Never landing drone: Autonomous soaring of a unmanned aerial vehicle in front of a moving obstacle

IF 1.5 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Chris PL de Jong, B. Remes, Sunyou Hwang, C. De Wagter
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引用次数: 3

Abstract

Increasing endurance is a major challenge for battery-powered aerial vehicles. A method is presented which makes use of an updraft around obstacles to decrease the power consumption of a fixed-wing unmanned aerial vehicle. A soaring flight controller has been developed that can autonomously soar while the unmanned aerial vehicle keeps its relative position to that of a moving object. Multiple simulations have been performed to analyse the limitations of the soaring controller under different conditions. The effect of a change in wind velocity and updraft has been analysed. The simulations showed that an increase in updraft decreases the energy consumption of the flight controller. An increase in wind velocity results in a higher updraft requirement, while a decrease in the wind velocity requires less updraft. The simulations achieved sustained flight at 0% throttle. The controller has been validated experimentally using the updraft generated by a moving ship. The practical, autonomous tests reduced the average throttle down to 4.5% in front of a ship. The method presented in this study achieved successful hovering flight using an energy control module for longitudinal positioning.
永不着陆的无人机:无人机在移动障碍物前自动飞行
提高续航能力是电池驱动飞行器面临的一大挑战。提出了一种利用障碍物周围的上升气流来降低固定翼无人机功耗的方法。已经开发了一种飞行控制器,当无人机保持其与移动物体的相对位置时,该控制器可以自主飞行。已经进行了多次仿真来分析在不同条件下翱翔控制器的局限性。分析了风速和上升气流变化的影响。模拟表明,上升气流的增加会降低飞行控制器的能耗。风速的增加会导致更高的上升气流需求,而风速的降低则需要更少的上升气流。模拟实现了在0%油门下的持续飞行。该控制器已通过使用移动船舶产生的上升气流进行实验验证。实际的自主测试将船前的平均油门降低到4.5%。本研究中提出的方法使用能量控制模块进行纵向定位,成功实现了悬停飞行。
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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来源期刊
CiteScore
3.00
自引率
7.10%
发文量
13
审稿时长
>12 weeks
期刊介绍: The role of the International Journal of Micro Air Vehicles is to provide the scientific and engineering community with a peer-reviewed open access journal dedicated to publishing high-quality technical articles summarizing both fundamental and applied research in the area of micro air vehicles.
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