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首页> 外文期刊>Transactions of the Japan society for aeronautical and space sciences >A Split-wing Micro Air Vehicle
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A Split-wing Micro Air Vehicle

机译：裂翼微型飞行器

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摘要

This paper presents a proposal for a split-wing aircraft. The split wing proposed is composed of a number of square plates. The distances between the square plates are varied according to flight conditions. For a flight where high efficiency is required, the distances are 0 and the characteristic of the wing is that of a wing with an aspect ratio equal to the number of square plates. On the other hand, during a flight where wind gusts are experienced, the distance is not 0 and the characteristic of the wing is close to that of a square. The split-wing enhances the flight stability of MA Vs. The enhanced stability will increase opportunities where MAVs can be utilized.
机译：本文提出了一种裂翼飞机的建议。提议的分流机翼由许多方形板组成。方板之间的距离根据飞行条件而变化。对于需要高效率的飞行，距离为0，机翼的特性是长宽比等于方板数的机翼的特性。另一方面，在经历阵风的飞行中，该距离不为0，并且机翼的特性接近正方形。分裂式机翼提高了MA V的飞行稳定性。增强的稳定性将增加使用MAV的机会。

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