防災用長滯空無人飛機之設計與應用

THE DESIGN AND APPLICATION OF UAV FOR DISASTER PREVENTION

10.6652/JoCICHE.201509_27(3).0004

藍艁昕(Zao-Sin Lan)；賴維祥(Wei-Hsiang Lai)

無人飛機 ； 飛機設計 ； 自動導航 ； 遙傳影像 ； UAV ； aircraft design ； autopilot ； remote sensing

中國土木水利工程學刊

27卷3期（2015 / 09 / 01）

191 - 199

繁體中文

本研究欲實際設計一款長滯空無人飛機『龍飛-II號』設計，並進行試飛驗證以適用災後救援及勘災等用途，因此建立一套無人飛機的設計與實作流程。其任務以快速執行偵蒐之無人飛機，飛行時間預計可至4小時、酬載5kg，可自動導航及規劃航路等功能。對於載具設計的步驟包括概念設計、初步設計、穩定性分析、細部設計及實際試飛等步驟。在初步設計與細部設計的部分，對於載具的氣動力外型及升阻力表現進行計算，並求取適合的飛行點，並完成載具設計。最後透過試飛來驗證設計載具性能，包括自主導航測試及外海飛行，以確定此無人飛機之可用性。

The research is about an unmanned aircraft system (UAS) “Dragon Fly-II” which is designed for the survey and disaster prevention. The mission is defined as a quick response of UAV with 4 ~ 6 flight hours with payload of 5kg, and autopilot as well as route planning. A process of design and test is built for an unmanned aerial vehicle. It can be divided into four parts, including aircraft design, controller design, subsystem establishment, and flight test. In the first part, considering preliminary design and detail design which are including the analysis of aerodynamics, lift and drag coefficient. Then we choose appropriate flight point and design it. After the UAV design and system integration, the UAV performance can be found due to the flight test. The flight tests including performance test, autopilot test and an oversea mission in a disaster survey which ensures the UAV available.