低空长航时太阳能无人机的关键设计参数

AFRICON 2009 Pub Date : 2009-11-03 DOI:10.1109/AFRCON.2009.5308105

Grant Wilkins, D. Fourie, J. Meyer

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引用次数: 16

摘要

本文提供了太阳能无人机长时间飞行所需的关键参数的理论研究结果。参数为电池能量密度、机翼表面积、无人机总重量和太阳表面积。这些发现是基于两个独立的模型，一个太阳能模型和一个空气动力学模型，这两个模型结合起来形成了一个太阳能无人机模型。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Critical design parameters for a low altitude long endurance solar powered UAV

The paper presented provides theoretical findings of the critical solar UAV parameters required for prolonged flight. The parameters being, battery energy density, wing surface area, total UAV weight and solar surface area. The findings are based on two individual models, a solar and an aerodynamic model, which are combined to form a solar powered UAV model.

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来源期刊

AFRICON 2009

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