| 基于PXI的舵机仿真器伺服系统控制方法 |
| |
| 引用本文： | 冷颖.基于PXI的舵机仿真器伺服系统控制方法[J].海军航空工程学院学报,2008,23(2):132-134. |
| |
| 作者姓名： | 冷颖 |
| |
| 作者单位： | 海军驻北京地区配套设备军事代表室,北京,100001 |
| |
| 摘 要： | 舵机是导弹飞行控制系统的执行机构,导弹的各种姿态运动都是靠舵机带动舵面偏转来实现的。文章在详细介绍舵机仿真器硬件设计基础上,完成了系统软件设计,对伺服系统进行了仿真,分析了系统的性能。
|
| 关 键 词： | 舵机 伺服系统 控制器设计 仿真 |
| 文章编号： | 1673-1522(2008)02-0132-03 |
| 修稿时间： | 2007年8月30日 |
Research on the Controlling Methods for Rudder Simulator Servo System Based on PXI |
| |
| LENG Ying.Research on the Controlling Methods for Rudder Simulator Servo System Based on PXI[J].Journal of Naval Aeronautical Engineering Institute,2008,23(2):132-134. |
| |
| Authors: | LENG Ying |
| |
| Institution: | LENG Ying(Matching Equipment Military Representatives Office of Navy in Beijing, Beijing 100001, China) |
| |
| Abstract: | Missile rudders are executive bodies of missile flight control system. All kinds of attitude motion of missile are depended on the actuator driver fins of rudder. The software designs of the electrical servo system were completed after the hardware designs were presented in details. Then simulation and analysis of the servo system were carried out. |
| |
| Keywords: | rudder servo system designs of controller simulation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《海军航空工程学院学报》浏览原始摘要信息 |
| 点击此处可从《海军航空工程学院学报》下载免费的PDF全文 |
