摘要
根据防空导弹飞行控制系统的特点,通过线性二次型的系统设计,推导出了具有最佳反馈的回路结构。按照实际系统的测量状态,构成了复合反馈的飞行控制系统,并对具有复合反馈飞行控制系统的性能和特点进行了分析,同时对回路的设计也进行了讨论。
In this paper driving a loop with a best feedback by thelinear quadratic system design according to the feature of flight controlsystem of air defense missiles. A flight control system with a compoundfeedback is constituted in the light of the measuring status of a real system,and the performance and feature of the flight control system with compound feedbaek are analyzed. The design about the loop is also discussed.
出处
《上海航天》
1995年第5期11-18,共8页
Aerospace Shanghai
关键词
防空导弹
飞行控制系统
回路设计
Air-defense missile, Flight control system, loop design,Robustness