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某型导弹发射装置伺服系统的滑模控制器设计与仿真
引用本文:王天辉,赵修平,徐广.某型导弹发射装置伺服系统的滑模控制器设计与仿真[J].舰船电子工程,2011,31(6):189-191.
作者姓名:王天辉  赵修平  徐广
作者单位:1. 海军航空工程学院研究生管理大队,烟台,264001
2. 海军航空工程学院飞行器工程系,烟台,264001
摘    要:在某些装置的伺服系统中,对系统的动态品质要求很高,传统的PID控制往往难以满足要求。以某型导弹发射装置的伺服系统为模型,设计了滑模控制器。通过与传统的PID控制器仿真对比,可以看出应用滑模控制器使伺服系统的动态品质有很大的改善。

关 键 词:伺服系统  滑模控制  PID

Sliding Mode Controler's Design and Simulation of Certain Type Missile Lancher's Servo System
Wang Tianhui,Zhao Xiuping,Xu Guang.Sliding Mode Controler's Design and Simulation of Certain Type Missile Lancher's Servo System[J].Ship Electronic Engineering,2011,31(6):189-191.
Authors:Wang Tianhui  Zhao Xiuping  Xu Guang
Institution:Wang Tianhui1) Zhao Xiuping2) Xu Guang1)(Administrant Brigade of Postgraduate,Naval Aeronautical & Astronautical University1),Yantai 264001)(Dept.of Aircraft Engineering,Naval Aeronautical & Astronautical University2),Yantai 264001)
Abstract:The dynamic performance of some servo system is required strict,and the traditional PID control is often difficult to satisfy the requirement.According to the model of a missile launcher servo system,the sliding mode control is designed.Compared with the traditional PID,we can find that the dynamic performance of some servo system is highly improved.
Keywords:servo system  sliding control  PID  
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