天线罩影响下的导弹制导控制系统设计

Design of Missile Guidance System with Radome Effects

针对天线罩误差对导弹制导控制系统的影响，本文提出了导引控制器的一种“综合”设计方法，这种方法是一种系统的设计方法，设计过程可由计算机实现，对设计者的经验要求较少。仿真实验表明，按此方法设计出的制导控制系统对于天线罩瞄准线误差斜率的摄动具有满意的鲁棒性。

This paper presents a synthesis method for designing missile guidance controllers under the effect of radome error. The method is a systematic method that can be carried out by computers with little needs for experience of the designer. Simulation results show that the guidance controllers designed by the method give the system satisfactory robust performance. [WT5”HZ〗