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Analysis of P(Y) Code and Carrier Multipath for JPALS Ship and Airborne Receivers

机译:jpals船舶和空机接收器的P(y)代码和运营商多径分析

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The Land-Based Joint Precision Approach and Landing System (JPALS) is a military differential landing system similar in architecture to the civil Local Area Augmentation System (LAAS) [1]. Sea-Based JPALS is a relative kinematics system that utilizes carrier phase based solutions for the required accuracy of landing on an aircraft carrier. Code multipath is expected to be a significant error source for both systems while carrier multipath is of particular concern for the Sea-Based system and its stringent availability and accuracy requirements [2]. To develop validated requirements for the ship reference stations and the airborne platforms, multipath experiments were conducted in a static environment with an F/A-18 air frame, and also onboard an aircraft carrier. In all experiments, dual-frequency P(Y) code and carrier phase data were collected. This paper describes the experimental methodology and presents results from the tests conducted. The aircraft static tests show multipath errors of up to 1 m in P(Y) code, and are matched well by simulations. Superimposing realistic flight profiles on these results illustrates how multipath errors are randomized by aircraft attitude motions, resulting in a reduction of multipath RMS by up to 30%. Outdoor multipath tests were conducted onboard the aircraft carrier USS Eisenhower with several days of static dock-side testing to characterize the aircraft carrier environment for code and carrier multipath. Experiments were also conducted while the ship was at sea in order to assess the effect of the sea-state on multipath. In addition to code multipath, a double difference phase multipath observable was also computed. Receiver tracking performance and multipath analysis results are presented.
机译:基于陆基联合精密方法和着陆系统(JPALS)是一种类似于架构的军事差动着陆系统,适用于民事局域增强系统(LAAS)[1]。基于Sea的JPALS是一种相对运动学系统,它利用基于运营商相位的解决方案,以便在飞机载体上降落所需的准确度。代码多径预计将为两个系统都是一个重要的错误源,而运营商多径对基于海上的系统特别关注及其严格的可用性和准确性要求[2]。为了开发船舶参考站和空中平台的验证要求,多径实验在具有F / A-18空气框架的静态环境中进行,并且也在船上。在所有实验中,收集了双频P(Y)代码和载波相位数据。本文介绍了实验方法,并提出了所进行测试的结果。飞机静态测试显示P(Y)代码中最多1米的多径误差,并通过模拟匹配。这些结果上的叠加现实的飞行概况说明了飞机姿态运动如何随机化,导致多径RMS减少高达30%。户外多路径测试是在飞机运输机USS Eisenhower中进行的静态码头侧测试,以表征代码和载波多径的飞机运营商环境。在船舶在海上进行实验,以评估海州对多径的影响。除了代码多径外,还计算了双差阶段多径观察到。提出了接收器跟踪性能和多径分析结果。

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