论文部分内容阅读
提出了一种新的时变模型参考变结构控制方案，设计了某型ＢＴＴ导弹俯仰偏航耦合通道自动驾驶仪控制律。该方案能有效地解决ＢＴＴ导弹通道间强烈的耦合现象，适应气动参数大范围变化，改善自动驾驶仪的动态性能和稳定性。
A new variable structure control scheme based on time-varying model is proposed. The control law of autopilot for a certain BTT missile pitch-yaw coupling is designed. The scheme can effectively solve the strong coupling between BTT missiles, adapt to a wide range of aerodynamic parameters and improve the dynamic performance and stability of the autopilot.