本論文目的在於應用DATCOM經驗公式與圖表進行高酬載高升力UAV分析。採用可信度極高之資料庫(Data Compendium, 簡稱DATCOM)法，分析UAV飛機之空氣動力係數與穩定導數。因為低速高承載任務需要，UAV正在加裝縫翼與尾緣襟翼，本論文也將進一步分析其空氣動力與穩定特性。本論文之完成，可成為分析UAV之良好典範。

The objective of this thesis is to apply of DATCOM Empirical Formulae, Figures and Tables for the Analysis of a High-Payload and High Lift UAV. To save the expenses, a highly reliable Data Compendium (or simply, DATCOM) method is used in the analysis of aerodynamic coefficients and stability derivatives. Due to the mission requirement of high wing loading in low speed, slats and trailing edge flaps is added to the original Ce-71 UAV. More analyses for aerodynamic and stability characteristics are conducted with modification. The completion of this thesis has established a good example for analyzing the UAV.

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