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发射空空导弹允许的载机操纵误差是导弹武器系统设计时需要解决的问题。它的大小影响到载机构成发射条件的难易程度。本文参考国外多种空空导弹的有关资料,给出了该项允许操纵误差的火控计算方法。
The operational error of launch aircraft allowed by launching air-to-air missiles is a problem to be solved in the design of missile weapon system. Its size affects the ease with which the carrier’s launch conditions are made. This paper refers to a variety of foreign air-to-air missiles relevant information, gives the allowable error of the fire control calculation.