期刊文献+

拍翼模型实验中一种控制实验模型运动的新方法 被引量:1

A new approach to control the motion of the model on flapping-wing model investigation
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摘要 设计了一套运动机构和控制系统,利用单片机控制存储器以恒定速度读写来实现步进电机的位移脉冲,使实验模型按拍翼运动规律同步地平动和转动。叙述了实验装置的机械结构和控制系统组成,同时还对实验结果进行了分析。 A type of device and the corresponding kinetic control system were developed. The step time of stepper motors were realized by using a microcontroller to control the read-wrlte velocity of storage and flappingwing motions of heaving and pitching in phase for the experimental model are obtained. And the structure of the mechanism and the composing of the control system are described. Also some of the experimental results were analyzed.
出处 《实验流体力学》 EI CAS CSCD 北大核心 2006年第1期45-48,共4页 Journal of Experiments in Fluid Mechanics
基金 中国科学院创新项目(No.KJCX-SW-L2No.KJCX-SW-L04)
关键词 拍翼运动 实验模型 步进电机 单片机 flapping-wing motion experimental model stepper motor microcontroller
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参考文献4

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同被引文献6

  • 1赵攀峰,刘春阳,祝隆伟,陈小燕,杨基明.二维平板翼拍翼运动的涡流场显示[J].中国科学技术大学学报,2005,35(4):441-447. 被引量:5
  • 2Ansari S A, Zbikowski R, Knowles K. Aerodynamic Modelling oflnsect - like Flapping Flight for Micro air Vehicles [ J ]. Progress in Aerospace Sciences,2006(42) : 129 -172.
  • 3Sun M, Lan SL. A Computational Study of the Aerodynamic Forces and Power Requirements of Dragon Fly (Aeschnajuncea) Hovering[J]. J Exp Biol 2004(207) : 1887 - 1901.
  • 4Sun M. High - lift Generation and Power Requirements of Insect Flight [ J ]. Fluid Dyn Res, 2005 ( 37 ) :21 - 39.
  • 5Platzer M F, Jones K D, Lund T G. Experimental and Computational Investigation of Flapping Wing Propulsion for Micro - air Vehicles[ R]. Symposium of Low- Reynolds Number Vehicles, University of Notre Dame, Indiana: 2000.
  • 6宋笔锋,白存儒,钟诚文,李为吉,候宇.微型扑翼机风洞试验探索性研究[J].流体力学实验与测量,2003,17(U09):37-40. 被引量:8

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