多旋翼无人机接触式结构健康监测技术

R. Watson, Taiyi Zhao, Dayi Zhang, Mina Kamel, C. Macleod, G. Dobie, G. Bolton, Antoine Joly, S. G. Pierce, Juan Nieto
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引用次数: 1

摘要

使用无人机(uav)进行结构健康监测(SHM)已经成为民用和能源发电应用中常见的危险或耗时的检查过程。在非接触式远程视觉检测无人机提供的表面筛选的基础上,系统现在开始采用基于接触式无损评估(NDE)换能器来检测和监测早期的地下缺陷。然而,在空气动力学干扰下,传统的多旋翼平台动力学对环境相互作用的挑战阻碍了传感器稳定和可重复放置的努力。本文对两种不同的无人机系统进行评估,作为克服这些挑战的一种手段。第一种利用矢量推力与三直升机布局。它可以动态重定向双轴倾斜螺旋桨,直接影响相互作用力,并在全向目标上部署干耦合超声测厚。在静态点和滚动扫描测量中,实验室测试表明平均绝对误差分别小于0.1 mm和0.3 mm。第二种无人机使用刚性固定的多向螺旋桨反转和重定向它的净推力。降落在圆柱形结构上,它可以绕着圆柱形结构的圆周爬行,在没有磁性或真空粘附的情况下支撑自己。任意静态位置保持在0.7 mm的平均偏差之内。最后,对每个系统的比较讨论为进一步发展基于接触式的空中SHM及其在工业实践中的采用提供了策略。
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TECHNIQUES FOR CONTACT-BASED STRUCTURAL HEALTH MONITORING WITH MULTIROTOR UNMANNED AERIAL VEHICLES
Use of Unmanned Aerial Vehicles (UAVs) for Structural Health Monitoring (SHM) has become commonplace across civil and energy generation applications with hazardous or time-consuming inspection processes. Expanding upon surface screening offered by non-contact remote visual inspection UAVs, systems are now beginning to incorporate contact-based Non-Destructive Evaluation (NDE) transducers to detect and monitor incipient sub-surface flaws. However, challenges to environmental interaction using conventional multirotor platform dynamics amid aerodynamic disturbances have frustrated efforts for stable and repeatable sensor placement. Herein, two distinct UAV systems are evaluated as a means to overcome these challenges. The first utilizes vectored thrust with a tri-copter layout. It may dynamically reorient dual-axis tilting propellers to directly effect interaction force and deploy drycoupled ultrasonic thickness measurement across omnidirectional targets. In static point and rolling scan measurement, laboratory tests demonstrate mean absolute error below 0.1 mm and 0.3 mm, respectively. The second UAV uses rigidly affixed multidirectional propellers to reverse and redirect its net thrust. Landing atop cylindrical structures it may crawl around their circumference, supporting itself without magnetic or vacuum adhesion. Arbitrary static position is maintained to within a mean deviation of 0.7 mm. Lastly, comparative discussion of each system informs strategies for further development of contact-based aerial SHM and its adoption to industrial practice.
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