• 한국군사과학기술학회지
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• 제18권5호
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• pp.602-611
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• 2015

Even though GNSS provides highly accurate navigation information all over the world, it is vulnerable to jamming in the electronic warfare due to its weak signal power. The United States and Korea have plans to use terrestrial navigation systems as back-up systems during outage of GNSS. In order to develop back-up systems of GNSS, an M&S software platform is necessary for performance evaluation of various vehicle trajectories and integrated navigation systems. In this paper a design method of an M&S software is proposed for evaluation of multiple radio positioning integration systems. The proposed M&S software consists of a navigation environment generation part, a navigation algorithm part, a GUI part and a coverage analysis part. Effectiveness of the proposed design method is shown by implementing an M&S software for the GPS, DME and eLoran navigation systems.

• 한국항행학회논문지
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• 제28권2호
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• pp.210-215
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• 2024

선박의 자동화 수준이 높아지고 자율운항선박의 개발에 따라 선박의 IPMS (integrated platform management system)는 다양한 운영체제로 통제되는 개별 장비들을 통합하고 다량의 데이터를 실시간으로 처리해야 한다. 이러한 상황에서 데이터 처리를 위해 DDS (data distribution service) 미들웨어 기반 선박 IPMS 시뮬레이터를 개발하고 성능을 평가하였다. 이종 운영체제로 동작하고 있는 신호입출력장치와 IPMS 서버에서 초당 1,000개의 토픽을 비동기로 발간하고 구독한 시뮬레이션을 수행하였으며, 초기 4초 동안 일부 토픽의 누락을 제외하고는 오류 없이 데이터를 수신하였다. 개발된 시뮬레이터는 실제 선박에서 DDS를 이용하여 다른 제어체계를 통합할 수 있음을 보여준다.

• 대한조선학회논문집
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• 제60권4호
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• pp.256-265
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• 2023

This paper describes the results of the development of the submarine Free Running Model (FRM). First, the goal of development was set based on the test conditions and the test environment, and the system was obtained accordingly. The target submarine, Joubert BB2 submarine, was selected with a scale of 18.35 in accordance with the development goal. In order to conduct a submarine FRM test underwater, where communication is impossible, the FRM must operate at least semi-autonomously. For this purpose, an Extended Kalman Filter (EKF) based underwater integrated navigation system and control system using a sailplane and an X-shaped sternplane were designed respectively. In addition, a ballast system was designed to enable the model to float to the water surface in case of an emergency. To verify its propulsion, navigation, and control performance, the FRM tests were conducted in both indoor and outdoor basins. As a result, the relationship between propeller RPM and vehicle speed was derived, and it was confirmed that the navigation and control performance met the target value.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2010년도 춘계학술대회
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• pp.699-701
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• 2010

해상 감시용 Multi Sensor 및 IFOG 개발을 위하여 주 야간 겸용 감시카메라의 통합 개발과 시스템 Control Unit 설계 및 항해 장비 연동 시스템 제작하였다. 선박 통합 시스템의 Control Unit의 분석은 Control Unit에 연결 가능한 항해 장비 리스트를 선별하는 것으로 시작 하였다. 항해 장비 리스트를 선별한 후 각 항해 장비의 용도와 특성, 연결 방법, 통신 방법, 데이터 종류에 따라 Control Unit와 항해 장비간의 데이터 방향성, 데이터 종류들을 선별하여 그 성능을 보여주었다.

• 한국항공운항학회지
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• 제31권1호
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• pp.11-17
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• 2023

In this study, the correlation analysis between total system error and environmental factor variables was performed to confirm the effect on the performance of the integrated navigation system by various environmental factors. To collect flight data of hybrid vertical take-off and landing UAVs, scenarios including various turning sections and straight sections such as left turn, right turn, turning rate, and path change angle were selected, and environmental data of wind direction, wind speed, temperature, air pressure, and humidity were collected in real time through weather station. As a result of the correlation analysis between the collected flight data and environmental data, it was concluded that the performance of the integrated navigation system by environmental factors within the collected data was not significant affected and was robust.

• 한국군사과학기술학회지
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• 제12권5호
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• pp.636-643
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• 2009

NHC means that the velocity of the vehicle in the plane perpendicular to the forward direction is almost zero. The main error source of NHC is the mounting misalignment which is the difference between the body frame of a land vehicle and the sensor frame of an inertial measurement unit. This paper suggests new NHC algorithm that can reduce position errors by real-time estimation of mounting misalignment. Then NHC/ZUPT integrated land navigation system is designed and its performances are analyzed by simulations with van test data. Simulation results show that the proposed NHC/ZUPT land navigation system improves navigation accuracy regardless of misalignment angle and is very useful when SDINS operates stand-alone for land vehicle navigation with large mounting misalignment.

