• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2012.06a
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• pp.455-457
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• 2012

우리나라를 비롯한 전 세계의 최근 물동량 증가로 우리나라 항만에 입출항 척수가 지속적으로 증가하고 있다. 이로 인해 연안 해역뿐만 아니라 원양 해역에서도 선박간의 조우 상황이 다수 발생하고 있으며, 특히 국내 연안 해역은 빈번한 선박 조우로 인한 해양사고 발생이 상당히 빈번하게 발생하고 있는 실정이다. 이에 따라 본 연구에서는 선박 및 해양 관련 업무 종사자들의 인적과실로 인한 해양사고를 예방하고, 해기인력의 질 향상을 위한 기초연구에 그 목적이 있다. 또한 이 연구를 통하여 해기인력의 해양사고예방을 위한 기존 시스템의 하드웨어 및 소프트웨어적인 측면에서 미흡한 부분을 보완하는 자료로 활용하고, 해기인력의 운항능력향상에 중점을 둔 기존 IT기반 시뮬레이터의 문제점과 개선 방안 등을 기초로 향후 해양사고 예방용 통합 시뮬레이션 개발의 주요자료로 활용할 수 있을 것이다.

• Proceedings of the Korea Information Processing Society Conference
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• 2016.10a
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• pp.625-627
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• 2016

최근 드론이 상용화되면서 전문가뿐만 아니라 일반 사람들이 실생활에서 드론을 사용하는 사례가 늘어나고 있다. 하지만 드론을 원하는 대로 안정적으로 조종하기 위해서는 오랫동안 훈련을 해야 한다. 현재 드론을 정확하고 안정적으로 비행할 수 있도록 지원하기 위한 여러 가지 연구들이 활발히 진행되고 있다. 본 논문에서는 드론이 전복되거나 원치 않는 방향으로 이동하는 것을 방지하기 위해 드론의 기울임 정도를 예측하는 방법을 제안한다. 이를 위해서 드론의 센서 값과 프로펠러의 회전속도 값을 인공 신경망을 이용하여 학습시키고, 그 결과 드론이 기울어지는 방향을 예측한다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2015.10a
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• pp.124-126
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• 2015

해양수산부는 2013년 북극해항로 시범운항을 계기로 북극해항로 상용화에 대비한 운항전문인력을 양성하기 위해 한국해양수산연수원에 사업을 위탁하여 극지해역 운항선박에 승선하는 선장과 항해사를 교육대상으로 하는 Ice Navigation 기초 및 직무교육과정을 개발하였다. 이 개발과정 중 전문교원이 극지연구소 소속 쇄빙연구선 아라온호에 승선훈련을 실시하여 북극권 고위도 해역에서의 항해장비와 통신장비 특성 및 운용, 얼음 및 운항정보, 결빙해역 쇄빙 및 선박조종 특성 등을 직접 경험하여 확인한 정보를 공유하고자 한다.

• Proceedings of the Safety Management and Science Conference
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• 2007.04a
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• pp.133-141
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• 2007

Aerial working platform is recently used broadly in heavy industry and construction field and also the utilization of it is growing. However, the raise of critical incident caused by unskilled operator is increasing gradually. To reduce and prevent such incident, the training for operating is essential. It's not easy to cover the requirements for the training with real platform because of the high price of it, safety and weather condition. This paper proposes a simulator for the training based on virtual reality to give the training safely regardless to the weather condition and the simulator is deliverable in lower price than real one. The simulator proposed in this paper is available to be set according to the level of trainee managing the assessment level and be also applied for the design of general heavy equipment training simulator based.

• Journal of the Korea Safety Management & Science
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• v.9 no.4
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• pp.57-62
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• 2007

Aerial working platform is recently used broadly in heavy industry and construction field and also the utilization of it is growing. However, the raise of critical incident caused by unskilled operator is increased gradually. To reduce and prevent such incident, the training for operating is essential. It's not easy to cover the requirements for the training with real platform because of the high price of it, safety and weather condition. This paper proposes a simulator for the training based on virtual reality to give the training safely regardless to the weather condition and the simulator is deliverable in lower price than real one. The simulator proposed in this paper is available to be set according to the level of trainee's skill managing and be also applied for the design of general heavy equipment training simulator.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.31 no.2
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• pp.116-121
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• 2023

