• Title/Summary/Keyword: Loosely Coupled

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Extreme Wave Hindcast in the Neighboring Seas of Korea from Loosely Coupled Wave-Tide-Surge Model (약결합된 해파-조석-해일 모형에 의한 한반도 주변해면의 최극해파 추정)

  • 최병호;엄현민
    • Proceedings of the Korean Society of Coastal and Ocean Engineers Conference
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    • 2000.09a
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    • pp.37-46
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    • 2000
  • 한반도 주변해역은 고조위와 태풍의 내습에 의한 강한 파랑으로 특징지워진다. 저조위때에 나타나는 1700$\textrm{km}^2$에 달하는 갯벌로 이루어진 서해안과 황해 동쪽 지역의 해안의 조건은 경기만에 l0m 범위의 높은 조위 차와 동계 계절풍과 태풍으로 인한 4-5m에 달하는 높은 파고를 발생시키는 고에너지와 높은 탁도 환경을 만들어 내는 매개체가 된다. (중략)

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ebXML Technical Archtecture

  • 김록원
    • Proceedings of the CALSEC Conference
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    • 2001.02a
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    • pp.405-426
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    • 2001
  • ◈ EDI ▶ 고비용이 요구되므로 주로 대기업에서 활용 ▶ 중소하청업체는 대기업 시스템에 통합된 모형 ◈ XML ▶ 전자 거래의 새로운 데이터 교환의 수단으로 등장 ▶ More open, more loosely-coupled more object- or component-oriented ▶ "EDI is dead"를 표방 ▶ 비즈니스 및 기술적 측면을 고려하지 알은 성급한 판단 ◈ EDI를 쉽게 포기하지 못하는 이유 ▶ EDI는 실제 비즈니스에 많이 이용되고 검증된 부분이 많음 ▶ EDI를 위한 그 동안의 많은 투자비용 ▶ XML을 이용한 비즈니스 메시지 설계 및 의미의 표준화가 이루어지지 않음(중략)

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A Study for Understanding and CSFs of SOA (SOA에 관한 이해와 구현 핵심성공요인 도출)

  • Lee, Sang-Min;Park, Jeong-Sun
    • Journal of the Korea Safety Management & Science
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    • v.12 no.4
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    • pp.247-254
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    • 2010
  • In this study, we reviewed SOA from the points of the concept, definition, technical components. Additionally, we derived seven critical factors which can lead SOA project to success: top level support, employees education, problem definition, service identification, appropriate development method, continuous development, start from small success.

Adaptive filter Design for INS/GPS (INS/GPS를 위한 적응필터 구성)

  • Yu Myeong-Jong
    • Journal of Institute of Control, Robotics and Systems
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    • v.11 no.8
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    • pp.717-725
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    • 2005
  • The adaptive filter is proposed for the INS/GPS. The proposed filter can estimate the variance of the process noise using the residual of the filter. To verify the efficiency of the adaptive filter, it is applied to the loosely-coupled INS/CPS that employs the additive quaternion error model. Simulation results demonstrate that the proposed filter is more effective in estimating the attitude error than EKF.

A Novel Quasi-Resonant ZCS-PFM DC-DC Switching Regulator with Loosely-Coupled Flyback Inductors

  • Chu E.H.;Chandhaket S.;Moisseev S.;Hiraki E.;Nakaoka M.;Kifune H.
    • Proceedings of the KIPE Conference
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    • 2001.10a
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    • pp.266-270
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    • 2001
  • This paper presents a novel topological prototype of voltage source series quasi-resonant zero current soft-switching pulse frequency modulated dc-dc power converter circuit using IGBTs which incorporates a high-frequency flyback transformer link. Its steady-state operating principle is described on the basis of simulation analysis, along with the open loop controlled power regulation characteristics of the multi-functional coupled inductors linked dc-dc power converter operating under a principle of zero current soft switching commutation.

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Performance Analysis of INS/GPS Integration System (INS/GPS 결합방식에 따른 성능분석)

  • Park, Young-Bum;Lee, Jang-Gyu;Park, Chan-Gook
    • Proceedings of the KIEE Conference
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    • 2000.07d
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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.