• 한국항해항만학회지
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• 제48권2호
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• pp.125-136
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• 2024

This research presents an innovative integrated ethanol solid oxide fuel cell (SOFC) system designed for applications in marine vessels. The system incorporates an exhaust gas heat recovery mechanism. The high-temperature exhaust gas produced by the SOFC is efficiently recovered through a sequential process involving a gas turbine (GT), a regenerative system, steam Rankine cycles, and a waste heat boiler (WHB). A comprehensive thermodynamic analysis of this integrated SOFC-GT-SRC-WHB system was performed. A simulation of this proposed system was conducted using Aspen Hysys V12.1, and a genetic algorithm was employed to optimize the system parameters. Thermodynamic equations based on the first and second laws of thermodynamics were utilized to assess the system's performance. Additionally, the exergy destruction within the crucial system components was examined. The system is projected to achieve an energy efficiency of 58.44% and an exergy efficiency of 29.43%. Notably, the integrated high-temperature exhaust gas recovery systems contribute significantly, generating 1129.1 kW, which accounts for 22.9% of the total power generated. Furthermore, the waste heat boiler was designed to produce 900.8 kg/h of superheated vapor at 170 ℃ and 405 kP a, serving various onboard ship purposes, such as heating fuel oil and accommodations for seafarers and equipment.

• 한국항행학회논문지
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• 제13권5호
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• pp.630-638
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• 2009

본 논문에서는 SCADE를 사용하여 항공기 안전필수 시스템인 공중충돌회피시스템(TCAS-II)을 위한 통합 시뮬레이터를 설계한다. 이 TCAS-II시뮬레이터는 기존의 충돌회피 알고리즘의 문제점을 분석하고 실제 공중충돌 상황을 더욱 현실성 있게 시스템 평가에 반영할 수 있도록 편리한 통합시뮬레이션 환경을 반영하여 구현한다. 또한 안전 필수요건인 소프트웨어 국제표준 신뢰성 요건을 만족하면서 실제로 실험할 수 없는 상황에 대한 TCAS-II의 성능분석 및 새로운 충돌회피 로직 연구를 위한 시나리오 편집기를 제시하고 이를 사용하여 전형적인 공중충돌 시나리오에 대한 시뮬레이션을 통해 그 성능을 검증한다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2018년도 추계학술대회
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• pp.95-96
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• 2018

본 논문에서는 위성항법시스템의 백업 PNT 시스템으로 각광받고 있는 eLoran 시스템의 기술개발 현황과 그 성능 커버리지 예측 분석에 대해 중점적으로 다룬다. eLoran 서비스 시범운영을 위한 테스트베드 구축현황과 eLoran 송신국 시스템, 보정기준국 시스템, 통합운영 제어시스템, 그리고 사용자를 위한 eLoran/GNSS 통합수신기의 개발현황에 대해 설명한다. eLoran 테스트베드 구축을 통한 시범운영을 위해서, 시험송신국 구축을 위한 계획 및 지상파 기반의 백업 PNT 서비스를 향한 향후 계획에 대해 논의한다.

• Journal of Positioning, Navigation, and Timing
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• 제13권1호
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• pp.53-61
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• 2024

Global Navigation Satellite Systems are expected to meet system-defined integrity requirements when users utilize the system for safety critical applications. While the guaranteed integrity performance of GPS and Galileo is publicly available, their integrity assurance procedure and related methodology have not been released to the public in an official document format. This paper summarizes the integrity assurance procedures of Global Positioning System (GPS) and Galileo, which were utilized during their system development, through a literature survey of their integrity assurance methodology. GPS Block II assures system integrity using the following methods: continuous performance monitoring and maintenance on Space Segment (SS) and Control Segment (CS), through a cause and effect analysis of anomalies and a failure analysis. In GPS Block III, to achieve more stringent integrity performance, safety requirements are integrated into the system design and development from its starting phase to the final phase. Galileo's integrity performance is provided in the Integrity Support Message (ISM) format, as Galileo utilizes a Dual Frequency Multi Constellation (DFMC) Satellite Based Augmentation System (SBAS) and Advanced Receiver Autonomous Integrity Monitoring (ARAIM) to serve safety critical applications. The integrity performance of Galileo is ensured by using a methodology similar to GPS Block II (i.e. continuous performance monitoring and maintenance on the system). The integrity assurance procedures reviewed in this paper can be utilized for a new satellite navigation system that will be developed in the near future.