导弹滚动回路的变增益参数设计

Variable gain parameter desigin for missile rolling loop

研究了一个导弹自动驾驶仪角度稳定回路半实物仿真问题，针对滚动回路出现的特殊现象和问题，进行了较为详尽的分析。在此基础上，进行了变增益参数设计。设计方法简单，用弹上数字计算机实现也很容易，而且可以收到很好的控制效果。

Hardwre-in-the-loop simulation problems for angular stabilization loop of a missile autopilot are studied and a detailed analysis is made on the specific phenomena and problems occurred in the rolling loop.On this basis,varial gain parameter design has been made.The design methed is simple,it is very easy to realize by means of digital computer on board ,the missile and very good control effects can be achieved. [