导弹舵机自适应离散滑膜控制器设计

摘要

针对所建立的导弹电动舵机的简化模型,设计了自适应离散滑膜变结构控制器,并对系统进行仿真,仿真及实验结果表明:该系统有良好的动态品质、稳定性和鲁棒性.%According to the established missile electric steering gear, the simplified model of adaptive discrete variable structure controller is designed, and in the system simulation experimental results show that the system has a good dynamic quality, stability and robustness.