• 한국안전학회지
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• 제31권6호
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• pp.84-92
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• 2016

Since the mankind started its space mission, the number of artificial space objects has been increasing exponentially. It contains not just the space machines which are in use but the machines which are out of order. Meantime, those dead machines are being a serious danger, a real threat to human's lives and property because of it could re-enter into the earth's atmosphere and fall to the ground causing mega-disaster. As the number of space activities gets growing so far, the re-entry of the space objects will be a lot more happened in the future. Therefore, not just natural space object like asteroids but the artificial space object like artificial satellite and space station can cause the disaster by falling to the ground. To protect our nation and our property, the government has set up the space disaster management center in Korea astronomy and Space science Institute. In this study, we surveyed public's recognition of the space object's re-entry situation and analyzed it to contribute building national space disaster management policy.

• 의료법학
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• 제8권1호
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• pp.215-234
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• 2007

The mission of the doctors is to take care of human life, body and health through the medical behaviors such as diagnosis and treatment. Under this job propensity, the doctors have care duty to take the best actions required to prevent the risk according to the patients' specific disease status. Such care duty of the doctor may be evaluated based on the medical behavior level at the medical institution and clinical medical study field. Such medical level should be understood in the normative level, considering the treatment environment, condition and specialty of the behavior, because it means the medical common sense known and acknowledged to the normal doctors. While the criminal suit requires the evidence for no doubt conviction, the civil suit requires more eased different standard. The results between the criminal and civil sentence may be different, because the confirmed former case may lead to long-term imprisonment and even death penalty, while the latter case puts only monetary penalty on the defeated party.

• 한국군사과학기술학회지
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• 제14권3호
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• pp.405-413
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• 2011

Defense Systems Test Center in ADD supports increasingly various missile test requirements such as higher altitude event, multi target operation and low-altitude, high velocity target tracking. In this paper, we have proposed the development of instrumentation radar tracking status simulator based on virtual reality. This simulator can predict the tracking status and risk of failure using several modeling algorithms. It consists of target model, radar model, environment model and several algorithms includes the multipath interference effects. Simulation results show that the predict tracking status and signal are similar to the test results of the live flight test. This simulator predicts and analyze all of the status and critical parameters such as the optimal site location, servo response, optimal flight trajectory, LOS(Line of Sight). This simulator provides the mission plan with a powerful M&S tool to rehearse and analyze instrumentation tracking radar measurement plan for live flight test at DSTC(Defense Systems Test Center).

• 한국항해학회지
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• 제18권2호
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• pp.41-56
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• 1994

This paper was a part of the risk management in planning a channel. It utilized Korea Marine Training & Research Institutes(KMTRI) which Houses a real-time, full-mission shiphandling simulator to examine the safety of the ship's transit in the planned channel of Asan port. 6 competent Captains participated in this study. The vessel modelled was a 60,000-ton ship. The two variables(factors) examined were environ-mental conditions such as flood-and-ebb current condition and day-and-night condition. The two variables were combined to produce four experimental conditions. To evaluate the safety of the environmental conditions, two categories of performance measures were analyzed. They were vessel's proximity to channel boundary and vessel controalbility. The findings regar-ding the effects of environmental conditions were as follows : - Closest Point of Approach(CPA) to channel boundary was enough for 60,000-ton ship to transit th-rough the channel with 99.999% confidence level. - Closest Point of Approach(CPA) to channel boundary further was under against-current condition than under with-current condition. -Vessel controlability was better under against-current condition than under with-current condition. -Vessel controlability was better under inbound transit than under outbound transit.

• 한국항공운항학회지
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• 제21권3호
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• pp.27-40
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• 2013

Rotorcraft operating in the domestic aviation safety techniques are applied CRM training is conducted but, aircraft accidents caused by human factors has not shown a declining trend. Thus, knowledge of aviation safety and human factors for the spread of awareness of improved rotorcraft flight operations department managers to understand the complexity of nature and culture, and to perform high-risk mission helicopter pilot study of local activation and enhance safety awareness research was conducted in order to. In this study, the development direction of CRM training studies in order to identify the leading NOTECHS (Non-Technical Skills; non-technical pilot skills) of the four categories as the independent variable and the dependent variable corresponding to the resulting effect on the key variables awareness of the differences were studied. In addition, the direction and strength of the relationship were analyzed to determine the relationship of each independent variable to assess the impact on the dependent variable regression analysis was performed. Pilot training and evaluation of non-technical skills related to the teaching reflected in the CRM training and assessment must be carried out with 5 star rating scale was preferred. Therefore, to meet our country rotorcraft operating environment 'NOTECHS' aviation safety by developing training programs reflected in the educational process, implementation, and periodic training and assessment is done in future research on this analysis and feedback is done to reflect the specific performance expect.

