摘要
利用状态反馈实现了航空发动机的动态解耦。在解耦时不需要增加新的状态反馈即可实现解耦系统的任意极点配置。最后的算例表明了该方法的有效性。
This paper discusses how to realize the dynamic decoupling of aero engine by state feedback.It states that the realization of optional poles disposition of dicoupling system can be achieved without adding new state feedback when decoupling.It illustrates the effectiveness of this method with an example.
出处
《中国民航学院学报》
1998年第3期1-4,共4页
Journal of Civil Aviation University of China
