空面导弹模型参考自适应控制设计与仿真  

Design and simulation of model reference adaptive control for air-to-surface missile

作　　者：史鲲[1] 张效义 陈勇 唐硕[1] 

机构地区：[1]西北工业大学航天学院,陕西西安710072 [2]中航洪都集团660所,江西南昌330024

出　　处：《飞行力学》2010年第3期51-54,共4页Flight Dynamics

摘　　要：为提高空面导弹控制系统的性能,解决传统PID控制在导弹大空域飞行、系统参数大范围变化时控制能力欠缺的问题,以法向过载作为被控量代替对迎角、侧滑角的控制,基于波波夫超稳定性理论设计了模型参考自适应控制器。六自由度仿真结果表明,所设计的自适应控制器具有良好的控制性能和鲁棒性。Traditional PID controller is lack of control ability when a missile flies in large range and its system parameters change in great bound.In order to improve the performance of air-to-surface missile＇s control system,the overload was taken as the controlled variable instead of the angle of attack and the slide angle,and a model reference adaptive controller was designed based on Popov＇s hyperstability theory.The results of six-degree-of-freedom simulation show that the designed adaptive controller has good control property and robustness.

关 键 词：空面导弹 过载 自适应控制 六自由度仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]