• 한국멀티미디어학회논문지
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• 제19권12호
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• pp.2014-2023
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• 2016

Web presence is one of the key issues for extensive deployment of Internet-of-Things (IoT). An obstacle to overcome for Web presence is relatively low computing power of IoT devices. In this paper, we present implementation of an IoT platform based on Constrained Application Protocol (CoAP) which is a web transfer protocol proposed by Internet Engineering Task Force (IETF) for the low performance IoT devices such as Wireless Sensor Network (WSN) nodes and micro-controllers. To qualify the performance of CoAP-based IoT system for such an application as smart grid, we designed a test platform consisting of Raspberry Pi2, Kmote WSN node and a desktop PC. Using open source softwares, CoAP was implemented on top of the platform. Leveraging the GET command defined at CoAP specification, performance of the system was measured in terms of round-trip time (RTT) from web application to the Kmote sensor node. To investigate abnormal cases among the test results, hop-by-hop delays were measured to analyze resulting data. The average response time of CoAP-based communication except the abnormal data was reduced by 23% smaller than the previous research result.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제8권10호
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• pp.3607-3623
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• 2014

The increasing demand in promoting cloud computing in either business or other areas requires more security of a cloud storage system. Traditional cloud storage systems fail to protect data integrity information (DII), when the interactive messages between the client and the data storage server are sniffed. To protect DII and support public verifiability, we propose a data integrity verification scheme by deploying a designated confirmer signature DCS as a building block. The DCS scheme strikes the balance between public verifiable signatures and zero-knowledge proofs which can address disputes between the cloud storage server and any user, whoever acting as a malicious player during the two-round verification. In addition, our verification scheme remains blockless and stateless, which is important in conducting a secure and efficient cryptosystem. We perform security analysis and performance evaluation on our scheme, and compared with the existing schemes, the results show that our scheme is more secure and efficient.

• 한국콘텐츠학회논문지
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• 제5권1호
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• pp.209-215
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• 2005

1990년대로부터 시작된 전자정부 프로젝트는 정보처리 기반의 구축, 정부내 조직 개혁, 웹을 통한 정부조달과 정부서비스의 제공 등에 초점을 둠으로써 대부분의 프로젝트가 정부기관의 기능을 강화하는 전자정부시스템의 개발에 집중되었다. 현재 거버넌스 관점에서 시민참여에 대한 이론 및 실증적 연구는 많이 되고 있으나 시민참여의 개선에 중점을 둔 전자정부 시스템, 소위 전자거버넌스 시스템의 개발에 대한 연구는 상대적으로 적은 관심 밖에 받지 못하고 있다. 본 논문은 전자거버넌스 시스템의 특성과 핵심 요구사항을 분석하고 이를 만족시킬 수 있는 기본적인 시스템 구조를 제시한다.

• 한국콘텐츠학회:학술대회논문집
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• 한국콘텐츠학회 2007년도 추계 종합학술대회 논문집
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• pp.259-264
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• 2007

기존의 그리드 환경에서 독립적으로 개발된 단위 e-Science 응용 서비스가 효율적으로 활용되기 위해서는, 기 개발된 단위 e-Science 응용 서비스들을 협업 환경에서 일련의 워크플로우로 통합할 수 있고 이를 실행할 수 있는 기술 및 관련 기술의 개발이 필요하다. 이를 위해 본 논문에서는 실제 활용되고 있는 e-Science 응용 환경 중 하나인 항공우주분야의 e-Science 환경의 연구 시나리오로부터 e-Science 워크벤치가 갖추어야 할 요구사항을 분석하였다. 또한 이렇게 분석된 요구사항을 바탕으로 실제 e-Science 워크벤치의 기능 및 아키텍처의 설계를 수행하였다.

• 한국정보통신학회논문지
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• 제9권2호
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• pp.361-365
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• 2005

원서명자의 서명권한을 대리서명자가 수행하도록 지정하는 대리서명기법은 Mambo[1]이래로 많은 연구가 이루어졌으며, 분산네트워크, 그리드 컴퓨팅, 전자 상거래 둥 많은 분야에 응용되고 있다. Araki[6]에서는 기존의 대리서명 기법을 확장하여 다단계 대리서명을 제안하였다 그러나 이 연간결과는 보안상의 취약점이 존재하는 것으로 드러났다. 이 논문에서는 다단계 대리서명을 위한 서명권한 위임 프로토콜을 설계하였다. 이 프로토콜은 보안채널을 요구하지 않으며 권한위임 및 위임수락 부인이 불가능하고 지정된 대리서명자 이외에 제3자에 의한 서명위조가 불가능하며 권한위임기간 만료이전이라도 위임을 철회할 수 있다는 장점을 갖는다.

