摘要
在运用逆奈奎斯特阵列法对某自旋导弹的姿态控制系统进行设计时,针对某自旋导弹姿态控制系统中各通道之间存在着强耦合的特点,采用了串联补偿和局部反馈相结合的方法对其实现了解耦,从而设计出了能满足动、静态性能要求的姿态控制器,并给出了仿真结果。
With inverse Nyquist array method in design of affitude control system for a self-spin missile, the series compensation combined with local feedback is put forward to decouple the close coupling a-mong the loops in the attitude control system of the self-spin missile. The attitude controller is designed then and the simulation results are presented, which show the system meets the dynamic and static performance specifications.
出处
《火炮发射与控制学报》
北大核心
2003年第z1期30-32,38,共4页
Journal of Gun Launch & Control
关键词
解耦
逆奈奎斯特法
控制器
仿真
decouple
inverse nyquist array
controller: simulation
