| 导弹发射架随动系统变结构控制器的设计 |
| |
| 引用本文： | 赵修平.导弹发射架随动系统变结构控制器的设计[J].系统工程与电子技术,2002,24(2):25-26. |
| |
| 作者姓名： | 赵修平 |
| |
| 作者单位： | 海军航空工程学院机械工程系,山东,烟台,264001 |
| |
| 摘 要： | 介绍了某型导弹发射架随动系统的应用技术和控制原理 ,并阐述了其控制中心———变结构控制器的构成、控制算法及软件实现。该控制器的算法依据系统误差的大小由三部分构成 :Bang -Bang控制、PID控制和FUZZY控制 ,具有快速控制精度高等优点。所设计的随动系统体积小、成本低、可靠性高、可维性好 ,具有良好的工程应用价值
|
| 关 键 词： | 导弹 随动系统 控制器 发射装置 |
| 文章编号： | 1001-506X(2002)02-0025-02 |
| 修稿时间： | 2001年3月7日 |
Design of a Variable-Structure Controller for the Missile Launcher Servo System |
| |
| ZHAO Xiu,ping.Design of a Variable-Structure Controller for the Missile Launcher Servo System[J].System Engineering and Electronics,2002,24(2):25-26. |
| |
| Authors: | ZHAO Xiu ping |
| |
| Abstract: | This paper introduces the applied technologies and control principle of a missile launcher servo system, and expounds the composition, control algorithm and software implementation of its control center--variable-structure controller. The control algorithm of the controller consists of three parts--"Bang-Bang" control algorithm, "PID" control algorithm and "FUZZY" control algorithm. The controller features high speed, high precision, etc. With the advantages of small volume, low cost,high reliability and good maintenability, the servo system has a good prospect in engineering applications. |
| |
| Keywords: | Missile Servo system Controller Launcher |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
