现代战斗机机载火力控制系统，是其完成作战任务的基础和保障。
Firepower control system of modern fighter must manage and control many kinds of weapons carried on fighter to accomplish the combat mission.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
提出了一种确定目标进入角的原理和方法，这种原理和方法具有较高的计算精度和实时性，易于工程实现，可用于机载火力控制系统完成空对空导弹允许发射区计算。
This method are with a high accuracy and real time application, and can be applied in the calculation of allowable launching area of air to air missile in air borne fire control system.
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