舵机间隙环节对控制系统的影响分析
타궤간극배절대공제계통적영향분석
Influence Analysis of Actuator＇s Gap on Control System
  • 万方数据
    航空兵器 항공병기
    HANGKONG BINGQI
    2012年 1期 25-27,33 ,共4页

    李友年%陈星阳

    리우년%진성양

    间隙环节%描述函数%超前校正网络 間隙環節%描述函數%超前校正網絡
    간극배절%묘술함수%초전교정망락
    gap%description function%leading correction net work
    导弹的舵机中存在间隙等非线性环节,而采用线性系统的分析方法无法分析出它们对控制系统的影响。本文主要介绍了采用描述函数法分析间隙环节对控制系统的影响,并采用超前校正网络来消除此影响。
    도탄적타궤중존재간극등비선성배절,이채용선성계통적분석방법무법분석출타문대공제계통적영향。본문주요개소료채용묘술함수법분석간극배절대공제계통적영향,병채용초전교정망락래소제차영향。
    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.
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