• Journal of Positioning, Navigation, and Timing
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• v.13 no.1
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• pp.45-52
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• 2024

As part of the Global Positioning System (GPS) modernization program in the United States, Civil Navigation (CNAV) and CNAV-2 messages were developed to introduce flexibility and modern features to the Legacy Navigation (LNAV) message. This paper explores the additional parameters introduced in CNAV/CNAV-2 compared to LNAV, focusing on their roles from the user's perspective. This paper compares the structural and parameter differences among LNAV, CNAV, and CNAV-2. Additionally, we analyze the types and roles of parameters newly incorporated into CNAV/CNAV-2 that were absent in LNAV.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.14 no.10
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• pp.2223-2229
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• 2010

The integrity monitoring of anomalous GPS signal have been researched because of the degradation of GPS satellite performance. It is known that anomalous GPS signal can occur by failure of GPS satellite, sudden increase of ionosphere delay error, SA, wrong modeling for navigation parameters from control segment, and an electromagnetic wave interference, etc. In case of GPS anomaly by satellites can arise from carrier frequency, code and navigation message. In this paper, the scenarios with navigation message errors were made by using GPS simulator, and the influences of GPS navigation message error to receiver were analysed. The anomalies of preamble, bits related TOW count message, subframe ID in HOW, bits related satellite healthy, and the other navigation message errors were described and simulated. Also, the number of satellites, DOP and pseudorange are analyzed to know how the anomalous signal can affect on GPS receiver.

• Journal of Advanced Navigation Technology
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• v.27 no.5
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• pp.510-518
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• 2023

This paper introduces a MATLAB graphical user interface (GUI) based software for performance analysis of navigation message and wide area differential correction of regional navigation satellite system (RNSS). This software was developed to analyze satellite orbit/clock-related performance of navigation message and wide area differential correction simulating RNSS for regions near Korea based on different distributions of monitor and reference stations. As a result of software operation, navigation message and wide area differential correction are given as output in MATLAB file format. From the analysis of output, it was confirmed that valid navigation message and wide area differential correction could be generated from the results about statistical feature of orbit and clock prediction errors, cm-level fitting errors for navigation message parameters, and 81.9% enhancement in range error for wide area differential correction.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.370-371
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• 2013

현재 운영 중인 DGPS RSIM은 다중 GPS/GNSS 수신기를 이용하여 의사거리 기반 보정정보와 그 무결성 기능을 제공하고 있다. 기준국 시스템 기반 무결성 기능 강화를 위하여, 본 논문에서는 기준국 수신기를 기반으로 전파간섭을 검출할 수 있는 간이 기법과 모니터링 시스템에 대해 다룬다. 기준국 시스템에 전파간섭의 영향을 받게 되었을 경우, 전파간섭 검출을 위한 신규 시스템을 추가하지 않고, 기준 운영 시스템, 즉 기준국 수신기의 실시간 원시정보 출력과 RSIM 메시지의 세부 파라미터 정보를 이용하여 전파간섭을 검출할 수 있는 기법 제안과 그 기법을 적용한 전파간섭 모니터링 시스템을 설계하고, 시뮬레이션 결과를 제시한다. 먼저 DGPS 기준국 시스템의 구성과 기능에 대해 설명하고, 무결성 기능의 한계를 제시한다. 또한 전파간섭이 발생했을 경우 기준국 수신기에 미치는 영향에 대해 분석하고, 분석 결과를 기반으로 기준국에 적용할 만한 간이 전파간섭 검출 기법과 이를 기반으로 한 시스템을 설계하여 그 활용 가능성을 제시한다. 성능평가 결과 제안한 기법 및 시스템이 국제해사기구(IMO)에서 요구하는 무결성 성능 중의 하나인 TTA(Time to Alarm) 10초 이내의 성능을 만족할 수 있음을 제시한다.

• Journal of the Korean Institute of Intelligent Systems
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• v.22 no.3
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• pp.328-333
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• 2012

Current differential GPS (DGPS) system consists of reference station (RS), integrity monitor (IM), and control station (CS). The RS computes the pseudorange corrections (PRC) and generates the RTCM messages for broadcasting. The IM receives the corrections from the RS broadcasting and verifies that the information is within tolerance. The CS performs realtime system status monitoring and control of the functional and performance parameters. The primary function of a DGPS integrity monitor is to verify the correction information and transmit feedback messages to the reference station. However, the current algorithms for integrity monitoring have the limitations of integrity monitor functions for satellite outage or anomalies. Therefore, this paper focuses on the detection and identification methods of satellite anomalies for maritime DGPS RSIM. Based on the function analysis of current DGPS RSIM, it first addresses the limitation of integrity monitoring functions for DGPS RSIM, and then proposes the detection and identification method of satellite anomalies. In addition, it simulates an actual GPS clock anomaly case using a GPS simulator to analyze the limitations of the integrity monitoring function. It presents the brief test results using the proposed methods for detection and identification of satellite anomalies.