摘要
由于对付TBM的高层反导防空导弹速度很高,气动加热问题十分严重,采用侧窗探测方式解决气动热影响问题。研究了侧窗探测条件下的制导控制技术,给出了拦截器的姿态控制规律,并进行了仿真。仿真结果表明给出的姿态控制规律是可行的。
Velocity of aerial defense missile,which is used to intercept TBM,is very high,so pneumatic pyrogenation is terrible.Side window detection is used to decreasing pneumatic pyrogenation.Control and guide method for side window detection is studied,attitude control law of interceptor is given,and simulation test is done.Simulation results indicate the attitude control law is viable.
出处
《现代防御技术》
北大核心
2007年第5期71-75,共5页
Modern Defence Technology
关键词
侧窗探测
制导控制
姿态控制
side window detection
control guidance
attitude control
