• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.53-56
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• 2012

항공기에 작용하는 공기역학적 힘인 양력과 항력은 항공기 날개 설계에서 성능을 좌우하는 성능지수로 주로 이용된다. 본 연구에서는 NACA0012 airfoil 모델의 공력특성을 EDISON 열유체 시뮬레이션 프로그램(이하 EDISON)을 이용해 분석하고 검증해 보았다. 아음속 유동의 특정 조건에서 받음각과 유동형태에 따른 공력특성 분석을 수행하여 받음각에 따라 변하는 양력계수, 항력계수, 양항비, 실속각과 천음속 유동 조건에 맞추어진 마하수 0.5~1.22 영역에서 변하는 항력계수를 기존 데이터와 비교 검증했다.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.3
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• pp.34-40
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• 2012

A pressure control law to regulate pressure of gas generator is suggested. To design a model based control law, the governing equation which consists of Robert and conservation equation is built and verified through the ground burning test. PID and nonlinear adaptive control laws are designed to analyze the loop response characteristics under the system which has varying eigen properties arisen from combustion volume change. 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 shows 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.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.

• Journal of the Institute of Electronics Engineers of Korea SD
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• v.41 no.3
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• pp.1-8
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• 2004

The anomalous behavior of the 1/f noise of halo or pocket ion implanted MOSFETs is investigated. The model for the anomalous 1/f noise behaviors of MOSFETs, which consist of inhomogeneous conductance along the channel is improved within a regional approximation as previous works and presented in a fen directly applicable to halo MOSFETs. The presented model reduces to the previous results, discussed in the linear region operation, for small drain bias. Comparisons with experimental results show that the 1/f model based on the regional approach can be applicable for limited ranges, especially for sufficiently large gate bias voltages.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2001.11a
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• pp.57-62
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• 2001

본 연구에서는 검증된 BSU 3톤/일급 석탄가스화공정에 대해 개발된 동적모델을 폐유가스화 공정모텔에 적용하였다. 대상공정에 포함된 조작변수들의 변동에 따른 주요 공정변수인 산소/폐유비를 3% 계단증가시킨 결과, 폐유가스화기의 압력은 15분의 시상수를 보이며 최종적으로 2.4%가 증가된 정상상태에 도달하였고, 온도는 초기 1분 이내에 약 3.2%의 급격한 증가를 보인 후 최종적으로 4.1% 증가된 정상상태에 도달하였다. 그리고 생성가스의 조성은 이산화탄소가 6% 증가되었고, 일산화탄소와 수소는 각각 2% 및 8% 감소된 새로운 정상상태에 도달하였다. 이러한 결과를 토대로 폐유가스화기의 부하변동에 따른 주요 공정변수들의 변동경향 및 신뢰성 있는 동적모사 결과를 얻고, 개발된 모델에 cascade 및 ratio 방식의온도, 압력 제어로직을 설계하여 실공정 적용실험을 통한 전산모사결과 및 안정된 운전특성을 검증할 수 있는 기초를 마련하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.19-22
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• 2009

Design and performance evaluation of $H_2O_2$ monopropellant thrusters to be used at attitude control of space launch vehicles were presented in this paper. Flight model thrusters were designed after two reactors for 100, 250 Newton were conformed at engineering model. Each thruster was evaluated by measurement of characteristic velocity, thrust, specific impulse, and pulse response times.

• Journal of Biosystems Engineering
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• v.23 no.6
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• pp.549-560
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• 1998

The dynamic model of a tractor-trailer system developed in the first part of this paper was verified in this article by comparing the simulated acceleration responses of the system with actually measured ones. A commercially available tractor and a trailer were used for the verification test. Values of the model parameters were measured or theoretically derived if the measurement was practically impossible. The tractor-trailer system was operated with different forward speeds over three equally spaced half-sine bumps on the flat concrete surface. Results of the verification tests showed that autospectra of the measured and simulated accelerations of the tractor-trailer system agreed well up to the frequencies slightly feater than the fundamental frequencies of the ground excitations and at the frequencies of engine excitations. The mean of normalized errors of the simulated responses to the measured ones was estimated to be less than 10% for all the test runs. The peak responses in the autospectra also coincided well both in the frequency and magnitude.

• Proceedings of the KIPE Conference
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• 2018.07a
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• pp.334-335
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• 2018

본 논문에서는 스위칭 소자의 저항을 고려한 벅 컨버터의 소신호 모델링을 통해 회로를 등가화하고, 등가 모델의 동특성을 분석하였다. 또한 분석한 결과를 토대로 3P2Z(3Pole 2Zero) 제어기를 기반으로 한 전압 보상 제어기를 구현하였다. MATLAB을 이용하여 등가 모델을 바탕으로 설계한 제어기의 안정도를 판별 및 분석하였고, 최종적으로 PSIM을 사용한 시뮬레이션을 통해 분석한 결과가 타당함을 검증하였다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2012.04a
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• pp.515-516
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• 2012

• Proceedings of the Korean Institute of Intelligent Systems Conference
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• 2002.12a
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• pp.135-138
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• 2002

본 논문에서는 비최소위상 시스템으로 표현되는 화력발전소 드럼의 수위제어를 위한 퍼지 제어기를 제안한다. 제안된 방법은 T. Takagi와 M. Sugeno의 퍼지모델을 기반으로 수행된다. 그리고 기존의 PID 및 LQ 제어기법을 적용한 방식과 비교하여 제안된 방법의 개선된 특성을 시뮬레이션 결과로부터 검증하였다.