基于无人机的地面导航与助降信号测量系统

Daniel Sommer, Ashok Sarath Chandra Reddy Irigireddy, Justin Parkhurst, Kevin Pepin, Eduardo-Rojas Nastrucci
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引用次数: 5

摘要

地面导航和着陆辅助站利用来自地面台站的信号帮助飞行员安全导航和降落飞机。这些系统需要定期测试,以确认其性能符合国际民用航空组织(ICA0)的限制。目前,这种测试是通过使用有人驾驶飞机在地面站周围或沿着跑道进行几次飞行来执行的。本文提出了一种基于GPS和编码重叠导航信号的定位信息的无人机系统(UAS)。该系统采用一架轻型六旋翼机,翼展55厘米,可自主飞行,并使用机载软件定义无线电(SDR)测量仪表着陆系统(ILS)和甚高频全向距离(VOR)系统。UAS测试系统的设计使飞行坐标可以预编程,使其适应不同的测试地点。系统数据存储在飞机上,同时遥测信息在飞行过程中发送给飞行员,告知他们系统的状态。一旦无人机完成飞行,将分析ILS、VOR和GPS测量结果,以确定这些制导和着陆辅助系统是否符合国际民航组织的性能要求。利用实时动态GPS (RTK)降低了定位测量误差。盲降系统在佛罗里达州代托纳海滩的DAB机场进行测试,VOR在佛罗里达州奥蒙德海滩的OMN机场进行测试。VOR塔台的方位角测量在292°到328°之间。执行了两次驾驶,并在使用50,000和100,000个样本的两个通道的后处理中应用了两个移动平均线。这导致测量数据与参考GPS之间的平均误差为4.18°,5.34°,2.24°和2.05°。由于测量的限制,测量的调制指数是有限的,在达到0.0和0.4调制指数之前是有界的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
UAV-Based Measuring System for Terrestrial Navigation and Landing Aid Signals
Terrestrial navigation and landing aid stations help a pilot to safely navigate and land an aircraft by using signals originating from ground-based stations. These systems need to be tested periodically toconfirm that their performance is within International Civil Aviation Organization (ICA0) limits. Currently, this test is performed by using a manned aircraft making several passes around the ground stations or along the runways. In this paper, an unmanned aerial system (UAS), called the positional information via GPS and encoded overlayed navigation signals (PIGEONS), is presented. The system employs a light-weight hexacopter, with a wingspan of 55 cm, that performs autonomous flight and uses an onboard software-defined radio (SDR) that measures the instrument landing system (ILS) and VHF omnidirectional range (VOR) systems. The UAS test system is designed so that flight coordinates can be preprogrammed, making it adaptable to different test locations. The system data is stored onboard while telemetry information is sent to the pilot during flight to inform them of the system's status. The ILS, VOR, and GPS measurements are analyzed once the UAS has completed the flight to determine the compliance of these guidance and landing aid systems with the performance requirements from the ICAO. Positioning measurement inaccuracies are reduced by using a Real-Time Kinematic (RTK) GPS. The ILS system was tested at DAB Airport in Daytona Beach, FL and the VOR was tested at OMN Airport in Ormond Beach, FL. The azimuth measurements for the VOR tower were taken between 292° and 328°. Two drive-bys were performed, and two moving averages were applied in post-processing to both passes using 50,000 and 100,000 samples. This resulted in average magnitudes of error between the measured data and reference GPS for the four passes of 4.18°, 5.34°, 2.24°, and 2.05°. Due to measuring limitations, the measured modulation indexes were limited, being bounded before hitting the 0.0 and 0.4 modulation indexes.
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