飞行力学在图像制导导弹设计中的应用

为满足作战需要 ,改善导弹的总体性能 ,又有利于降低研制成本 ,对图像制导导弹的导引头最大跟踪角速度、极限框架角、搜索方案以及导弹的速度方案 ,进行了分析设计。以此为例 ,对飞行力学在导弹总体与分系统设计中的应用进行了说明。研究结果表明 :飞行力学是协调导弹总体与各分系统之间关系的重要手段 ,在导弹总体和各分系统的设计过程中 ,积极主动地应用飞行力学进行综合设计 ,可获得最佳的总体性能。

The use of flight dynamics in image guided missile design

To satisfy tactical needs, improve overall performance of the missile and reduce developing cost, the maximum tracking speed, the limit frame angle and the searching program of the imaging seeker and the speed program of an image guided missile are analyzed. Taken these problems as examples, the application of flight dynamics in design of missile and its sub systems is shown.The results show that flight dynamics is an essential tool to harmonize relations between missile and its sub system. For optimal overall performance, it is necessary to use flight dynamics in comprehensive design of missile and its sub systems.