• Journal of the Korea Society for Simulation
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• v.22 no.4
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• pp.99-107
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• 2013

In this study, a conceptual study was performed for the leisure boat simulator used for navigation training. The aim of this work was to secure the basic operational capability of a leisure boat as a simulated driving device for a general novice operator. A leisure boat simulator was designed to support a user more efficiently regarding navigation proficiency and safety training, as well as to minimize the limitation of place and time and it conveniently and cheaply. A cockpit for navigation status display and operational input, 3D visualization graphic device, and parallel display device were designed to give the trainee a maximum sense of reality by applying a motion platform with six degree of freedom, in which disturbance movement such waves, winds, and tide were simulated for the operator. Leisure boat simulator training scenario was developed by analysis of water-related leisure activities act and sea traffic safety act.

• Proceedings of the Korean Society of Disaster Information Conference
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• 2023.11a
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• pp.182-184
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• 2023

본 논문에서는 안전한국훈련의 체계적은 포괄적 훈련 프로세스 모델을 개발하기 위해 국제표준인 ISO 22398과 미국의 국토안보훈련(Homeland Security Exercise and Evaluation Program, HSEEP)의 훈련 모델에 기반해 국내 안전훈련을 위한 훈련 모델을 개발하였다. ISO 22398에서는 훈련 프로그램, 훈련 프로젝트, 그리고 지속적 개선을 통한 환류 구조를 제시하고 있었고, 미국의 국토안보훈련에서는 대비 순환과 훈련 순환 구조를 서로 엮는 것으로 포괄적인 훈련 환류 구조를 완성하였다. 한국의 안전훈련이 연속성을 가지기 위해서는 두 훈련 모델을 통합해 지속적으로 환류지속이 가능한 훈련 모델의 개발이 필요해 이를 제시하였다.

• Proceedings of the ESK Conference
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• 1993.10a
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• pp.145-162
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• 1993

조종실은 항공기-조종사 시스템에서 항공기와 조종사간의 긴밀한 상호작용이 이루어지는 유일한 공유영역으로서, 조종사의 인간성능 특성과 조종업무 특성의 체 계적 반영이 요구되어 진다. 인간공학적으로 설계된 조종실은 조종 편이성, 운용성 및 비행 안정성의 향상을 가져올 수 있다. 항공산업 육성의 초기 단계에 있는 국내 에서는 항공기 장비성능 개발 연구가 활발히 진행되고 있으나, 조종실에 대한 인간 공학적 분석 연구는 미흡한 실정이다. 조종사의 인간요소특성에 적합한 조종실 공 간을 체계적으로 설계하기 위하여, -조종실 공간 설계요소의 체계적 추출 및 계층적 구조 설정 -공간 설계에 적용될 인체측정요소의 정의 및 계층적 구조 설정, -설계요 소의 특성 파악을 위한 설계요소간 연관관계 분석, -설계요소와 인간요소간의 연관 관계 분석, -기존 전투기, 훈련기의 설계 제원 현황 및 설계지침 파악, -한국인 인체 측정자료의 Data Base화, -인간공학적인 조종실 공간 설계제원 분석을 수행하였다. 조종실 공간 설계요소로는 143 항목이 정의 되었으며, 설계요소들 간의 연관관계 Matrix 분석을 통하여 선행/병행/후행 설계요소 및 설계요소의 중요도가 파악되었다. 조종실 공간 설계에 적용될 인간 측정요소로는 133개 항목이 정의 되었으며, 설계요소 와 인간요소간의 연관관계 분석을 통하여 설계요소별로 고려되어질 인간요소를 분석 하였다. 또한 설계요소와 관련된 다른 설계요소, 인간요소 및 인체측정치, 설계지침을 종합적으로 적용함으로써 인간공학적인 조종실 공간 설계제원을 제시하였다.

• Journal of the Korean Institute of Navigation
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• v.25 no.4
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• pp.443-453
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• 2001

선박조종시뮬레이터는 해기사의 교육 훈련, 항만 수로 설계 시 안전성 평가, 선박설계시 조종성능의 검토등으로 널리 활용되고 있다. 본 논문은 최근 한국해양대학교에서 개발한 선박조종시뮬레이터를 소개하고 개발 과정과 활용에 대하여 논의한다. 본 시뮬레이터는 Operation Panel, Instructor's Console, Ship Dynamics Calculation, 3D Bridge View, 2D Bird's Eye View 및 Navigational Indicators의 6구성요소로 이루어져 있으며, 이를 위해 8대의 퍼스널 컴퓨터가 배치되어 있다. 모든 구성요소들은 효율적인 정보 교환을 위하여 분산처리네트워크 방식으로 연결되어 있다. 또한, 본 논문은 항만내에서의 저속 시 조종운동 수학모델과 가상현실 모델링에 대해서도 논의한다. 마지막으로, 부산항에 대한 2축2타선박의 접안 조종 시뮬레이션 예를 보여주고 있다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.11
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• pp.1104-1111
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• 2008

