A RFI Testbed for Examining GNSS Integrity in the Various Environments

Yu‐Hsuan Chen, Zixi Liu, J. Blanch, Sherman Lo, Todd Walter
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Abstract

A testbed is built for examining the GNSS integrity under RFI for aviation environment. The combination of hardware and software enables us to simulate the RFI and GNSS environment on the aircraft in the laboratory. Considering existing different jamming types and power level effect on the GNSS integrity, several jamming type data sets are pre-generated and jamming power is adjustable by setting the transmitter gain. The receivers collect the raw measurements needed for protection level computation or output built-in protection level. The algorithm to compute the protection level is the multiple hypothesis solution separation algorithm (MHSS). Then, convert the protection level to Navigation Integrity Category (NIC) which is a field in Automatic Dependent Surveillance-Broadcast (ADS-B). Three receivers from surveying to consumer grade are tested for examining different responses of receiver brands.
用于检测各种环境下GNSS完整性的RFI测试平台
建立了航空环境下RFI下GNSS完整性测试平台。硬件和软件的结合使我们能够在实验室中模拟飞机上的RFI和GNSS环境。考虑到现有的不同干扰类型和功率电平对GNSS完整性的影响,预先生成了几种干扰类型数据集,并通过设置发射机增益来调节干扰功率。接收器收集保护级别计算或输出内置保护级别所需的原始测量。计算保护等级的算法是多假设解分离算法(MHSS)。然后,将防护级别转换为ADS-B (Automatic Dependent Surveillance-Broadcast)中的导航完整性类别(Navigation Integrity Category, NIC)字段。从调查级到消费级的三个接收器进行测试,以检验接收器品牌的不同反应。
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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