飞翼式复合无人机设计与任务精度分析

Dong-gyu Sung, Eun-hak Koh, Ju-Chan Kim, Y. Nam, Jeong-ho Lee, Jae-seung Lee, Chan-bin Lee, Yeong-bae Jeon, Cheol-kyun Choi, Jae-Woo Lee
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引用次数: 0

摘要

结合固定翼和旋翼的复合型无人机是一种可以垂直起降的飞行器,固定翼可以增加飞行时间,飞行速度更快。根据添加推力矢量或升力风扇的方式和旋翼位置的不同,复合无人机分为多种类型。在本研究中,我们设计并制造了一种固定翼4个V-TOL电机的复合材料无人机,并将任务分配给航空机体,通过实际飞行试验来判断任务精度。本研究采用的设计过程和任务评估过程可用于各种无人机的开发。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flying-wing Type Compound Drone Design and Mission Accuracy Analysis
A compound drone that combines a fixed wing and a rotary wing is an aircraft that can take off and landing vertically, and can increase flight time and fly faster with fixed wings. The compound drones are divided into many types depending on the method of adding the thrust vectoring or the lift fan and the position of the rotor. In this study, we designed and fabricated a composite drone with four V-TOL motors in a fixed-wing, and assigned missions to the aviation body, hence judged mission accuracy using the actual flight test. The design process and the mission evaluation process employed in this study can be utilized on the development of various unmanned aerial vehicle.
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