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本文介绍了关于气动力控制寻的导弹雷达天线罩引起的脱靶距离的分析。文中对导弹制导系统的稳定性作了分析并研究了稳定性与脱靶距离的关系,还阐述了脱靶距离的无量纲曲线与一些重要参数,从而证明有可能在天线罩设计与气动力设计之间进行一些折中。为保证气动力设计与天线罩设计之间的适当平衡和保证系统能在实际碰到的参数允许范围内工作,在初步设计中这些折中是非常重要的。
This paper introduces the analysis of the off-target distance caused by the missile radar radome of aerodynamic control. In this paper, the stability of missile guidance system is analyzed and the relationship between stability and off-target distance is also studied. The dimensionless curve of off-target distance and some important parameters are also expounded, which proves that it is possible to design the radome design and aerodynamic design Make some compromises. These compromises are very important in a preliminary design to ensure the proper balance between aerodynamic design and radome design and to ensure that the system can work within the parameters actually encountered.