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    請使用永久網址來引用或連結此文件: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/120829

    題名: Design, Manufacturing, and Flight Testing od an Experimental Flying Wing UAV
    作者: Chung, Pei-Hsiang;Ma, Der-Ming;Shiau, Jaw-Kuen
    關鍵詞: UAV design;flight testing;flying wing
    日期: 2010-07-28
    上傳時間: 2021-06-10 12:10:21 (UTC+8)
    摘要: This paper presents the design, manufacturing, and flight testing of an electric-powered
    experimental flying wing unmanned aerial vehicle (UAV). The design process starts with defining
    the performance requirements including the stall speed, maximal speed, cruise altitude, absolute
    ceiling, and turn radius and speed. The wing loading and associated power loading are obtained
    based on the defined performance requirements. The wing area, UAV mass, and power requirements
    are determined from the endurance and payload requirements. The power requirement determines
    the motor size. Aerodynamics and stability designs are obtained based on the selected airfoil and
    obtained wing area. After completing the design, the UAV is manufactured using composite materials.
    The UAV is equipped with an AXi 4130/20 kv305 brushless motor and a Pixhawk flight control board.
    Its total weight is 8.6 kg. Flight tests were conducted to evaluate the UAV’s performance and dynamic
    characteristics and to demonstrate the success of the design.
    關聯: Applied Science 9(15), 3043
    DOI: 10.3390/app9153043
    顯示於類別:[航空太空工程學系暨研究所] 期刊論文


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