• Proceedings of the Korean Nuclear Society Conference
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• 1996.05c
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• pp.52-58
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• 1996

본 연구에서는 반응성 마그네트론 스퍼터 이온플래이팅법에 의해 Co계 합금인 stellite 6B 기판 위에 증착된 TiN 박막의 증착특성을 조사하였다. 증착된 박막의 증착속도는 기판에 인가된 bias 가 증가함에 따라 박막의 치밀화와 resputtering으로 인해 감소하였으며 박막의 형상은 bias가 인가되지 않은 상태에서의 open columnar 구조에서 bias가 인가된 경우 columnar 구조가 사라진 매끈하고 치밀한 구조로 변화하였다. 기판 bias가 인가된 경우 N/Ti 조성비는 거의 stoichiometry를 만족하였으며 증착된 박막의 우선성장 방위는 $N_2$의 양이 감소할 수록 (200)에서 (111)로, bias 증가에 따라서는 (200)에서 (111)을 거쳐 (220)으로 변화하였다. 박막의 경도는 박막이 압축응력을 나타낼수록 증가하였으며, bias가 인가된 경우 약 2000~3300kgf/$\textrm{mm}^2$의 높은 경도를 나타내었다.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05c
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• pp.105-110
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• 1996

$CO_2$ laser beam을 이용하여 예민화 Alloy 600 재료의 표면을 용융하여 상온의 $Na_2$S$_4$O$_{6}$ 용액에서 일정변형률 시험을 하였으며, TEM으로 용융된 부위의 미세조직을 관찰하였다. Laser beam으로 표면용융시킨 예민화 Alloy 600에서는 표면용융하지 않은 시편의 IGSCC 파괴와는 달리 연성파괴가 일어났으며, 이 시편의 파단면은 as-received 시편의 연상파괴에 의한 파단면과 유사하게 dimple 형상을 보여주었다. 한편, laser로 표면용융된 부위의 응고조직은 cellular 조직을 나타내고 있었으며, cell boundary는 높은 밀도의 dislocation이 엉켜있었다. EDX로 cell과 cell 사이, 그리고 결정립과 결정립 사이의 경계를 가로질러 성분분석을 한 결과 두경계면에서 Cr이 matrix에서보다 높게 측정되었다. Laser로 표면용융한 예민화 Alloy 600에서의 IGSCC 저항성 증가는 이러한 경계면에서의 Cr 증가 때문인 것으로 유추된다.

• 제어로봇시스템학회:학술대회논문집
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• 1993.10a
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• pp.250-255
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• 1993

In this paper, for detection and isolation of instrument and process faults related with steam generator(S/G) in nuclear power plant, two types of observers are designed based on the linearized dynamic model of S/G : a bank of Dedicated Observers (DOS) for instrument faults detection and a bank of Unknown Input Observers(UIO) for process faults detection. And then, they are combined to decide which one between the above two faults occurs. In principle, the failure in ith instrument(process) can be isolated by monitoring the error between the ith output and its estimation obtained from the ith DOS(UIO). It is shown via computer simulations that the present scheme is feasible in finding out the source of a fault.

• Journal of Institute of Control, Robotics and Systems
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• v.22 no.5
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• pp.339-345
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• 2016

This paper presents a robust speed control of an autonomous vehicle using a disturbance observer. For the purpose, the transfer function of speed dynamics of an autonomous vehicle is identified using step response data. Based on the identified transfer function, model based PID (Proportional-Integral-Derivative) control is designed. In order to design a robust control against load variations on the vehicle, a disturbance observer (DOB) based control is devised. The performance of the designed DOB based control is demonstrated by real experiments.

• Journal of Institute of Control, Robotics and Systems
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• v.17 no.8
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• pp.753-759
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• 2011

The HIV (Human Immunodeficiency Virus) causes AIDS (Acquired Immune Deficiency Syndrome). The process of infection and mutation by HIV can be described by a 3rd order state equation. For this HIV model that includes the dynamics of the mutant virus, we present a parameter estimation scheme using two state variables sporadically measured, out of the three, by employing a genetic algorithm. It is assumed that these non-uniformly sampled measurements are subject to random noises. The effectiveness of the proposed parameter estimation is demonstrated by simulations. In addition, the estimated parameters are used to analyze the equilibrium points of the HIV model, and the results are shown to be consistent with those previously obtained.

• Journal of Institute of Control, Robotics and Systems
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• v.20 no.8
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• pp.822-827
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• 2014

This paper presents a robust observer-based output feedback control for stabilization of linear time invariant systems with polytopic uncertainties. To this end, this paper not only finds a robust observer gain but also suggests how to determine the model used in the observer, which is not obvious due to model uncertainties in the conventional observer design method. The robust observer gain and the observer model are selected in a way that the whole closed-loop is stable by solving LMIs and BMIs (Linear Matrix Inequalities and Bilinear Matrix Inequalities). A simulation example shows that the proposed robust observer-based output feedback control successfully leads to closed-loop stability.

• Proceedings of the Korea Port Economic Association Conference
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• 2007.07a
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• pp.291-312
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• 2007

This paper is designed to look for a specialized strategies by drawing the special features of Busan New Port from both a comparative analysis of major factors of harbor competitiveness and a SWOT analysis of Yangshan Port, one of the biggest competitive ports in Northeast Asia, so that Busan New Port may preoccupy a status as the hub port of the area. The researcher would like to suggest the following measures to make Busan New Port serve as the central port of Northeast Asia on the basis of the findings; Korea should push ahead with creating a railroad transportation linking with Eurasia Contient, secure the amount of goods and resources with the help of the early development of the surrounding complex of the port, make a considerable progress in the level of port service, come up with a differentiation strategies for harbor marketing activities and improve its productivity.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.277-280
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• 2006

This paper describes the aerodynamic interference characteristics between the ing and the engines in a commercial airplane which is realized by reverse engineering based on the photo measurement. Steady three-dimensional compressible inviscid Euler equation is solved in the unstructured grid system under the cruise condition. The lift and drag forces in the wing with engines increase by 1.49% and 3.9%, respectively compared with the wing without engines.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.323-326
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• 2006

This paper presents the computational results for the two-dimensional compressible non-reacted flow in a converging-diverging micro thrust nozzle of which the ratio of exit to throat width (0.541 in.) is 1.8. The RNG model is applied to calculate the turbulence by loading the standard coefficients. The results agreed very well with the experiments in the view of the shock structure and the pressure distribution at the various pressure ratios between the stagnation and the environmental states. The plume structures are also discussed on the view of the shock-cell structure.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.61-64
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• 2003

A comprehensive understanding is given for the hot-firing test results, which were obtained throughout the verification program of mono-propellant hydrazine thrusters producing 0.95 lbf (4.2 Newtons) of nominal steady-state thrust at an inlet pressure of 350 psia (2.41 ㎫). The scrutiny is made in terms of thrust and temperature behavior of steady state firing mode at the given propellant injection pressures of 400, 250, 100, and 50 psi. Engineering philosophy of data measurement and reduction is shortly mentioned, too.