• 인터넷정보학회논문지
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• 제8권3호
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• pp.57-63
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• 2007

분산 무선 네트워크에서 작업을 수행하기 위해서는 이동 단말기에 안정적인 전원의 공급이 필수적인 요소이다. 본 논문에서는 무선 네트워크에서 작업을 수행하기에 제한적인 조건인 전원문제의 해결을 위해서 모바일 단말기들의 이동성 관리를 통한 분산 작업을 효율적으로 수행하는 방안을 제시하였다. 에너지 사용량은 통계모델을 통하여 분석할 수 있으며, 또한 이동성 관리를 통해서 모바일 단말기 내에서 분산작업 수행시에 필요한 에너지 필요량을 예측할 수 있다. 그러므로 본 논문을 통하여 정규적인 이동성을 가지는 이동 단말기들을 통하여 안정적으로 분산 작업을 수행할 수 있는 알고리즘 및 그 유효성을 제시하였다.

• 한국전산유체공학회지
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• 제20권4호
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• pp.28-35
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• 2015

BARAM system that means 'wind' in Korean has been established as a virtual wind tunnel system for aircraft design. Its aim is to provide researchers with easy-to-use, production-level environment for all stages of CFD simulation. To cope with this goal an integrated environment with a set of CFD solvers is developed and coupled with an highly-efficient visualization software. BARAM has three improvements comparing with previous CFD simulation environments. First, it provides a new automatic mesh generation method for structured and unstructured grid. Second, it also provides real-time visualization for massive CFD data set. Third, it includes more high-fidelity CFD solvers than commercial solvers.

• 대한기계학회논문집B
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• 제21권8호
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• pp.1024-1033
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• 1997

The past several years have witnessed an ever-increasing acceptance and adoption of parallel processing, both for high performance scientific computing as well as for more general purpose applications. Furthermore with increasing needs to perform the complex flow calculations in an efficient manner, the use of the message passing model on distributed networks has emerged as an important alternative to the expensive supercomputers. This work attempts to provide a generic framework to enable the parallelization of all CFD-related works using the master-slave model. This framework consists of (1) input geometry, (2) domain decomposition, (3) grid generation, (4) flow computations, (5) flow visualization, and (6) output display as the sequential components, but performs computations for (2) to (5) in parallel on the workstation clustering. The flow computations are parallized by having multiple copies of the flow-code to solve a PDE on different spatial regions on different processors, while their flow data are exchanged across the region boundaries, and the solution is time-stepped. The Parallel Virtual Machine (PVM) is used for distributed communication in this work.

• Journal of Computing Science and Engineering
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• 제2권4호
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• pp.321-338
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• 2008

This paper presents a Modified Multiple Depth First Search algorithm for the exploration of the indoor environments occupied with obstacles in random distribution. The proposed algorithm was designed and implemented to employ one or a team of Khepera II mini robots for the exploration process. In case of multi-robots, the BlueCore2 External Bluetooth module was used to establish wireless networks with one master robot and one up to three slaves. Messages are sent and received via the module's Universal Asynchronous Receiver/Transmitter (UART) interface. Real exploration experiments were performed using locally developed teleworkbench with various autonomy features. In addition, computer simulation tool was also developed to simulate the exploration experiments with one master robot and one up to ten slaves. Computer simulations were in good agreement with the real experiments for the considered cases of one to one up to three networks. Results of the MMDFS for single robot exhibited 46% reduction in the needed number of steps for exploring environments with obstacles in comparison with other algorithms, namely the Ants algorithm and the original MDFS algorithm. This reduction reaches 71% whenever exploring open areas. Finally, results performed using multi-robots exhibited more reduction in the needed number of exploration steps.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.120-124
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• 2007

Helicopters and rotary-wing vehicles encounter a wide variety of complex aerodynamic phenomena and these phenomena present substantial challenges for computational fluid dynamics(CFD) models. This investigation presents the rotor aerodynamic analysis items for the helicopter development and variety aerodynamic analysis methods to provide the better solution to researchers and helicopter developers between aerodynamic problems and numerical aerodynamic analysis methods. The numerical methods to make an analysis of helicopter rotor are as below - CFD Modelling : actuator disk model, BET model, fully rotor model,... - Grid : sliding mesh, chimera mesh / structure mesh, unstructure mesh,... - etc. : panel method periodic boundary, quasi-steady simulation, incompressible,... The choice of CFD methodology and the numerical resolution for the overall problem have been driven mostly by available computer speed and memory at any point in time. The combination of the knowledge of aerodynamic analysis items, available computing power and choice of CFD methods now allows the solution of a number of important rotorcraft aerodynamics design problems.