• Title/Summary/Keyword: RTCM 2.3

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Architecture Design for GNSS Correction Message Generating Module based on RTCM version 2.4 (RTCM 2.4 기반 GNSS 보정정보 메시지 생성 모듈의 아키텍처 설계)

  • Jang, Wonseok;Kim, Youngki;Seo, Kiyeol
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.19 no.10
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    • pp.2285-2291
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    • 2015
  • At present, available positioning satellites are not only the GPS, but also GLONASS, GALILEO, QZSS, BeiDou. However, the differential GPS, the augmentation service for increase the positioning accuracy, is follow the RTCM version 2.3 standard. So, it can service the correction information about only GPS. For solve this problem, RTCM is making the new version of RTCM message standard that can service the correction information for all of available GNSS. In South Korea, the software DGNSS RSIM system was installed at almost the whole DGNSS reference station. In this reason, that can cope with the new RTCM version 2.4 quickly. However, the DGNSS Reference Station based RSIM 1.3 can not make the GNSS's PRC simultaneously and can not support RTCM version 2.4. Thus, in this paper, the version of RTCM 2.4 is analyzed and the RTCM version 2.4 message generating module's architecture for software DGNSS reference station is designed.

Architecture Design for RSIM version 1.3 based Software RS and IM (RSIM 버전 1.3 기반의 소프트웨어 RS, IM 아키텍처 설계)

  • Jang, Wonseok;Kim, Youngki;Seo, Kiyeol
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.18 no.9
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    • pp.2124-2130
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    • 2014
  • The standard for DGPS reference station system defined by RTCM is in the current version of 1.2. This standard currently supports only GPS of the United States. However, the current operating GNSS satellite consisted of not only GPS, but also GALILEO of Europe, GLONASS of Russia, QZSS of Japan, BeiDou of China and so on. Therefore, the existing standard is not able to support them. Accordingly, a new standard in the version of RTCM's RSIM 1.3 is established in order to provide correctional services to GNSS satellites. In this paper, the version of RSIM 1.3 is analyzed and the software for DGNSS reference station architecture supporting the version of RSIM 1.3 is designed.

Analysis of RSIM version 1.3 for development of software DGNSS RSIM (소프트웨어 DGNSS RSIM 개발을 위한 RSIM 버전 1.3의 분석)

  • Jang, Wonseok;Kim, Youngki;Seo, Kiyeol
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2014.05a
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    • pp.303-305
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    • 2014
  • 현재 한국에서 설치, 운영되고 있는 DGPS 기준국은 RTCM의 DGPS 기준국 관련 표준인 RSIM 버전 1.2를 기반으로 제작되어져 있다. RSIM 버전 1.2는 GPS의 보정정보를 생성하는 기준국을 위해 제정된 표준으로 현재의 다양한 GNSS들에 대한 보정정보를 서비스하는 것은 불가능하다. 이에 RTCM에서는 GPS외에 다양한 GNSS들을 지원할 수 있도록 새로운 기준국 표준 버전인 RSIM 버전 1.3을 제정하고 있다. 이러한 시점에서, 한국의 DGPS 기준국이 DGNSS 기준국으로 발전하여 각 GNSS의 보정정보를 서비스하기 위해 필수적인 신규 버전 기반 소프트웨어 RSIM 시스템을 개발하기 위해 본 논문에서는 RSIM 버전 1.3의 특징을 분석하고 소프트웨어 RSIM에서 구현되어야 하는 필수 기능들을 도출하였다.

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Assessment of Position Degradation Due to Intermittent Broadcast of RTK MSM Correction Under Various Conditions

  • Yoon, Hyo Jung;Lim, Cheol soon;Park, Byungwoon
    • Journal of Positioning, Navigation, and Timing
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    • v.9 no.3
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    • pp.237-248
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    • 2020
  • GNSS has been evolving dramatically in recent years. There are currently 6 GNSS (4 GNSS, AND 2 RNSS) constellations, which are GPS (USA), GLONASS (Russia), BeiDou (China), Galileo (EU), QZSS (Japan), and IRNSS (India). The Number of navigation satellites is expected to be over 150 by 2020. As the number of both constellations and satellites used for the improvement of positioning performance, high accuracy, and robustness of precise positioning is more promising. However, a large amount of the correction messages is required to support the augmentation system for the available satellites of all the constellations. Since bandwidth for the correction messages is generally limited, sending or scheduling the correction messages might be a critical issue in the near future. In this study, we analyze the relationship between the size of the bandwidth and Real-Time Kinematics (RTK) performance. Multiple Signal Messages (MSM), the only Radio Technical Commission for Maritimes (RTCM) message that supports multi-constellation GNSS, has been used for this assessment. Instead of the conventional method that broadcasts all the messages at the same time, we assign the MSM broadcasting interval for each constellation in 5 seconds. An open sky static and dynamic test for this study was conducted on the roof of Sejong University. Our results show that the RTK fixed position accuracy is not affected by the 5-second interval corrections, but the ambiguity fixing rate is degraded for poor DOP cases when RTK correction are transmitted intermittently.

