导弹火控系统精度分配实例设某空舰导弹的有效射程为60公里,运载母机的飞行地速为(300～450)公里/小时。导弹采用自控+自导控制体制,要求导弹在自控段终点自导头扑捉目标的概率不小于95％,则相应要求机载导弹火控系统给出射击诸元的精度为:瞄准角最大误差δψ_(max)≤1.5°自控飞行距离的最大误差δrzk_(max)≤900m要求对该火控系统组成中各设备的精度进行分配。一、空舰导弹武器火控系统在使用范围内的状态组合 Example Assignment of Missile Fire Control System Precision Assuming that the effective range of an air ship missile is 60 kilometers and that of the carrier aircraft is 300-350 kilometers per hour. The self-guided missile control system requires the missile at the end of the self-pilot to capture the target probability of not less than 95%, then the corresponding requirements of airborne missile fire control system gives the shooting accuracy: aiming angle maximum error δψ_ (max) ≤1.5 ° The maximum error of self-controlled flight distance δrzk_ (max) ≤900m requires the allocation of the accuracy of each device in the composition of the fire control system. First, the empty ship missile fire control system in the use of the combination of the state