本論文之主要目的在於研究一可於無合適跑道條件下進行起降作業之固定翼飛行載其,提供第一緣人員在裝備及起降場地缺乏之任務現場附近執行即時空中偵照任務。本文內容則依研究計劃之時程,分為任務定義、機體設計、飛行力學模型建立、控制器模擬、載具製造、航電系統概念與試飛計劃等幾個階段。 The goal of this paper is the study of a portable fixed wing unmanned aerial vehicle for the first line operators. The vehicle that can be launched by hand and landing without runway or well-paved landing field and has real-time reconnaissance capability. With the schedule of study project, this article will include Mission Requirement, Vehicle Design, Vehicle's Flight Dynamic Model, the Simulation of Controller Design, Making ofthe Vehicle, Concept of Avionic System and the Schedule ofTest Flight.