• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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• pp.131-131
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• 2000

In this paper, a design method of a fault diagnosis filter for a system with multiplicative faults which cause to change its parameters is developed. Linear time-invariant systems are dealt with in discrete-time domain. The residual which is sensitive to a damage of control surface of an aircraft by parity space approach is defined. Next, the fault is isolated by a new decision logic. Control reconfiguration is achieved by the result of fault diagnosis. Finally, the feasibility of the method is illustrated with a simulation study of a fault diagnosis system for a damaged control surface of an aircraft.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2006년도 하계종합학술대회
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• pp.571-572
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• 2006

A simulation tool for design space exploration of a real-time reconfiguration system was developed in this paper. We described an algorithm for a partial real-time reconfiguration to utilize already existing configured functional units and applied it to H.263 encoder application. This scheme allows us to find a starting configuration for the further optimization without actually building a prototype.

• International Journal of Aeronautical and Space Sciences
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• 제14권2호
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• pp.183-192
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• 2013

This paper presents formation reconfiguration using impulsive control input for spacecraft formation flying. Spacecraft in a formation should change the formation size and/or geometry according to the mission requirements and space environment. To modify the formation radius and geometry with respect to the leader spacecraft, the follower spacecraft generates additional control inputs; the two impulsive control inputs are general control type of the spacecraft system. For the impulsive control input, Lambert's problem is modified to construct the transfer orbit in relative motion, given two position vectors at the initial and final time. Moreover, the numerical simulation results show the transfer trajectories to resize the formation radius in the radial/along-track plane formation and in the along-track/cross-track plane formation. In addition, the maneuver characteristics are described by comparing the differential orbital elements between the reference orbit and transfer orbit in the radial/along-track plane formation and along-track/cross-track plane formation.

• 한국경제지리학회지
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• 제16권2호
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• pp.198-217
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• 2013

본 연구에서는 원격진료 이용자 행태를 시공간 재구조 관점에서 살펴보았고, 원격진료의 양면적 성격, 즉 확장성과 제약성에 관해 고찰하였다. 연구 결과에 의하면, 원격진료의 도입은 직접적인 온라인 서비스의 수혜자인 환자의 행태 변화에 영향을 끼치나, 이는 원격진료 이전의 일반적 의료 행태와 확연한 차이를 보인 것은 아니다. 이와 더해, 의원급 병원의 의료진 및 원격진료 최종 서비스 제공자인 토가네현립병원의 의료진의 행태에는 거의 영향을 주지 않는 것으로 나타났다. 원격진료의 도입으로 인해 의료기관에로의 접근성 및 효용성의 향상에 도움이 된 것은 사실이나, 여전히 원격진료는 최소한 한번 이상의 직접 진료를 요구하고 있고, 인간의 생명과 직접적으로 연계됨에도 불구하고 불완전한 기술적 특성을 가지고 있으며, 원격진료 이용에 있어서의 의사-환자, 의사 사이의 합의 문제로 인해 시공간적 제약성을 내포하게 된다. 결과적으로, 당초 원격진료가 처음 고안되었을 당시 많은 이용자들에게 주었던 기대감(확장성)과 달리, 오늘날의 원격진료는 시공간을 초월한 개념이라기보다는 기술, 사회, 문화, 경제 등의 다양한 요인으로 인해 제약성을 내포한 형태로 발전하고 있다고 할 수 있다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 하계학술대회 논문집 D
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• pp.2439-2442
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• 2000

This paper presents a practical On-The-Fly(OTF) integer ambiguity resolution algorithm for real-time precise positioning with low cost, $L_1$ single frequency, conventional C/A code GPS receiver. A state reconfiguration scheme is adopted in the Kalman filter to deal with the variation of ambiguity states caused by varying sets of visible GPS satellites. The proposed algorithm reduces the ambiguity search space from the coarse m-level C/A code pseudorange measurements of the conventional C/A code reciever, thereby reducing the computational time. Simulation results are presented to show that the algorithm achieves a cm-level accuracy.

• Journal of Power Electronics
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• 제16권3호
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• pp.1012-1024
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• 2016

This study deals with an on-line software fault detection, localization, and system reconfiguration method for electrical system drives composed of three-phase AC/DC/AC converters and three-phase permanent magnet synchronous machine (PMSM) drives. Current sensor failure (outage), speed/position sensor loss (disconnection), and damaged DC-link voltage sensor are considered faults. The occurrence of these faults in PMSM drive systems degrades system performance and affects the safety, maintenance, and service continuity of the electrical system drives. The proposed method is based on the monitoring signals of "abc" currents, DC-link voltage, and rotor speed/position using a measurement chain. The listed signals are analyzed and evaluated with the generated residuals and threshold values obtained from a Sliding Mode Current-Speed-DC-link Voltage Observer (SMCSVO) to acquire an on-line fault decision. The novelty of the method is the faults diagnosis algorithm that combines the use of SMCSVO and adaptive thresholds; thus, the number of false alarms is reduced, and the reliability and robustness of the fault detection system are guaranteed. Furthermore, the proposed algorithm's performance is experimentally analyzed and tested in real time using a dSPACE DS 1104 digital signal processor board.