항공 사고는 첨단 항공 기술의 발달로 꾸준히 감소해 왔지만, 여전히 발생하고 있다. 조종사는 목적지 공항까지 안전하고 효율적으로 비행하기 위해 위협과 오류를 관리해야 한다. 조종사에게 영향을 미치는 위협은 환경적 위협과 항공사 위협으로 나눌 수 있으며, 환경사위협에는 객실 위협이 포함된다. 조종사와 객실 승무원은 정상적인 운항 중에는 협력이 필요하며, 비상시에는 안전한 비행을 위해 효과적인 협력이 절대적으로 필요하다. 조종사가 비행 중에 간섭이나 작업 흐름의 중단이 발생할 때 에러를 할 가능성이 높아진다. 항공사들은 안전 운항을 방해할 수 있는 객실위협의 종류를 적극적으로 식별하고 분석하여, 조종사들이 안전한 비행을 유지하기 위해서 위협을 관리하도록 절차 및 훈련을 개선해야 한다. 본 연구는 안전관리시스템(SMS)의 안전도구인 LOSA(Line Operation Safety Audit)를 기반으로 기내위협의 유형을 파악하고, 항공사들에게 조종실위협 관리를 체계적으로 개선하는 데 필요한 객실위협과 간섭에 대한 자료를 제공하고자 한다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.24 no.6
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• pp.701-708
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• 2018

Human error is an important cause of maritime accidents and the identification of human error is fundamental to maritime-accident preventions. In particular, the pattern of technical behavior taken in the circumstance of bridge teams(navigator & helmsman) provides important information to identify human error. The purpose of this study is to identify and analyze technical behavior pattern of bridge teams using Williamson's turn for rescue of persons overboard. The focus of this study is to build and analyze a cognitive model of the human behavior factors of the bridge teams in the process of implementing the experiments. The experimental environment was constructed using a ship-handling simulator and conducted an experiment on participants from 24 bridge teams. As a result of the experiment, it was able to identify the behavior pattern of the ship's maneuvering and maintain trajectory using the rudder and engine. This study is expected to correct human error in the bridge teams application to the certification and training of seafarers.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.4
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• pp.25-32
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• 2006

An advanced method of Relaxed Static Stability (RSS) is utilized for improving the aerodynamic performance of modern version supersonic jet fighter aircraft. The flight control system utilize RSS criteria in both longitudinal and lateral-directional axes to achieve performance enhancements and improve stability. The T-50 advanced trainer employs the RSS concept in order to improve the aerodynamic performance and the flight control law in order to guarantee aircraft stability. The longitudinal two modes are the short period with high frequency and the phugoid mode with low frequency. The design goals of longitudinal control laws is concerned with the short period damping and frequency optimization using lower order equivalent system and utilizing the requirement of MIL-F-8785C. Analysis of short period mode has been and continues to be performed This paper addresses the analysis of aircraft phugoid node characteristics such as damping, natural frequency, and analysis of aircraft pitch motion that impacted by angle of attack limiter and auto pitch attitude control law.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.6
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• pp.83-91
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• 2006

An advanced method of Relaxed Static Stability (RSS) is utilized for improving the aerodynamic performance of modern version supersonic jet fighter aircraft. The flight control system utilizes RSS criteria in longitudinal axis to achieve performance enhancements and improve stability. The flight control law of T-50 advanced trainer employs RSS concept in order to improve the aerodynamic performance and guarantee aircraft stability. The longitudinal center of gravity(X-c.g) varies as a function of external stores, fuel state and gear position. Shifts in X-c.g relate directly to longitudinal static margin in aircraft stability. This paper deals the maximum aft X-c.g for critical aircraft loadings and checks static margin limits using sensitivity such as damping, natural frequency, gain and phase margin. And nonlinear analysis was conducted for such as short period input. And also, this paper shows the T-50 aircraft stability based on the result of high angle of attack flight such as upright and inverted departure.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.2
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• pp.106-112
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• 2005

Modern versions of supersonic jet fighter aircraft have several different weapon loading configuration to support air-to-air combat and air-to-ground delivery of weapon modes. These various aircraft loading conditions could result in asymmetric configurations to the aircraft once delivered. These asymmetric configurations could result in decreased handling qualities for the pilot maneuvering, stability, control issues and aerodynamic performance of the aircraft. In order to eliminate or decrease these adverse impacts on the pilot's ability, development of T-50 flight control law attempts to control the aircraft in both longitudinal and lateral-directional axes. Especially, the design of the lateral-directional roll axis control laws, utilizing a simple roll rate feedback structure and gains such as F-16, is developed for the T-50 aircraft to meet the aircraft's design requirements. Consequently, it is found that the improved control law decreases the roll-off phenomenon in lateral axes during pitch maneuver.