• 한국항공우주학회지
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• 제37권11호
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• pp.1104-1111
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• 2009

항공기는 저고도에서 임무를 수행할 때, 대공 미사일과 지형 장애물 같은 다양한 위협들에 제약을 받는다. 특히, 항공기는 지면 근처에서 항상 지형과의 충돌 위험을 갖는다. 본 연구에서는 이 문제에 효과적으로 대비하기 위하여, 지형 회피가 고려된 비행경로 생성 알고리듬을 개발하였다. 비행경로 생성 알고리듬에서는 먼저 등고선의 그룹화를 통해 경로점을 생성하고, Dijkstra 알고리듬을 이용하여 적절한 경로점 조합을 구성한다. 구성된 경로점 조합에 대해서는 최적제어 이론을 기반으로 한 최적 경로점 유도법칙을 적용하여, 제어에너지를 최소로 하는 최적의 비행경로를 제시한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.428-428
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• 2002

The scientific objectives of PACRIM (Pacific Rim) are to advance the understanding of polarimetric and interferometric radar and to promote its application in environmental research designed to detect and quantify changes found in both the physical and humanly dominated ecosystems on the earth's surface. The information derived is used to more readily identify environments at risk; improve environmental decision making and the management of resources and thereby lead to the implementation of more effective and sustainable land use practices. PACRIM is a collaborative research project was organized by NASA's Mission to Planet Earth, Airborne Sciences Program; the Jet Propulsion Laboratory; CSIRO-COSSA and the Centre for Remote Sensing and GIS at the University of New South Wales. A decade of working with AIRSAR data (1993-2003) in the Australia-Asian-Pacific region has provided the opportunity for more than 400 investigators from 20 countries to collect, analyse, interpret and apply state-of-the-art radar data to earth-science studies. This has been achieved by scientists working within seven broad research themes; o Forestry and vegetation o Geology and tectonic processes o Interferometry o Disaster management o Coastal analysis o Agriculture o Urban and regional development. This paper presents an overview of the three data acquisition missions (1993,1996 and 2000) and the science research outcomes achieved from analyzing high quality radar data.

• 항공우주시스템공학회지
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• 제13권5호
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• pp.57-64
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• 2019

항공전자 시스템은 유지비용 감소 및 운용성능 향상을 위하여 기능을 모듈화, 통합화 설계를 적용한 모듈 통합형 항공 전자 시스템으로 개발 되어지고 있으며, 다양한 임무 제어 수행을 위해서 가상화 기술을 적용한 파티셔닝 운용체제를 적용 하고 있다. 가상화 기술을 적용 할 경우 CPU 처리 부하 분배는 중요한 고려 대상이며, 특히 입출력 처리 시간에 대한 불확실성은 안정성 있는 항공전자 시스템 설계에 있어 위험 요소 중 하나이다. 본 논문에서는 유즈케이스를 통해 입/출력 처리 방식에 따르는 CPU 처리 부하량을 비교 분석하여 공간적/시간적 파티셔닝 예시에 적용함으로써 입/출력 처리 방식의 영향성을 검토하고자 한다.

• 한국기계가공학회지
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• 제18권8호
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• pp.31-37
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• 2019

The inter-development of FMECA is very important to assess the effect of potential failures during system operation on mission, safety and performance. Among these, criticality analysis is a core task that identifies items with high risk and selects the analyzed objects as the key management targets and reflects their effects to the design optimization. In this paper, we analyze the theory related to criticality analysis following US military standard, and propose a method to quantify the failure effect probability for objective criticality analysis. The criticality analysis according to the US military standard depends on the subjective judgment of the failure probability. The methodology for quantifying the failure effect probability is presented by using the reliability theory and the Bayes theorem. The failure rate is calculated by applying the method to quantify failure effect probability.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.551-554
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• 2012

한국항공우주연구원에서는 현재 1.5톤급 위성 발사체인 한국형 발사체 KSLV-II를 개발중이며 시스템의 설계 리뷰를 앞두고 있다. 또한, 발사체의 개발과정에 있어서 임무 보증 업무의 일환으로 신뢰성과 안전, 품질등을 관리하고 있으며 발사체의 안전 확보를 위해서 기존에 공표된 안전 보장 계획 및 시스템 안전 프로그램 계획에 따라 관련 업무를 수행하고 있다. 본 연구에서는 상기의 계획에 의거하여 수행된 사전 안전 분석의 내용과 방법에 대하여 설명하고 실제 추진기관 시스템에 대하여 도출된 위험요소들을 소개하고자 한다. 도출된 위험 요소들은 향후 개발이 진행되면서 위험 수준을 완화하는 방향으로 관리될 계획이다.