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| 飞行器伺服控制系统开发技术的研究与应用 | |
| 引用本文： | 贾新强,严忠,卢建华.飞行器伺服控制系统开发技术的研究与应用[J].海军航空工程学院学报,2010,25(1):45-48, 64. |
| 作者姓名： | 贾新强 严忠 卢建华 |
| 作者单位： | 1. 海军驻西安东郊航空设备军事代表室,西安,710065 2. 92213部队,山东,烟台,264001 3. 海军航空工程学院,控制工程系,山东,烟台,264001 |
| 摘 要： | 介绍了一种新的控制系统设计方法和工具IEE(工程集成环境),并将此方法应用到飞行器直接驱动舵机(DDA)数字伺服控制系统开发过程中,完成了快速原型系统的设计与试验,取得了较好的效果,证明了IEE设计方法的可行性和先进性。 |
| 关 键 词： | IEE 伺服控制系统 DDA MATIAB xPC |
Research and Application in Development Technology of Aircraft Servo-Control System |
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| JIA Xin-Qiang,YAN Zhong and LU Jian-hua.Research and Application in Development Technology of Aircraft Servo-Control System[J].Journal of Naval Aeronautical Engineering Institute,2010,25(1):45-48, 64. | |
| Authors: | JIA Xin-Qiang YAN Zhong and LU Jian-hua |
| Institution: | 1. Aviation Equipment Military Representatives Office of Navy in East ofXi＇an, Xi＇an 710065, China： 2. The92213rd UnitofPLA, Yantai Shandong264001, China： 3. Department of Control Engineering, NAAU, Yantai Shandong264001, China) |
| Abstract: | In this paper, a new kind of design method for the control system and the engineering tool lEE （integrated engineering environment） were introduced. It was applied to the development process of the aircraft direct driving actuator （DDA） digital servo-control system and accomplished the design and test of fast prototype system, in which it achieved a better result. It proved the feasibility and the level of advancement of this design method. |
| Keywords: | IEE DDA MATLAB xPC |
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