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Ultrawideband coupled relative positioning algorithm applicable to flight controller for multidrone collaboration

  • Jeonggi Yang;Soojeon Lee
    • ETRI Journal
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    • v.45 no.5
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    • pp.758-767
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    • 2023
  • In this study, we introduce a loosely coupled relative position estimation method that utilizes a decentralized ultrawideband (UWB), Global Navigation Support System and inertial navigation system for flight controllers (FCs). Key obstacles to multidrone collaboration include relative position errors and the absence of communication devices. To address this, we provide an extended Kalman filter-based algorithm and module that correct distance errors by fusing UWB data acquired through random communications. Via simulations, we confirm the feasibility of the algorithm and verify its distance error correction performance according to the amount of communications. Real-world tests confirm the algorithm's effectiveness on FCs and the potential for multidrone collaboration in real environments. This method can be used to correct relative multidrone positions during collaborative transportation and simultaneous localization and mapping applications.

Client-Server System Architecture for Inferring Large-Scale Genetic Interaction Networks (대규모 유전자 상호작용 네트워크 추론을 위한 클라이언트-서버 시스템 구조)

  • Kim, Yeong-Hun;Lee, Pil-Hyeon;Lee, Do-Heon
    • Bioinformatics and Biosystems
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    • v.1 no.1
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    • pp.38-45
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    • 2006
  • We present a client-server system architecture for inferring genetic interaction networks based on Bayesian networks. It is typical to take tens of hours when genome-wide large-scale genetic interaction networks are inferred in the form of Bayesian networks. To deal with this situation, batch-style distributed system architectures are preferable to interactive standalone architectures. Thus, we have implemented a loosely coupled client-server system for network inference and user interface. The network inference consists of two stages. Firstly, the proposed method divides a whole gene set into overlapped modules, based on biological annotations and expression data together. Secondly, it infers Bayesian networks for each module, and integrates the learned subnetworks to a global network through common genes across the modules.

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Research on supporting the group by clause reflecting XML data characteristics in XQuery (XQuery에서의 XML 데이터 특성을 고려한 group by 지원을 위한 질의 표현 기법에 대한 연구)

  • Lee Min-Soo;Cho Hye-Young;Oh Jung-Sun;Kim Yun-Mi;Song Soo-Kyung
    • The KIPS Transactions:PartD
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    • v.13D no.4 s.107
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    • pp.501-512
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    • 2006
  • XML is the most popular platform-independent data expression which is used to communicate between loosely coupled heterogeneous systems such as B2B Applications or Workflow systems. The powerful query language XQuery has been developed to support diverse needs for querying XML documents. XQuery is designed to configure results from diverse data sources into a uniquely structured query result. Therefore, it became the standard for the XML query language. Although the latest XQuery supports heavy search functions including iterations, the grouping mechanism for data is too primitive and makes the query expression difficult and complex. Therefore, this work is focused on supporting the groupby clause in the query expression to process XQuery grouping. We suggest it to be a more efficient way to process grouping for restructuring and aggregation functions on XML data. We propose an XQuery EBNF that includes the groupby clause and implemented an XQuery processing system with grouping functions based on the eXist Native XML Database.

Performance Analysis of an Integrated Navigation of an Airborne AESA Radar (항공기 탑재 AESA 레이다의 통합 항법 성능 분석 연구)

  • Lee, Dong-Yeon;Kwon, Hyeokjoon;Lee, Donguk;Lee, Haemin;Jung, Youngkwang;Jeong, Jaehyeon;Park, Sanggyu;Lee, Sungwon;Park, June Hyune;Tahk, Min-Jea;Bang, Hyochoong;Ahn, Jaemyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.4
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    • pp.281-290
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    • 2021
  • For successful operations of an airborne Active Electronically-Scanned Array (AESA) radar, which has various advantages over traditional radar systems, accurate and robust navigation is critical. This paper discusses a study on the performance analysis of an integrated navigation based on the Embedded GPS/INS (EGI) system for an aircraft equipped with an AESA radar. The models for generating the inputs for the GPS/IMU are developed. A navigation filter for a loosely-coupled GPS/IMU system is constructed. Overall navigation performance assessment procedure using a six degree of freedom aircraft simulator - along with the GPS/IMU models and the navigation filter - is introduced. The steps of the performance analysis procedure are explained using a comprehensive case study.