DGNSS 서비스 도입에 관한 연구

  • Gwon, Min-U;Kim, Yeong-Jae;Lee, Byeong-Gon
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2014.10a
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    • pp.286-288
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    • 2014
  • 위성항법중앙사무소에서는 GNSS 체제에 대비하여 위성항법보정시스템 고도화 기반마련을 위해 DGNSS 시범 서비스를 운영 중에 있다. RTCM2.4와 RSIM1.3 발효 시 신속한 DGNSS 전국망 서비스를 위한 위성항법중앙사무소의 현 실태와 준비사항들을 검토하였다.

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Design and Evaluation of a GNSS Receiver Network For Lane-By-Lane Traffic Monitoring (차선별 교통 모니터링을 위한 위성항법 수신기망 설계 및 성능 평가)

  • Kim, Hee-Sung;Lee, Hyung-Keun
    • Journal of Advanced Navigation Technology
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    • v.14 no.2
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    • pp.151-160
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    • 2010
  • For the realization of future intelligent transportation systems, fine-grained lane-by-lane traffic monitoring and control functionalities are among the most important technology barriers to overcome. To satisfy the accuracy requirement for traffic monitoring, a GNSS receiver network is designed. The designed receiver network consists of three different types of entities; reference server, broadcaster, and client. For deployment flexibility, all the entities utilize the international message standard RTCM SC-104 version 3.0. For fine-grained traffic monitoring, the client is designed to utilize position-domain carrier-smoothed-code filters to provide accurate vehicle coordinates in spite of frequent addages and outages of visible satellites. An experiment result is presented to evaluate the positioning accuracy of the proposed method.

Design and Performance Evaluation of DGPS Based on Optimal and Sub-optimal Reference Point (Optimal 및 Sub-optimal 기준점을 사용한 DGPS 설계 및 성능평가)

  • 고광섭;홍성래;정세모
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.2 no.3
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    • pp.343-352
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    • 1998
  • The use of DGPS enhances standalone GPS accuracy and removes common errors from two or more receivers viewing the same satellites. The design of DGPS system contains a precise reference point which is able to compute the common errors to update the pseudo range of users receivers. It should take a great time and cost to provide precise and sufficient accuracy of the reference point. That is, it is natural to measure the parameters from satellites with specific survey instrument system, and then obtain that by post processing. The purpose of the study is to examine the bounds of accuracy which resulted from RTCM correction data transmitted from a simply designed DGPS system. In the paper, We design and evaluate the DGPS system based m the surveyed reference point, and Sub-optimal no by a Standalone GPS as well. As a result of the study, it is shown that the designed system may be applied to the specific marine activity in civilian and military.

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Trend and Analysis of Protection Level Calculation Methods for Centimeter-Level Augmentation System in Maritime

  • Jaeyoung Song;TaeHyeong Jeon;Gimin Kim;Sang Hyun Park;Sul Gee Park
    • Journal of Positioning, Navigation, and Timing
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    • v.12 no.3
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    • pp.281-288
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    • 2023
  • The International Maritime Organization (IMO) states that the recommended horizontal accuracy for coastal and offshore areas is 10 m, the Alert Limit (AL) is 25 m, the time to alert is 10 seconds, and the integrity risk (IR) is 10-5 per three hours. For operations requiring high accuracy, such as tugs and pushers, icebreakers, and automated docking, the IMO dictates that a high level of positioning accuracy of less than one meter and a protection level of 0.25 meters (for automated docking) to 2.5 meters should be achieved. In this paper, we analyze a method of calculating the user-side protection level of the centimeter-level precision Global Navigation Satellite System (GNSS) that is being studied to provide augmentation information for the precision Positioning, Navigation and Timing (PNT) service. In addition, we analyze standardized integrity forms based on RTCM SC-134 to propose an integrity information form and generate a centimeter-level precise PNT service plan.