無尾翼無人飛行載具之設計與實現

機構典藏 > College of Engineering > Graduate Institute & Department of Aerospace Engineering > Thesis > Item 987654321/35603

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Title:	無尾翼無人飛行載具之設計與實現
Other Titles:	Design and realization of the tailless uninhabited aerial vehicle
Authors:	林源鍾;Lin, Uan-chung
Contributors:	淡江大學航空太空工程學系碩士班馬德明;Ma, Der-ming
Keywords:	無尾翼;最佳控制;無人飛機;tailless aircraft;optimal control;UAV
Date:	2008
Issue Date:	2010-01-11 06:51:26 (UTC+8)
Abstract:	本論文目標為設計無尾翼構型的UAV以及其控制系統。UAV設計採用標準飛機設計的流程，分為概念設計、初步設計、細部設計等各階段。將載具由初步的概念逐漸由各項的需求來規劃設計整體的外型與結構。姿態控制器使用狀態回授控制並以LQ最佳化方法來設計控制器的增益值，並使用MATLAB®來模擬UAV使用控制器在控制上的結果。以ARM®搭配PIC®單晶片組成整個控制系統硬體以及發展UAV使用的地面監控軟體。最後並完成設計導航與導引系統以使無尾翼構型的UAV達到自主飛行的目的。 The thesis is to design a tailless UAV and its guidance, navgation and autopilot systems. Procedure of UAV design uses standard aircraft design procedure which includes concept design, preliminary design and detail design. The configuration and structure of UAV depend on the performance reqirements. Attitude control uses state feedback control and LQ criterion to design control gain. The MATLAB® is implemented to simulate the control responses. The ARM® and PIC® microcontrollers are used to build up the avionics and ground control station.
Appears in Collections:	[Graduate Institute & Department of Aerospace Engineering] Thesis

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