The supersonic advanced trainer based on digital flight-by-wire flight control system uses aircraft flight information such as altitude, calibrated airspeed and angle of attack to calculate flight control law, and this information is measured by IMFP(Integrated Multi-Function Probe) equipment. The information has triplex structure using three IMFP sensors. Final value of informations is selected by mid-value selection logic to have more flight data reliability. As the result of supersonic flight test, pitch oscillation is occurred due to IMFP noise when altitude hold autopilot mode is engaged. This tendency may affect stability and handling quality of an aircraft during autopilot mode. This paper addresses autopilot control law design to remove pitch oscillation and these control laws are verified by non-real time simulation and flight test. Also, pitch response characteristics of pitch attitude hold autopilot mode is improved by upgrading the control law structure and feedback gain tuning during bank turn.

• Journal of Advanced Navigation Technology
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• v.27 no.4
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• pp.330-336
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• 2023

Rapid urbanization is rapidly progressing around the world, and urban problems such as traffic congestion, environmental pollution, and noise pollution are emerging, due to this urban concentration phenomenon, logistics and transportation costs are increasing. Urban Air Mobility(UAM) is a three-dimensional futuristic urban transportation that is expected to become an important transportation axis of smart cities as a service(MaaS) linked to roads, railways, and personal transportation. However, as of July 2023, research on airspace systems, Bertieport design, navigation, and communication for UAM operation is actively being conducted, but little research has been conducted on the concept of pilot education and training and education and training programs. Therefore, this paper aims to present a suitable plan for the domestic pilot training system through SWOT analysis of vertical takeoff and landing(VTOL) pilot education and training programs in the United States and Europe.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.22 no.4
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• pp.160-166
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• 2021

In this study, we aim to develop a scenario for educational utilization of disaster response robots that can be used at fire sites and analyze the effectiveness of scenarios according to robot utilization education. Our scenarios were developed based on direction, reality, and rationality determined through the use of a questionnaire survey distributed to current firefighters. In addition, the educational utilization of disaster response robots and training effectiveness were analyzed through repetitive robot control training by a robot development team, current firefighters, and college students. Robot control was divided into direct control, monitor control, and simulation control, and tests were carried out five times. As a result of the analysis of the robot control test, the average time spent for each group was 28 seconds for college students, followed by development teams (30second) and incumbent firefighters (38second). According to the individual analysis results, firefighters (maximum 35second) in direct control, the development team (maximum 14second) in monitor control, and firefighters (maximum 22second) in simulation control showed the effect of shortening control time. These results show that robot control education and training is necessary for robots to be used more effectively at disaster sites.

• Journal of the Korean Society of Marine Environment & Safety
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• v.7 no.3
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• pp.1-16
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• 2001

In view of the fact that marine casualties have more often occurred recently, there is a need for ship-handling simulator as a useful tool for maritime training, safety assessment and so on. Moreover various kinds of hull forms have appeared for the purpose of improving ship manoeuvrality. Therefore ship-handling simulator is in need of a database for various ships, and it can make diverse maneuvering simulations possible to apply respective mathematical model to ship-handling simulator. In this paper, we adopted twin-screw and twin-rudder ship and discussed mathematical model of maneuvering motions for her. It was discussed from the viewpoint of hull damping forces at low advance speed and interaction between hull, propeller and rudder. Using this model, maneuvering motion of twin-screw and twin-propeller ship was simulated numerically and her principal manoeuvrability was examined.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.11
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• pp.70-75
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• 2006

The cabin pressurization system response should be consistent with the design limits such as the cabin pressure schedule, the pressure regulation tolerance, the maximum rate of pressure change during normal and abnormal operation and the maximum cabin air inflow rate change. In this paper, the results of pressure loss analysis and flight test for cabin pressurization system of T-50 advanced trainer are introduced. The pressure tolerance at unpressurized condition using calculated exit area of pressurization components through pressure loss analysis is predicted. Pressurization components of D company are selected and the predicted pressure tolerance is in good agreement with flight test results. Finally, T-50 pressurization system is verified by some flight tests of T-50 advanced trainer to comply with various pressurization design criteria of MIL-E-18927.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.2
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• pp.115-121
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• 2002

This report summarized the static test of the rudder system for the KTX-1 basic trainer. The test loads are applied up to the limit and ultimate loads in a stepping sequence. Test loads and test results matt the strength and stiffness requirements of the rudder control system.. Using #004 full scale structure test airframe.