弹用舵机的状态变量反馈控制系统设计

摘要

Based on the analysis of missile steering system , the transfer function model is established .Combined with the use condition of operating actuator ,three system performance indicators are set up .Using state variable feedback control theory ,the model for closed‐loop system is designed .Through MATLAB simulation analysis ,the performance of the control system is verified .%通过对弹用舵机系统的分析，建立了舵机系统的传递函数模型。结合舵机的使用工况，拟定了3项系统性能指标。利用状态变量反馈控制理论，对模型进行了闭环系统设计。通过MATLAB仿真分析，验证了控制系统的性能。