导弹混合导引规律设计与仿真研究

Research on Design and Simulation of Missile's Variable Structure Control Method

通过分析导弹的拦截几何和现有控制规律,给出了模糊控制器的设计。将滑模变结构控制与模糊逻辑导引规律有机结合,给出了一种滑模变结构混合模糊逻辑导引规律,通过导弹制导控制半实物系统平台进行仿真,验证了所设计的导引规律的正确性和有效性。

A simulation program was designed based on missile features and its guidance and control system. The hardware-in-the-loop simulation platform for guidance and control system was built to prove the guidance law. The simulation results prove this hardware-in-the-loop simulation platform is feasible and the designed adaptive sliding guidance law is effective.