淡江大學機構典藏:Item 987654321/38241
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/38241


    Title: 單旋槳垂直起降飛行載具穩定增強器的設計與模擬
    Other Titles: Design and simulate enhance stability controller for single propeller VTOL
    Authors: 馬德明;江榮德
    Contributors: 淡江大學航空太空工程學系
    Keywords: 單旋槃飛行載具;垂直起降;穩定增強器;VTOL;single propeller vehicle;enhance stability controller
    Date: 2001-03
    Issue Date: 2010-01-11 14:57:48 (UTC+8)
    Publisher: 新竹縣：中華民國燃燒學會
    Abstract: 淡江大學無人飛行載具實驗室參考目前現有的幾種垂直起降的形式完成製作單旋槳垂直起降無人飛行載具模型飛機，主要採用由格魯曼公司工程師所開發的Vertigo 設計概念:以單引擎及穩定控制舵片來達成垂直起降。然而，在垂直起降時由於推力中心在重心下方，形成倒單擺模式，以及單旋槳所產生的扭矩問題，並無法完全由穩定控制舵片克服，因此，必須對垂直起降載具的飛行模式暸解及分析六自由度的運動方程式後而設計一穩定增強器以補控制舵片之不足。
    TKU UAV LAB takes VERTIGO concept design to build up single propeller VTOL vehicle. But we face the problem: when vertical taking off and Transition, control van below the center of gravity .It is unstable like Inverse pendulum. In this paper, we will design an enhance stability controller and simulate it to satisfy fly quality.
    Relation: 中華民國2001燃燒學會民航學會航太學會學術聯合會議論文集=CIROC CSCA AASRC joint conference，頁AA619-AA624
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

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