设计某寻的导弹的自动驾驶仪回路 ,使导弹控制系统在正确响应制导指令的同时 ,对弹体气动力参数变化、量测噪声等具有很好的抑制作用 .将模型参考自适应控制方法与变结构控制方法相结合 ,为某型导弹设计了结构简单、实现方便的模型参考变结构控制系统 .仿真结构表明 ,模型参考变结构自动驾驶仪不仅能准确传递制导指令 ,而且具有很好的鲁棒性 ,能有效地抑制气动力浮动、量测噪声等干扰因素 The design of a missile autopilot circuit makes the missile control system have a good suppressive effect on the projectile aerodynamic parameter variation and measurement noise while correctly responding to the guidance instructions.The model reference adaptive control method and A variable structure control method is combined to design a model reference variable structure control system with simple structure and convenient implementation for a certain type of missile.The simulation structure shows that the model reference variable structure autopilot can not only transmit the guidance command accurately but also has good Lu Excellent, can effectively inhibit the aerodynamic fluctuations, noise and other interference measurement