English  |  正體中文  |  简体中文  |  全文筆數/總筆數 : 58317/91854 (63%)
造訪人次 : 14002389      線上人數 : 218
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜尋範圍 查詢小技巧:
  • 您可在西文檢索詞彙前後加上"雙引號",以獲取較精準的檢索結果
  • 若欲以作者姓名搜尋,建議至進階搜尋限定作者欄位,可獲得較完整資料
  • 進階搜尋
    請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/60561

    題名: Smart flapping wings with a PVDF sensor to modify aerodynamic performance of a micro UAV
    作者: Yang, Lung-jieh;Hsu, Cheng-kuei;Feng, Chao-kang;Shih, H.-M.;Feng, G.-H.;Gao, M.-W.
    貢獻者: 淡江大學機械與機電工程學系
    關鍵詞: Micro UAV;flapping wing;polyvinylidene fluoride
    日期: 2007-06-10
    上傳時間: 2011-10-14 14:44:08 (UTC+8)
    出版者: N.Y.: IEEE (Institute of Electrical and Electronic Engineers)
    摘要: This paper describes a new configuration of flapping wings to study the aerodynamic behavior of a microUAV (unmanned aerial vehicle). The flapping wings are composed of a pure parylene right wing and a PVDF-parylene composite left wing on purpose. The PVDF (polyvinylidene fluoride) sensor could only export the lift signals from the left wing. In comparison to the total lift signal picked by the load cell from the wind-tunnel facility, we can figure out and separate the lift contributions donated by left wing and right wing, respectively. Therefore, we found a new design methodology to adjust the aerodynamic performance of microUAVs by changing the phase lag between the two flapping wings through fine tuning the mechanism linkages.
    關聯: Technical Digest of the 14th International Conference on Solid-State Sensors, Actuators and Microsystems (Transducers '07-Lyon), pp.1705-1708
    DOI: 10.1109/SENSOR.2007.4300480
    顯示於類別:[機械與機電工程學系暨研究所] 會議論文


    檔案 描述 大小格式瀏覽次數
    Smart flapping wings with a PVDF sensor to modify aerodynamic performance of a micro UAV.pdf538KbAdobe PDF338檢視/開啟



    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - 回饋