Development of a Novel Implementation of a Remotely Piloted Aircraft System over 25 kg for Hyperspectral Payloads

IF 4.4 2区 地球科学 Q1 REMOTE SENSING
Drones Pub Date : 2023-10-27 DOI:10.3390/drones7110652
Juan Pablo Arroyo-Mora, Margaret Kalacska, Oliver Lucanus, René Laliberté, Yong Chen, Janine Gorman, Alexandra Marion, Landen Coulas, Hali Barber, Iryna Borshchova, Raymond J. Soffer, George Leblanc, Daniel Lavigne, Ludovic Girard, Martin Bérubé
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Abstract

A main aspect limiting the operation of low-altitude remotely piloted aircraft systems (RPAS) over 25 kg, integrating pushbroom hyperspectral sensors, comes from the challenges related to aircraft performance (e.g., flight time) and regulatory aspects deterring the users from pushing beyond this weight limit. In this study, we showcase a novel implementation using the DJI Agras T30 as an aerial system for integrating an advanced hyperspectral imager (HSI, Hyspex VS-620). We present the design and fabrication approach applied to integrate the HSI payload, the key considerations for powering the HSI and its gimbal, and the results from vibration and wind tunnel tests. We also evaluate the system’s flight capacity and the HSI’s geometric and radiometric data qualities. The final weight of the T30 after the integration of the HSI payload and ancillary hardware was 43 kg. Our vibration test showed that the vibration isolator and the gimbal reduced the vibration transmission to above 15 Hz but also introduced a resonant peak at 9.6 Hz that led to vibration amplification in the low-frequency range near 9.6 Hz (on the order of an RMS of ~0.08 g). The wind tunnel test revealed that the system is stable up to nearly twice the wind speed rating of the manufacturer’s specifications (i.e., 8 m/s). Based on the requirements of the Canadian Special Flight Operations Certificate (RPAS > 25 kg) to land at a minimal battery level of ≥30%, the system was able to cover an area of ~2.25 ha at a speed of 3.7 m/s and an altitude of 100 m above ground level (AGL) in 7 min. The results with the HSI payload at different speeds and altitudes from 50 m to 100 m AGL show hyperspectral imagery with minimal roll–pitch–yaw artefacts prior to geocorrection and consistent spectra when compared to nominal reflectance targets. Finally, we discuss the steps followed to deal with the continuously evolving regulatory framework developed by Transport Canada for systems > 25 kg. Our work advances low-altitude HSI applications and encourages remote sensing scientists to take advantage of national regulatory frameworks, which ultimately improve the overall quality of HSI data and safety of operations with RPAS > 25 kg.
一种用于高光谱载荷超过25公斤的遥控飞机系统的新实现方法的开发
限制超过25公斤的低空遥控飞机系统(RPAS)运行的一个主要方面是,集成了推力扫帚高光谱传感器,来自与飞机性能(例如飞行时间)和监管方面的挑战,阻碍了用户超越这一重量限制。在这项研究中,我们展示了一种新的实现,使用大疆Agras T30作为集成先进高光谱成像仪(HSI, Hyspex VS-620)的空中系统。我们介绍了用于集成HSI有效载荷的设计和制造方法,为HSI及其万向节提供动力的关键考虑因素,以及振动和风洞测试的结果。我们还评估了系统的飞行能力和HSI的几何和辐射数据质量。整合HSI有效载荷和辅助硬件后,T30的最终重量为43公斤。我们的振动测试表明,隔振器和云台将振动传输降低到15 Hz以上,但也引入了9.6 Hz的共振峰,导致振动在9.6 Hz附近的低频范围内放大(RMS约为0.08 g)。风洞测试表明,该系统在制造商规格额定风速(即8 m/s)的近两倍下保持稳定。根据加拿大特殊飞行操作证书(RPAS >25kg),在最小电池容量≥30%的情况下着陆,系统能够在7分钟内以3.7 m/s的速度和距离地面100 m的高度覆盖约2.25 ha的区域。从50 m到100 m AGL的不同速度和高度下,HSI有效载荷的结果显示,与标称反射率目标相比,高光谱图像具有最小的滚转-俯仰-偏航伪像,并且与地球校正前的光谱一致。最后,我们讨论了应对加拿大运输部为系统制定的不断发展的监管框架所采取的步骤;25公斤。我们的工作推进了低空HSI应用,并鼓励遥感科学家利用国家监管框架,最终提高HSI数据的整体质量和RPAS操作的安全性;25公斤。
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
Drones
Drones Engineering-Aerospace Engineering
CiteScore
5.60
自引率
18.80%
发文量
331
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