- 學位論文
太陽能飛機鴻鵠之設計與實作
Design and Fabrication of Hong Hu Solar Powered Unmanned Aerial Vehicle
並列摘要
The purpose of the study is included of structure design of UAV in detail and Fabrication. The motor of the portable UAV is AXi 4130/20 kv305 electric brushless motor. This UAV has 3.7 m wingspan and 10kg weight with three parts of solar panels on the top of the wing and horizontal tail with power of 45 watt. To make the portable UAV lighter, the structure of wing is the combination of C beams and 3D printed structures.Then, 3D printed structures are designed as truss structure. From these designation, the portable UAV can be lighter.
參考文獻
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[1] 王以昕, “最小功率需求的電動無人機設計,” 於 淡江大學航空太空工程學系, 新北市, 2017.
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延伸閱讀
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- 王恩旭（2008）。太陽能動力史特靈發電系統研發與測試〔碩士論文，國立清華大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0016-2002201314193781
- 莊岱諺（2011）。太陽光電發電系統之設計與模擬〔碩士論文，健行科技大學〕。華藝線上圖書館。https://doi.org/10.6824/UCH.2011.00025
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- 柯旻江（2016）。Design and Implementation of Electrical Power System for Solar Powered High Endurance UAV〔碩士論文，國立虎尾科技大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0028-3108201614462100