| 风洞试验模型舵机系统研制 |
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| 引用本文： | 王辉,肖京平,高大鹏,柳庆林,秦三春,王文慧.风洞试验模型舵机系统研制[J].气动实验与测量控制,2012(3):72-75. |
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| 作者姓名： | 王辉 肖京平 高大鹏 柳庆林 秦三春 王文慧 |
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| 作者单位： | [1]中国空气动力研究与发展中心,四川绵阳621000 [2]四川大学电气信息学院,成都610065 |
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| 摘 要： | 提高试验效率一直是风洞试验的目标之一。介绍了中国空气动力研究与发展中心新研制的风洞试验模型舵机系统。地面调试与试验验证结果表明，新系统控制精度在满足国标要求的前提下，可大幅提高试验效率，降低能耗，具有很高的推广价值。
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| 关 键 词： | 飞行器 舵机 风洞试验 微电机 |
Research on automatic control system of wind tunnel test model |
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| Authors: | WANG Hui XIAO Jing-pingI GAO Da-peng LIU Qing-lin QIN San-chun WANG Wen-hui |
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| Institution: | 1. China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China; 2. College of Electrical Engineering and Information Technology, Sichuan University, Chengdu610065, China) |
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| Abstract: | Improving the efficiency has always been one goal of wind tunnel test. In this pa- per, the automatic control system on aircraft model in wind tunnel test developed by China Aero- dynamics Research and Development Center is introduced. The results of debugging on ground and validation test indicate that the accuracy of the automatic control system meets the require- ment of wind tunnel test national standard. The efficiency of wind tunnel test has been improved highly, and the energy cost has been decreased appreciably. The new system is worthy of promotion. |
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| Keywords: | aircraft automatic control system wind tunnel test small electric motor |
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