• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.215-218
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• 2003

In this study, a performance model of the Smart UAV propulsion system with ducts, tip jets and variable main nozzle, which has flight capability of the rotary wing mode for the take-off/landing and low speed forward flight as well as the fixed wing mode for high speed forward flight, has been newly developed. With the proposed model, steady-state performance analysis was performed at various flight modes and conditions, such as rotary wing mode, fixed wing mode, compound wing, mode altitude and flight speed.

• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.1
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• pp.49-56
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• 2003

A steady-state performance simulation program using $EASY5^{(R)}$ on the turboprop engine was developed through in this study. The PT6A-62 turboprop engine which is the power plant of the first Korean basic trainer KT-1, was selected for this study. In order to evaluate the proposed perfrmance model the analysis results of $EASY5^{(R)}$ model were compared with the simulated results by the GASTURB program, which is well blown commercially for the simulation performance analysis at various cases. The first case was the uninstalled condition with various altitudes from ground to 30000ft and flight Mach No. 0. The second case was the install condition with various altitude from ground to M at the maximum take off and the ECS (Environmental Control System) OFF conditions. The third case was install condition with the altitude range from 5000 ft to 1000ft and Mach No. 0.1 to 0.3 at maximum ECS operating condition. It was confirm that the results by the $EASY5^{(R)}$ model were well agreed with those by GASTURB within maximum 5.0%

• Proceedings of the SAREK Conference
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• 2009.06a
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• pp.730-735
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• 2009

The purpose of this study is to consider improvement performance to prevent condensation and draw the optimum insulation design method for building using simulation tool. In this study, the three corners, weak part in condensation, were conducted by three-dimensional steady state simulation. From the results, it is required to strengthen insulation design, and it is founded that existing insulation system typically applied to most Korean apartment buildings has serious insulation defect that insulation is disconnected by structural components at the joints of wall-slab and wall-wall in envelope. So, it is considerate to need a concrete technology improvement.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1967-1968
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• 2008

본 논문에서는 안정성이 강화된 다중채널 적응 필터를 사용한 능동소음 제어 시스템을 제안한다. 초기에는 IIR필터의 극점을 원점방향으로 강제로 이동시켜 안정성을 확보하고, 망각인수를 도입하여 정상상태에 도달하면 최적 수렴치로 유지하게 함으로서 제어 정상상태 성능에는 영향을 미치지 않고 안정도가 강화 된 적응 IIR 필터 알고리즘을 제안한다. LMS 알고리즘의 수렴 성능을 개선하기 위한 방법으로 정규화기법을 사용하면 수렴 속도가 향상되지만 이에 비례하여 안정성이 떨어지게 된다. 소음원 입력의 파워가 시변 할 경우 적응 알고리즘의 안정성이 약화되는 문제점이 발생하는데, 본 논문에서는 Leaky LMS알고리즘과 비슷한 구조이지만 안정성이 강화된 IIR정규화 LMS 알고리즘을 제안한다. 제안한 알고리즘의 유용성을 비교 분석하기 위하여 실험을 수행하였다.

• The KSFM Journal of Fluid Machinery
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• v.5 no.2 s.15
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• pp.43-49
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• 2002

In this paper, the steady-state performances analysis of a tilting pad gas bearing(TPGB) we analyzed by using finite element method for compressible Reynolds' equation. TPGB is used in a high-expansion-ratio expander running at a speed of 230,000 rpm. In order to solve the nonlinear finite element equations, the Newton-Raphson method is applied. The variations of the loading capacity, friction force and tilting angle of a single pad v.s. eccentricity direction of eccentricity and bearing number are investigated. The condition for the equilibrium of a pad, which is important for safe working of the bearing, is stated. The performances of the three pad bearing such as loading capacity, friction moment are predicted.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.26 no.10
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• pp.2067-2072
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• 2002

The closed-loop state and input observer is a pole-placement type observer and estimates unknown state and input variables simultaneously. Pole-placement type observers may have poor performances with respect to modeling error and sensing bias error. The effects of these ill-conditioning factors must be minimized for the robust performance in designing observers. In this paper, the steady-state performance of the closed-loop state and input observer is investigated quantitatively and is represented as the estimation error bounds. The performance indices are selected from these error bounds and are related to the robustness with respect to modeling errors and sensing bias. By considering both transient and steady-state performance, the main performance index is determined as the condition number of the eigenvector matrix based on $L_2$-norm.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.11
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• pp.4718-4725
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• 2011

Intake-air flow and distribution characteristics of the 1600cc gasoline engine intake manifold have been studied using the computer simulation. Simulation has been conducted using both one-dimensional performance simulation and three-dimensional CFD software. Steady state flow simulation result of the intake manifold shows good distribution characteristics that the standard deviation of flow coefficients is below 1.0 percentage for both one- and three-dimensional simulation. Even though one-dimensional simulation result slightly overestimates compared with three-dimensional simulation result, both results show very good agreement in flow coefficient trend. Also, unsteady state simulation result shows consistent distribution characteristics with that of steady state. It is shown that unsteady state distribution characteristics might be able to be predicted through the steady state mass distribution result.

• Proceedings of the KIPE Conference
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• 2013.07a
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• pp.393-394
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• 2013

스위칭 방식의 DC/DC 컨버터에서 컨버터의 전류 및 전압은 스위칭 리플을 포함한 DC 맥류형태를 취하고 있다. 따라서 이러한 리플 및 노이즈를 저감하기 위해서 LPF(low-pass filter)를 사용하여 전압 및 전류를 검출하는 것이 일반적이다. 이러한 LPF의 차단주파수를 낮추면 정상상태에서 리플 및 노이즈 저감에는 그 성능이 우수하나 필터의 시 지연으로 인하여 제어기의 동특성은 현저히 저감된다. 따라서 본 논문에서는 낮은 차단주파수를 갖는 LPF를 기반으로 하여 과도상태 동특성을 개선할 수 있는 하이브리드 소프트웨어 필터를 제안한다. 제안된 하이브리드 필터는 필터의 입력 분을 관측하여 그 변동에 대한 평가함수를 정의하고 그 결과에 따라 스위칭 하는 방식을 취함으로 과도상태에서는 높은 차단주파수를 갖고 정상상태에서는 낮은 차단주파수를 갖는 필터회로 구성이 가능하였다. 또한 제안된 하이브리드 방식의 타당성을 검증하기 위하여 psim을 통하여 시뮬레이션을 행하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2002.10a
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• pp.42-43
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• 2002

• 한국항공운항학회:학술대회논문집
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• 2004.11a
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• pp.196-201
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• 2004