• Journal of Astronomy and Space Sciences
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• 제21권3호
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• pp.209-220
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• 2004

Some methods have been presented to get optimal formation trajectories in the step of configuration or reconfiguration, which subject to constraints of collision avoidance and final configuration. In this study, a method for optimal formation trajectory-planning is introduced in view of fuel/time minimization using parameter optimization technique which has not been applied to optimal trajectory-planning for satellite formation flying. New constraints of nonlinear equality are derived for final configuration and constraints of nonlinear inequality are used for collision avoidance. The final configuration constraints are that three or more satellites should be placed in an equilateral polygon of the circular horizontal plane orbit. Several examples are given to get optimal trajectories based on the parameter optimization problem which subjects to constraints of collision avoidance and final configuration. They show that the introduced method for trajectory-planning is well suited to trajectory design problems of formation flying missions.

• 한국생산제조학회지
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• 제21권3호
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• pp.473-478
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• 2012

In this paper, the air bubble formation mechanism in the rectangular and triangular line-and-space pattern during dispensing UV Nanoimprint Lithography (UV-NIL) at an atmospheric condition is studied. To investigate the air bubble formation, an analytic model based on geometric approach and a numerical model based on CFD(computational fluid dynamics) were used in the analysis. It was found in the numerical analysis that every time the flow front passed through a corner of the pattern, it proceeded with a newly formed shape, occurring due to interface reconfiguration, since the flow fronts were formed such that they minimized the surface energy. Moreover, the conditions for the air bubble formation were investigated by applying the analytic analysis based on geometric approach and the numerical analysis. Good overall agreement was found between the analytic and numerical analysis.

• 한국벤처창업학회:학술대회논문집
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• 한국벤처창업학회 2022년도 춘계학술대회
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• pp.157-161
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• 2022

Building on the DC interaction model between a parent company and its spin-offs, we examine that a dyadic relationship can be differentiated within the functions of space, motivation, and time. We investigate that these three factors encompassing the parent-spin-off DC relationship can be applicable to both linear(i.e., geographic proximity and low spin-off CEO's salary is positive) and nonlinear(i.e., too much frequency of new spin-off creation is as harmful as too little) effects on determining the performance of spin-off firms. The direction of causality is underpinned by social capital, human capital, and compensation-activation theory rather than by the normal consequences of previous empirical research. Further, our results suggest the overlap between DC and entrepreneurship; namely, spin-off firms create, learn, and exploit opportunities through a reconfiguration of parent DC so that DC establishes itself as a key concept in the entrepreneurship domain.

• 한국항공우주학회지
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• 제33권9호
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• pp.56-65
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• 2005

시간유한요소법은 시간영역을 고정시키고 행렬 미분방정식 형태의 공간전파 관계식을 풂으로써 시간과 공간에 대한 동적 해석을 수행하는 방법이다. 이 방법은 공간이산화 유한요소법이나 시/공간 동시이산화 유한요소법에 비해 공간에 관한 자유도가 발생하는 것이 두드러진 특징으로, 이를 이용하여 분포형 구동기의 공간에 따른 특성을 최적화하는 데에 효율적으로 사용될 수 있다. 본 논문에서는 임의의 초기조건을 반영할 수 있도록 구성된 상태변수 벡터를 이용하여 구조물을 시간영역에서 이산화하고, 공간영역에서 전파관계식 및 경계조건을 이용하여 공간전파 관계식을 형성하였다. 이 때 구동기의 공간에 따른 형상 분포는 설계되어야 할 변수의 함수이고, 시간반응은 형상함수를 이용하여 이산화 하였다. 포텐셜 에너지 및 운동에너지를 구조물의 변위제어에 적절한 최적의 성능지수로 설정하고, 이를 최소화하도록 미지의 함수인 구동기의 분포형상을 구하였다. 일반적으로 구조물은 임의의 초기조건에서 외란을 받게 되나, 본 연구에서는 구현가능한 제어법칙을 이용하여 최종시간에서 안정화(rest) 조건을 만족한다고 가정하였다. 구동기 분포형상 최적화를 위해 상태/준상태 방정식을 유도하였다. 서브행렬 재형상화와 시/공간 경계조건을 통해 상태변수와 준상태변수에 대한 Ricatti 미분방정식을 유도하였다. 이를 통해 구동기 분포형상 최적화를 구현하였으며, 수치 시뮬레이션을 통해 적절한 구동기의 분포형상 최적화를 수행할 수 있음을 보였다.