淡江大學機構典藏:Item 987654321/96496
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/96496


    Title: 拍撲式微型飛行系統之研製(I)
    Other Titles: Research on Fabrication of Flapping Micro Aerial Vehicles (I)
    Authors: 楊龍杰;王信雄;劉冠君;徐振貴;馮國華;施宏明
    Contributors: 淡江大學機械與機電工程學系
    Keywords: 微飛行器;拍撲翼;現地量測;微機電系統;壓電;Micro aerial vehicle (MAV);Flapping wing;On-site measurement;Micro-electro-mechanical system (MEMS);Piezoelectric
    Date: 2006-11
    Issue Date: 2014-03-07 11:51:36 (UTC+8)
    Abstract: 本研究以拍撲式微飛行器之實際升空飛行為研究目標。基於以往計畫執行所得之微飛行器製作技術加以精進，在本計畫前段利用微機電技術來完成飛行器之自主飛行測試，飛行距離已可達10公尺。同時借重多維度的測力設備，得出本微飛行器之空氣動力特性，包含升力係數與推力係數等量測數據。為得到更好的飛行表現，改良現有傳動系統，並透過高性能且質輕之鋰電池、多功能質輕的複合式晶片之襄助來縮減重量，以及利用類似鳥類的尾翼設計，來大幅延長本微飛行器之滯空時間。改良後的微飛行器之無線遙控飛行時間已超過10秒，距離達40公尺以上。
    The objective of this project is to develop a flapping MAV capable of flight via wireless control. Based on the previous fabricating experience of MAVs, we have a great progress in this year. The first half of the research result, we fabricated a MAV having a successful flight capability of 10-meter range by MEMS process. The aerodynamic forces of this MAV were also obtained by a multi-dimensional load-cell in the facility of the wind tunnel. In the later half year, we re-designed a smoother gear-transmission system, and kept on searching light-weighted materials for the components of the MAV. Finally, integrated all the components including a (we) wireless receiver, tail actuator, and a poly-lithium battery in(a) to the MAV. In the flight testing, the MAV had a successful flight of 40-meter range and of 10-second endurance under wireless control on flapping power and tail attitude simultaneously.
    Relation: 國科會自動化學門九十四年度專題計畫成果發表會暨學門規劃研討會論文集，6頁
    Appears in Collections:[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Proceeding

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