某型防空导弹自适应自动驾驶仪设计  

Adaptive Autopilot Design for Air Defense Missile

作　　者：李云[1] 刘兴堂[1] 杨遵[1] 

机构地区：[1]空军工程大学导弹学院,陕西三原713800

出　　处：《弹箭与制导学报》2006年第2期27-29,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：采用模型参考自适应控制理论中的Popov超稳定性方法,设计了某防空导弹的自适应自动驾驶仪,进行了数字仿真,给出了仿真结果,得出了结论。An approach of Popov hyperstability for model reference adaptive control theory was adopted. An adaptive autopilot for air defense missile was designed. Digital simulation was made and the result was presented. Finally, some conclusion was given out.

关 键 词：模型参考自适应控制 超稳定性理论 防空导弹 自动驾驶仪 

分 类 号：TJ761.13[兵器科学与技术—武器系统与运用工程]