• Journal of the Korean Society for Aviation and Aeronautics
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• v.26 no.4
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• pp.149-154
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• 2018

Risk Based Oversight is a way of performing oversight, where planning is driven by the combination of risk profile and safety performance. Risk Based Oversight enables prioritization and allocation of State's safety management resources commensurate with the safety risk profile of each service provider. This paper presents the concept of Risk Based Oversight and applies it to the current Korean aviation safety oversight process. In particular, this study presents a method for generating operating profiles, one of the key concepts of Risk Based Oversight. Operations Specifications of Part 121 Airlines can generate operating profiles. In this study, a practical study was conducted to generate the operating profile and scoped DCTs using Part 121 Airlines's Operations Specifications.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2011.06a
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• pp.164-166
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• 2011

기존 연구에서 다중선박의 충돌위험도를 추정하는 알고리즘을 개발한 바 있다. 본 연구에서는 이를 기반으로, 실제 선박에 온보드형으로 설치하여, 운용할 수 있도록 전자해도 기반의 충돌위험도 표시 시스템을 설계하고, 그 표시 프로그램을 구현하였다. 국립해양조사원에서 배포하는 전자해도(IHO S-57) 파일을 이용할 수 있으며, 실시간으로 입력되는 해상교통 정보를 받아 충돌위험도를 계산하여, 표시할 수 있도록 구성하였다. 그리고, 개발된 프로그램의 성능을 검증하기 위하여, 선박운항 시뮬레이터를 이용하여, 실제 선박충돌사고의 AIS 데이터를 이용한 재생시뮬레이션을 수행하였다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2014.06a
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• pp.232-234
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• 2014

현재 연안여객선의 여객과 화물의 승선 예매 및 발권시스템은 타 교통수단에 비교하여 매우 부족하며 여객이 느끼는 실질적인 서비스 수준도 상대적으로 미흡하다는 평가를 받고 있다. 해양수산부 등 관련 기관에서는 이를 개선하기 위해 승선권 무인취급시스템 등을 구축하고자 노력하고 있으나 아직 부족한 현실이다. 본 연구에서는 여객 및 화물 정보를 QR-Code 등을 통하여 인식한 후, 선박 자체관리 프로그램 및 Web상에서 연동되는 선박예매/발권시스템을 구축하였다. 시스템의 Database 정보에는 승선객의 프로파일 정보, 중간기착지 방문 정보, 여객의 최초승선지 및 하선 정보, 화물 적양하 기록 등이 포함된다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2012.10a
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• pp.178-182
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• 2012

PEAT(Procedure/airspace Efficiency Assessment Tool) evaluates the efficiency of the flight procedures designed by Procedure and Airspace Design Program, such as fuel consumption fight time, flyability, noise footprint and etc. For noise footprint analysis among the efficiency metrics, the input generation module for INM(Integrated Noise Model) was designed in this research. The INM input files shall contain the information about aircraft types, noise model, airport and runway configuration, number of flights, flight routes, and also should be satisfied with the exact file formats for input data, since INM is not originally executable with file inputs. Therefore, it has been designed to convert the input data given in XML file to DBF. In this paper, the design result of the module which has functionalities to generate appropriate input file for INM, and to convert and save the analysis results from INM, is presented.

• Special Issue of the Society of Naval Architects of Korea
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• 2017.10a
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• pp.59-62
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• 2017

Recently oil price has got lower, but energy efficiency has been considered as an important factor to minimize ship operational costs and reduce greenhouse gas emissions. For the reason, it is necessary that energy efficiency improvement for hull form design and operational performance reflect an understanding of the vessel's operational profile. Throughout the life of the vessel, this can lead to important economies of fuel, even if, in some cases, a small penalty can be taken for design condition. In the present paper, hull form was developed for 5,000TEU class container carrier at given operation profile. As a CFD result at several design point, optimized hull form has improved resistance performance in comparison with the basis hull form. To reducing the viscosity and the wave resistance at multi draft and multi speed, the hull form was investigated for Cp-curve, frame and local shape. Numerical study has been performed using WAVIS & Star-CCM+ and verified by model test in the towing tank.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.15 no.11
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• pp.2333-2339
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• 2011

In the field of maritime transport, various researches on next generation of standards are underway to realize e-navigation. While IHO leading the way, many studies on several S-100 based standards for exchange, sharing and utilizing maritime geographical information and related data are going on. IHO S-100 as a profile of ISO 19100 series of standards. Based on their application and service they provide, there can be different S-10x standards. In order to support the safe operation, various information should be integrated. When integrating a various information, it is crucial to make sure the same data model should be treated consistently and interpreted clearly across different profiles, such as S-101, S-102, etc. in this case. In this paper, I suggested a way to covert maritime metadata of S-100 to ontology so that we can perform consistent semantic analysis and processing of data in S-100 standards, which is the basis of other S-10x standards.

• The Sea:JOURNAL OF THE KOREAN SOCIETY OF OCEANOGRAPHY
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• v.17 no.2
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• pp.130-137
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• 2012

The underwater glider using conception of Lagrangian method, is a new observation platform to understand the properties of the ocean vertically. In 2011 March, KORDI made a first successful autonomous trip from Hupo to west coast of Uleungdo piloting Littoral Glider of Alaska Native Technology LLC. The journey considered many environmental variables and route vigilantly selected, the glider covered 177 km horizontally and took approximately 6 days (153 hours). Despite the existence of 1 kt eddy current, Sound velocity sampling was conducted from 5 meters and reaching maximum of 200 meters depth at each dive. It successfully collected sound velocity and temperature profile at every 5 seconds totaling up to 1408 profiles using SVT&P sensor. During the flight it was also a mission to check the diverse modes of the glider i.e. spiral, waypoints, heading, drift and hover could function without a defect in a given situation. These modes were thoroughly monitored and it could be considered that the glider handled it well during the flight. As a result of this test flight, it was evident that the given underwater glider could operate under 2kt current environment with users defined heading and depth, also with the payload up to 5 kg without changing internal buoyancy.