• 대한전기학회:학술대회논문집
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• 대한전기학회 2007년도 추계학술대회 논문집 전력기술부문
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• pp.162-164
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• 2007

This paper presents a HVDC site selection algorithm to increase transfer capability using VSC HVDC system which can control active power as well as reactive power. Using normal powerflow results and simple index $k_r$ the HVDC site selection algorithm is enhanced and more tightly-coupled transmission lines are identified in a domain of generators.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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• pp.251-256
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• 1994

Integration of intelligent robot workcell is now a hot issue in CIM and robotics area. This piper dealt with relatively low-level essential topics, i.e., multi-robot coordination and real-time communication for the integration of intelligent robot workcell. For the coordination of multi-robot system, the tightly-coupled coordination is proposed using the various sensors. In order to handle the numerous communication data, time-critical communication network (Field-bus) is introduced and investigated. Finally, intelligent robot workcell is suggested using the Mini-MAP and Field-bus.

• 대한전자공학회논문지
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• 제25권8호
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• pp.927-936
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• 1988

This paper proposes a pipelined memory access method as a new technique for a bus interface between processors and memories in tightly coupled multiprocessor systems. Since the shared bus is bottle neck of the system, model of pipelined access to memory has been developed. Results of the evaluation by the discrete time Markov model showed a significant improvement of the efficiency.

• 전자통신동향분석
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• 제14권4호통권58호
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• pp.133-134
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• 1999

MiDAS/IR 은 자료 저장 관리 시스템인 MiDAS-III 를 기반으로 하여 한글 전문 정보검색을 지원하는 시스템이다. 대부분의 정보검색 시스템은 자료를 상용 DBMS 또는 자료 저장 관리 시스템에 저장하고 정보검색 색인은 별도의 파일에 저장하여 관리하는 형태를 갖추고 있는데 반하여, MiDAS/IR은 MiDAS-III 와 정보검색기를 밀결합(Tightly coupled)시켜 자료는 물론 정보 검색 색인이 모두 하나의 저장소(MiDAS-III)에서 관리된다. 따라서 MiDAS/IR 은 정보검색 질의와 일반 데이터베이스 질의가 하나로 통합됨으로써 응용 프로그램의 작성이 쉽고 빠른 장점을 가지고 있다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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• pp.55-55
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• 2000

This paper presents a fault detection and isolation(FDI) method based on Ceneralized Likelihood Ratio(GLR) test for the tightly coupled INS/GPS. State and measurement GLR tests detect INS or GPS fault. Once the fault is detected, Multi-hypothesized GLR scheme performs the fault isolation between INS and GPS and find which satellite malfunctions. Simulation results show that the GLR method is effective enough to detect and isolate a fault of the integrated navigation system.

• 연구논문집
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• 통권24호
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• pp.129-140
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• 1994

Design and implementation of monitoring and control system using dual-microprocessor node is presented for real time process. The proposed system is implemented with 2 of the single chip microprocessors in tightly coupled mode and results in speed up of $s_p=1.74.$ Under the assumption that the nodes are interconnected in multidrop. the overall system performance such as average throughout-delay characteristics and effective throughput are analyzed using M/G/1 gueueing model, and results show that the proposed node can be used to medium sized distributed monitoring and control system.

• Journal of Advanced Marine Engineering and Technology
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• 제31권1호
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• pp.58-66
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• 2007

Genetic Algorithms (GA) have some difficulties in practical applications because of too many function evaluations. To overcome these limitations, an approximated modeling method such as Response Surface Modeling(RSM) is coupled to GAs. Original RSM method predicts linear or convex problems well but it is not good for highly nonlinear problems cause of the average effect of the least square method(LSM). So the locally approximated methods. so called as moving least squares method(MLSM) have been used to reduce the error of LSM. In this study, the efficient evolutionary GAs tightly coupled with RSM with MLSM are constructed and then a 2-dimensional inviscid airfoil shape optimization is performed to show its efficiency.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 하계학술대회 논문집 D
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• pp.2433-2435
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• 2000

Inertial Navigation System(INS) provides short-term accurate navigation solution but its error grows with time due to integration characteristics. Meanwhile, Global Positioning System(GPS) provides long-term stable solution but it has poor error characteristics in high dynamic region. So for its synergistic relationship, an integrated INS/GPS systems has been widely used as an advanced navigation system. Generally, two kinds of integration method are used. One is loosely coupled mode which uses GPS-derived position and velocity as measurements in an integrated Kalman filter. The other is tightly coupled one which uses pseudorange and pseudorange rate as Kalman filter measurements. In this paper the system error models and observation models for two kinds of integrated systems are derived, respectively, and their performance are compared through Monte-Carlo simulations.

• Journal of Communications and Networks
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• 제11권3호
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• pp.306-317
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• 2009

We consider the problem of architecting a reliable content delivery system across an overlay network using TCP connections as the transport primitive. We first argue that natural designs based on store-and-forward principles that tightly couple TCP connections at intermediate end-systems impose fundamental performance limitations, such as dragging down all transfer rates in the system to the rate of the slowest receiver. In contrast, the ROMA architecture we propose incorporates the use of loosely coupled TCP connections together with fast forward error correction techniques to deliver a scalable solution that better accommodates a set of heterogeneous receivers. The methods we develop establish chains of TCP connections, whose expected performance we analyze through equation-based methods. We validate our analytical findings and evaluate the performance of our ROMA architecture using a prototype implementation via extensive Internet experimentation across the PlanetLab distributed testbed.

• 한국항공우주학회지
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• 제41권2호
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• pp.134-141
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• 2013

항공기에 탑재되어 운용되는 링레이저 자이로 기반 스트랩다운 관성항법장치(SDINS)와 위성항법장치(GPS)의 결합 시스템의 실시간 구현에 있어서 설계시 고려해야할 문제에 대해서 살펴본다. SDINS/GPS 결합 시스템의 실시간 구현시, 레버암, 측정치 획득 및 오차 보상 외에, 링 레이저 자이로 기반의 SDINS의 특성을 고려해야만 한다. 뱅크턴을 반복적으로 수행하는 항공기에서 발생하는 누적 수직축 자세 오차를 추정하기 위해, 자이로의 비정렬이 모델링된 모델을 구현한다. 항공기 탑재 시험을 통해 수직축 자세 오차의 누적문제 및 실시간 구현 상의 문제를 해결하고, 자세 오차 추정 성능 향상 결과를 살펴본다.