本文为美国佛罗里达国际大学（作者：Josh Bayliss）的学士论文，共130页。

本项目的目标是设计一架无人驾驶飞机，参加每年由国际无人机系统协会组织的2013年学生无人机系统（SUAS）竞赛。这个设计项目不需要从零开始制造无人机，相反，它需要对预制产品进行充分的选择、定制和修改。SUAS竞赛由几个方面构成，这些因素决定了需要添加到无人机机身中的组件。最终设计将能够在增加GPS、高度计、计算机、自动驾驶仪、照相机等有效载荷的情况下实现至少40分钟的持续飞行。无人机的机身是一架RC飞机。

本文考虑了多种设计方案，最终的设计选择将取决于制造商的详细规格参数。此外，根据所需的推力重量比和必要的飞行距离选择合适的电机（液体燃料 vs. 电力）。机身的设计需要足够大，以容纳自动飞行所需的电子元件。机翼载荷也是一个需要考虑的问题，因此机翼设计需要满足相应的要求。

The goal of this project is to design anunmanned aerial to be entered into the 2013 Student Unmanned Aerial Systems(SUAS) competition that is organized every year by the Association for UnmannedVehicle Systems International. This design project does not entailmanufacturing UAV from the ground up. Rather, it requires adequate selection,customization, and modification of a pre-fabricated product. The SUAScompetition consists of several factors, which determine components that willneed to be added to the UAV body. The final design will be able to achievesustained flight for a minimum of 40 minutes with the added payload of GPS,altimeter, computer, autopilot, camera, etc. The body of the UAV is an RCplane. Several designs are being considered. The final design choice will hingeon manufacturer specifications. Additionally, an adequate motor (liquid fuelvs. electric) will be chosen depending on the thrust-to-weight ratio requiredand the necessary range. The fuselage of the design needs to be sufficientlylarge enough to accommodate the electronic components necessary for autonomousflight. Wing loading is also of concern, thus the wing design needs to beappropriate.

1 引言

2 设计方案比较

3 设计分析

4 无人机主要组件

5 结构设计

6 成本分析

7 原型系统描述

8 原型系统测试计划

9 设计制造

10 测试

11 项目管理

12 全面学习的内容

13 未来工作展望

14 结论

15 参考文献

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