a variable structure guidance law was designed for the maneuvering targets. The guidance characteristics were analyzed. Due to the small target information needed, the designed guidance law can be conveniently used in practical engineering. The results of digital simulation confirm the feasibility of the design guidance law.