空面导弹指挥仪模型及其解算

A Model for Fire Control System of Air-to-Surface

以攻击陆地/海上目标的某空面导弹机载武器火控系统为研究对象,导出了一种空面射击的指挥仪模型,用于解算导弹自控飞行时间和射击瞄准角。文中的模型主要由目标运动方程组、导弹的运动方程组等构成。最后进行了仿真解算,验证了模型和算法的正确性。

This paper makes a study of the airborne fire-control weapons system of some air-to-surface missile,and s di- rector mode of some Air-to-Surface shooting is presented to compute the flight time of the automatic control missile and the shoot angle.The model in this paper is mainly made up of the movement equations of the objective and the missile. Finally.it makes simulating calculation to validate the correctness of the model and the arithmetic.