• Tuberculosis and Respiratory Diseases
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• v.39 no.2
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• pp.199-204
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• 1992

A 46 years old male showed radiologically a single cavitary nodular lesion in right upper lung, which extended to the regional chest wall. This finding has to be made into differential diagnosis of numerous pulmonary diseases including infections such as mycobacterial, fungal or bacterial, granulomatous diseases, and neoplasms. For the definite diagnosis, fine needle aspiration biopsy guided by biplane fluoroscopy was performed. The aspirates contained several sulfur granules, in the center of which many gram positive, filamentous organisms were compactly intermingled. Such a findings was compatible with pulmonary actinomycosis. Now the lesions is cleared out by medical treatment with amoxicillin for 3 months.

• Proceedings of the Korea Institutes of Information Security and Cryptology Conference
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• 2006.06a
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• pp.608-612
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• 2006

센서네트워크는 유비쿼터스 컴퓨팅 기술의 핵심으로 자리 잡아가고 있다. 이러한 센서네트워크는 네트워크가 갖는 특성으로 인하여 일반 네트워크보다 보안에 취약하므로 안전한 통신을 위하여 센서 노드 간 키를 설정하는 것은 보안을 위한 기본적인 요구사항이 되고 있다. 센서네트워크를 클러스터링하여 각 클러스터별로 유일한 다항식을 할당하는 클러스터기반 키 분배에서 클러스터 헤더가 할당하는 다항식 부분정보(polynomial share)인 일변수 다항식 정보는 키 분배시 도청에 의하여 클러스터 헤더의 키인 이변수 다항식을 계산할 수 있었다. 따라서 본 논문에서는 클러스터헤더가 동일한 클러스터내의 센서노드들에게 다항식 부분정보를 배분할 때 다항식을 계산한 상수값을 분배함으로써 클러스터에 도청으로부터 다항식을 알아낼 수 없게 하여 센서노드 간 안전한 통신을 할 수 있게 하였다.

• Proceedings of the Korean Information Science Society Conference
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• 2004.04a
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• pp.289-291
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• 2004

정보시스템에 대한 침입탐지는 네트워크 기반의 침입탐지시스템에 의존하였으나, 네트워크 규모의 확대와 암호사용의 증가로 인하여 호스트 기반의 침입탐지시스템을 중심으로 연구되고 있다. 본 논문에서는 CB(Check-Box)에 규정된 정책을 이용한 호스트 기반의 침입탐지 시스템을 설계하여 이를 실험하였다. 침입탐지 실험을 위한 시스템호출 기술은 커널에 프로세스들의 특성을 자세하게 정의하고, 이를 실행할 수 있도록 기반을 구축함으로서 가능하게 하였다. 이러한 기법의 특성은 실행 가능한 프로세스가 시스템에 자원에 정당하게 접근할 수 있는 정책을 자세하게 규정해야 하며, 규정을 기술하기 위한 언어는 보안영역을 효과적으로 표현하고 번역될 수 있어야 한다. 본 연구는 Linux의 커널에서 침입탐지기법에 대한 모형을 제시하고, 공격에 대한 탐지와 탐지결과를 검증할 수 있는 정책을 설정하였다. 제안된 시스템은 커널의 변화에 대한 영향력을 최소화하도록 함으로서 새로운 커널을 쉽게 설치할 수 있기 때문에 정책에 의한 호스트기반의 침입탐지시스템은 운영 탐지 분석을 통하여 침입을 예방할 수 있는 방안을 마련할 수 있다.

• Journal of Engineering Education Research
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• v.16 no.6
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• pp.52-57
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• 2013

In this paper, the evaluation system in order to achieve the program education objectives of Accreditaion Board for engineering education of Korea, analyze the educational objectives evaluation tool case studies of programs that are run by each university, the program educational objectives to match the actual situation of university I have developed a distinction between questions the evaluation and assessment system. Configuration, execution, measurement, analysis, is a five-step mooring, the evaluation tool, is a graduate research you are currently using the most in Korea, the employer survey, education target assessment model of the program, employment trends of graduates, I decided to graduate focus group interviews. Distinction between questions, the evaluation also developed a questionnaire to derive the important keywords of education for each objectives. Improvement evaluation tool, the evaluation criteria is required, the University is preparing evaluate (NGR) in South Korea engineering education certification next regularly, requires research on semantic analysis of the results of measurement of the educational goals of the program in the future some.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.618-623
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• 2011

A pressure control law to regulate pressure of gas generator is suggested. To design a model based control law, the governing equation which is consisted of Robert and conservation equation is built and verified through the ground burning test. PID and nonlinear adaptive control laws are designed to evaluate the loop response characteristics under the system which has varying eigen properties as combustor volume is increased. It is suggested that new approach, gain scheduling design, is required to overcome the defects identified from numerical simulation results of the two control laws. The newly suggested scheme showed good control performance even under disturbances and measurement noise.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.588-593
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• 2011

In this study, the performance analysis method for ramjet engine system with atmospheric air disturbance was proposed. Flight path was determined to satisfy dynamic pressure constant at each flight altitude. The atmospheric air disturbance incoming into a engine intake was simulated by the model Tank proposed. The performance parameters was investigated at each flight condition with air disturbance. Engine operation stability was evaluated as analysis of the normal shock position.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.579-583
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• 2011

The component based propulsion modeling and simulation of an air-breathing engine such as ramjet and scramjet is studied. The simulation model has been realized considering the characteristics of the air-breathing engine which is composed of air intake, combustor and nozzle including engine controller and fuel supply system. To estimate the engine performance and to verify the engine controller, real time based Hardware in the Loop System simulating actual environment is constructed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.295-298
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• 2008

In this paper, prototype dynamic modeling scheme to control ramjet propulsion systems were proposed. From the physical understandings of engine system, a typical 2nd-order system model was applied to simulate the dynamic characteristics of fuel supply system. The shock location varience in diffuser to chamber pressure fluctuation is calculated so that the out of phase between two signals was observed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.128-132
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• 2009

Digital control system for active combustion control of lab-scale combustor equipped with secondary fuel injection is designed. Controllability with adaptive law is revealed with the Cambridge Combustor model and the requirement for control system is derived. The input and output requirements of frequency estimator and fuel supply actuator for the adaptive control law is verified with cold tests. The system can be used as digital based active combustion controller having 150Hz combustion instability.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.111-115
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• 2009

The method of test for observing the combustion instability and controling the instability actively by using secondary injection of fuel through flame stabilizer was studied by constructing model combustor of supersonic engine. The frequency of combustion instability was detected by measuring the pressure of combustor using pressure sensor and by optical sensing of flame intensity. Electro-magnetic valve was adopted as actuator for active control and the characteristics of modulated fuel was studied by measured pressure of valve outlet and scattering signal of spray at secondary fuel injection.