航空兵器Issue(1)：25-27,33,4.
舵机间隙环节对控制系统的影响分析
Influence Analysis of Actuator＇s Gap on Control System
李友年 1陈星阳1
作者信息
- 1. 中国空空导弹研究院,河南洛阳471009
- 折叠
摘要
Abstract
There are some non-linear parts in the actuator of missile, such as the gap and the like. Adopting the methods of analyzing linear system can not get the result that they impact the control system. In this paper, an application of description function is used to analyze the influence for control system, and leading correction net work is used to eliminate this influence.关键词
间隙环节/描述函数/超前校正网络Key words
gap/description function/leading correction net work分类
军事科技引用本文复制引用
李友年,陈星阳..舵机间隙环节对控制系统的影响分析[J].航空兵器,2012,(1):25-27,33,4.
