导弹制导控制与目标杀伤

Guidance and control of the missile and target damage

采用协方差分析描述函数技术 (CADFT)对寻的导弹的制导精度进行了研究 ,提出了空气动力控制、直接侧向力控制的寻的导弹飞行末端的制导精度的一种新的解析模型 ,并研究了导弹直接碰撞杀伤目标的必要条件 ,该理论研究成果具有简单、实用、精度高的特点 。

Guidance accuracy of homing missile is studied with CADFT (Covariance Analysis Describing Function Technique) in this paper. A new analytical model of guidance accuracy for homing missile with aerodynamic control and gas dynamic control system respectively is given for the homing missile direct impacting and damaging the target are studied. The simple, practical and high accurate results given in this paper give a new way to study the performance and the general rule of homing guidance and control system.