淡江大學機構典藏:Item 987654321/114760
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/114760


    Title: 鴻鵠太陽能飛機 : 飛控系統與地面站的設計
    Other Titles: Design of flight control system and ground station of Hong-Hu solar powered UAV
    Authors: 司徒秉昇;Szutu, Ping-Shen
    Contributors: 淡江大學航空太空工程學系碩士班
    馬德明;Ma, Der-Ming
    Keywords: 氣動力導係數;特徵矩陣;aerodynamic derivative;eigenmatrix
    Date: 2017
    Issue Date: 2018-08-03 15:03:07 (UTC+8)
    Abstract: 本篇研究主旨在於計算設計完成之太陽能飛機的氣動力導係數,並且使用氣動力導係數計算該飛機之安定性,判斷該飛機之安定性是否為穩定。再藉由飛機安定性為穩定狀態下之氣動力導係數計算出特徵矩陣,並且在Matlab/Simulink&SISOTool環境下使用特徵矩陣去設計該飛機之控制器。再使用Pixhawk與X-PLANE 10結合,模擬在類真實狀態下的飛行,驗證該控制器是否符合真實情況之飛行,最後藉此控制器使太陽能飛機能夠穩定在空中巡航。
    The main idea of this research is about calculate the aerodynamic derivate of solar powered aircraft .Moreover , we use aerodynamic derivate to manage the safety and stability of aircraft . While aircraft is stable , we use aerodynamic derivative to circulated eigenmatrix , further created the controller of aircraft in Matlab/Simulink&SISOTool environment . We use the combination of Pixhawk and X Plane 10 to imitate the real flying situation . By this experiment , we verify the controller fits the real flying situation or not .Eventually ,we are able to stabilize the solar powered aircraft to cruising with controller.
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Thesis

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