本論文提出一種用於汽油引擎無人機上的輔助電力系統以延長無人機的飛行時間，系統的結構設計和主要的配件選用將在論文中的細節討論。本論文主要的目標是將汽油引擎具有的高推力或高升力的優點用於無人機上同時設計一個輔助電力系統可以用於固定翼或垂直起降的汽油引擎無人機。此系統將在測試中驗證了選用的引擎通過發電機可提供三百瓦的連續能量輸出。實驗結果證明此方法應用在汽油引擎無人機的可行性。

This thesis presents an auxiliary power generation system for engine powered UAV to extend its flight endurance. System architechtre design with appropriate main component selectrion is detailed discussed. The proposed idea tries to take the advantages of engine power for lift or thrust, and also create auxiliary power for the UAVs wither for vertical take-off and landing or fixed wing. The proposed system is constructed with primary test to get 300W continuous power for UAV. The results show the proposed idea is feasible and useful for UAV developments.

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