• 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.

• 한국항공운항학회:학술대회논문집
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• 한국항공운항학회 2004년도 추계학술발표대회 논문집
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• pp.295-301
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• 2004

• 한국항행학회논문지
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• 제23권3호
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• pp.245-250
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• 2019

관성항법장치는 시간 경과에 따라 관성센서 및 초기정렬 오차로 인해 항법 오차가 발생한다. 이를 보상하기 위한 방법으로 위성항법시스템 및 속도계 등을 이용하여 보정항법을 수행한다. 수중 환경에서는 GNSS 신호가 통하지 않기 때문에, 수중운동체에 탑재한 관성항법장치는 주로 속도계 보조센서를 이용하여 보정항법을 수행한다. 속도계 보조센서는 DVL, EM-Log, RPM이 있으며, 시스템 환경에 따라서 센서 종류가 적용된다. 본 논문은 고속 및 심해 환경에서 운용되는 관성항법장치의 RPM 속도보정항법을 설계하였다. 또한 직진 방향의 성분을 갖는 RPM 속도계의 한계를 보완하며, 해조류 속도 오차를 보상하는 알고리즘을 제안하였다. 제안한 알고리즘은 몬테카를로 시뮬레이션 결과를 통해 성능을 입증하였다.

• 산업공학
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• 제13권1호
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• pp.65-77
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• 2000

Nowadays, the modeling of systems have been enabled by various models and methodologies that are used for different purpose and perspectives upon the systems. The integrated modeling methodology that integrates these models and methodologies has become challenging issues in system integration such as CIM and PDM. The primary objective of this paper is to propose the comprehensive integrated modeling methodology that integrates the Extended IDEF0 function model, OOIDEF0 information model, navigation model, interface model, and organization model for an effective analysis and design of the CIMS for ship production. This methodology can be used for the integrated system, and cover the systems development life cycle in an integrated fashion. In order to prove the consistency and efficiency of the proposed methodology, the CIMS for ship production is modeled.

• Journal of Electrical Engineering and Technology
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• 제7권4호
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• pp.615-625
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• 2012

GPS attitude outputs or carrier phase observables can be effectively utilized to compensate the attitude error of the strapdown inertial navigation system. However, when the integer ambiguity is not correctly resolved and/or a cycle slip occurs, an erroneous GPS output can be obtained. If the erroneous GPS output is applied to the attitude determination GPS/INS (ADGPS/INS) integrated navigation system, the performance of the system can be degraded. This paper proposes an ADGPS/INS integration system using the triple difference carrier phase observables. The proposed integration system contains a cycle slip detection algorithm, in which the inertial information is combined. Computer simulations and flight test were performed to verify effectiveness of the proposed navigation system. Results show that the proposed system gives an accurate and reliable navigation solution even when the integer ambiguity is not correctly resolved and the cycle slip occurs.

• 한국데이타베이스학회:학술대회논문집
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• 한국데이타베이스학회 1999년도 춘계공동학술대회: 지식경영과 지식공학
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• pp.155-159
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• 1999

자율무인잠수정(AUV, Autonomous Underwater Vehicle)이 해저 속에서 주어진 임무(mission)를 수행하는데 있어 가장 먼저 선행되어야 하는 것은 목표점(Goal Position)까지 안전하고 빠르게 항행할 수 있는 자율 항행시스템(Autonomous Navigation System) 관련 기술의 개발이다. 이러한 시스템은 IPMS(Integrated Platform Management System)률 기반으로 하여 자율무인잠수정에 자율성을 부여하는 항행전문가시스템(Navigation Expert System)이 결합된 구조이다. 본 논문에서는 IPMS에 기반 한 자율항행시스템의 개념적 구조를 설계하고 항행전문가시스템의 추론방법으로서 퍼지관계곱(Fuzzy Relational Products) 기반 평가함수를 이용한 항행 휴리스틱탐색(navigation heuristic search) 기법을 제안한다.

• 한국지능정보시스템학회:학술대회논문집
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• 한국지능정보시스템학회 1999년도 춘계공동학술대회-지식경영과 지식공학
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• pp.155-159
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• 1999

자율무인잠수정(AUV, Autonomous Underwater Vehicle)이 해저 속에서 주어진 임무(mission)를 수행하는데 있어 가장 먼저 선행되어야 하는 것은 목표점(Goal Position)까지 안전하고 빠르게 항행할 수 있는 자율항행시스템(Autonomous Navigation System) 관련 기술의 개발이다. 이러한 시스템은 IPMS(Integrated Platform Management System)를 기반으로 하여 자율무인잠수정에 자율성을 부여하는 항행전문가시스템(Navigation Expert System)이 결합된 구조이다. 본 논문에서는 IPMS 에 기반한 자율항행시스템의 개념적 구조를 설계하고 항행전문가시스템의 추론방법으로 퍼지관계곱(Fuzzy Relational Products) 기반 평가함수를 이용한 항행 휴리스틱탐색(navigation heuristic search) 기법을 제안한다.

• International Journal of Fuzzy Logic and Intelligent Systems
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• 제2권1호
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• pp.1-8
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• 2002

It has been integrated into several navigation systems. This paper shows that system recognizes difficult indoor roads without any specific marks such as painted guide line or tape. In this method the robot navigates with visual sensors, which uses visual information to navigate itself along the read. The Neural Network System was used to learn driving pattern and decide where to move. In this paper, I will present a vision-based process for AMR(Autonomous Mobile Robot) that is able to navigate on the indoor read with simple computation. We used a single USB-type web camera to construct smaller and cheaper navigation system instead of expensive CCD camera.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.114.3-114
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• 2001

The pure navigation system using Inertial Navigation Unit(INU) which has very accurate short term stabilities but not long term gives rise to position errors propotional to time. On the contrary, Global Positioning System(GPS) which is bounded its errors to some fixed ranges shows higher accuracy in the long term, and lower accuracy in the short term than that of INS. Recently the integration of these two systems is one of the main topic in the field of navigation system. In this thesis, the implementation of kalman filter on the real time navigation computer and step jump error compensation method is suggested.

• Journal of Positioning, Navigation, and Timing
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• 제7권1호
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• pp.15-24
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• 2018

This study analyzed positioning accuracy of the multi-differential global navigation satellite system (DGNSS) algorithm that integrated GPS, GLONASS, and BDS. Prior to the analysis, four sites of which satellite observation environment was different were selected, and satellite observation environments for each site were analyzed. The analysis results of the algorithm performance at each of the survey points showed that high positioning performance was obtained by using DGPS only without integration of satellite navigation systems in the open sky environment but the positioning performance of multi-DGNSS became higher as the satellite observation environments degraded. The comparison results of improved positioning performance of the multi-DGNSS at the poor reception environment compared to differential global positioning system (DGPS) positioning results showed that horizontal accuracy was improved by 78% and vertical accuracy was improved by 65% approximately.