• 한국산업정보학회논문지
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• 제16권1호
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• pp.37-48
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• 2011

센서 네트워크 기술은 이러한 센서 노드를 특정한 지역에 대량으로 배치하여 네트워크를 구성한 후 센서 노드를 정보 제공의 매체로 활용하는 기술이다. 센서 노드는 매우 제한적인 하드웨어 자원을 가지고 있기 때문에 효율적인 자원 관리와 센서 네트워크상에서의 다양한 응용 환경을 제공하는 운영체제가 필요하다. 또한 원격 코드 업데이트는 이미 배포된 네트워크에서 응용 프로그램의 오류가 발생하여 이를 수정하거나 성능 개선을 위해 꼭 필요한 기술이다. 본 논문에서는 원격 코드 업데이트가 용이한 새로운 센서 노드용 운영체제, EPRCU(Easy to Perform Remote Code Update)를 제안한다. EPRCU는 이벤트 드리븐 방식의 실행 모델에서 에이징(Aging) 기법을 적용한 우선순위 기반의 프로세스 스케줄링 방식을 사용한다. 작업의 기본 단위인 프로세스는 로더에 의한 동적 메모리 할당 및 프로그램 메모리 관리 기능을 제공함으로써 무선 통신을 이용한 코드 업데이트 수행이 용이할 뿐만 아니라 다양한 센서 네트워크 응용에도 적합하다.

• 대한임베디드공학회논문지
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• 제2권3호
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• pp.145-154
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• 2007

Dynamic update of kernel can change kernel functionality and fix bugs in runtime. Dynamic update is important because it leverages availability, reliability and flexibility of kernel. An instruction-granularity update technique has been used for dynamic update. However, it is difficult to apply update technique for a commodity operating system kernel because development and maintenance of update code must be performed with assembly language. To overcome this difficulty, we design the function-granularity dynamic update system which uses high-level language such as C language. The proposed update system makes the development and execution of update convenient by providing the development environment for update code which is same for kernel development. We implement this system for Linux and demonstrate an example of update for do_coredump() function which is reported it has a vulnerable point for security. The update was successfully executed.

• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2007년도 추계학술발표회
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• pp.211-214
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• 2007

본 논문에서는 800MHz대역의 TRS(Trunked Radio System)대역을 비롯한, GSM(Global System for Mobile telecommunication), CDMA(Code Division Multiple Access) 대역을 통합할 수 있는 광대역 마이크로스트립 안테나를 설계하고자 한다. 그리고 선박 및 해상 안전에 상용 가능한 선박 기지국 중계기용 안테나를 설계하였다. 마이크로 스트립 안테나의 협대역을 개선하기 위해서 직사각형 패치에 U자 형태의 급전구조를 갖고, 그라운드와 급전 사이에 유전체(${\varepsilon}_T$ = 2.1), 패치와 급전 사이에는 유전체 (${\varepsilon}_T$ = 1)인 서로 다른 유전체를 사용하여 이중 공진 효과를 이용하였다. 설계된 안테나의 주파수 대역폭(VSWR 2:1)은 $780MHz{\sim}1.83GHz$로 2.61GHz의 광대역 특성을 보였으며. 또한 E-평면과 H-평면 모두 이득은 9.dBi이상. 3dB 빔폭은 E-평면 과 H-평면 $60^{\circ}$이상의 개선된 특성을 보였다.

• Steel and Composite Structures
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• 제19권6호
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• pp.1333-1354
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• 2015

A higher order analytical solution for static analysis of a truncated conical composite sandwich panel subjected to different loading conditions was presented in this paper which was based on a new improved higher order sandwich panel theory. Bending analysis of sandwich structures with flexible cores subjected to concentrated load, uniform distributed load on a patch, harmonic and uniform distributed loads on the top and/or bottom face sheet of the sandwich structure was also investigated. For the first time, bending analysis of truncated conical composite sandwich panels with flexible cores was performed. The governing equations were derived by principle of minimum potential energy. The first order shear deformation theory was used for the composite face sheets and for the core while assuming a polynomial description of the displacement fields. Also, the in-plane hoop stresses of the core were considered. In order to assure accuracy of the present formulations, convergence of the results was examined. Effects of types of boundary conditions, types of applied loads, conical angles and fiber angles on bending analysis of truncated conical composite sandwich panels were studied. As, there is no research on higher order bending analysis of conical sandwich panels with flexible cores, the results were validated by ABAQUS FE code. The present approach can be linked with the standard optimization programs and it can be used in the iteration process of the structural optimization. The proposed approach facilitates investigation of the effect of physical and geometrical parameters on the bending response of sandwich composite structures.

• Steel and Composite Structures
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• 제25권6호
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• pp.685-692
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• 2017

In this study, the effect of various adhesively bonded composite patches on mechanical properties of notched Al-Mg alloy plates was analyzed. For this purpose firstly, the un-notched and notched specimens were fabricated from 5086 Al-Mg alloys which have been used in armor-plated military vehicles. The surface notches as a flaw were machined with circular cutting tool to form notch aspect ratio a/c=0.15 and notch-to-thickness ratios a/t=0.5 in the radial direction on the test specimens. Then, various composite patches which reinforced by glass, carbon and Kevlar fibers were bonded adhesively at elliptically surface notches. Finally, experimental measurements conducted by applying tensile static loading. The experimental results showed that repairing with composite patches with order of carbon, glass and Kevlar fibers have remarkable effect on tensile strength of the notched plate. Also the finite element models were developed using Abaqus/Explicit code to predict the tensile strength and elongation of unrepaired notched specimen and specimen repaired by carbon fiber composite patch. The comparison between numerical and experimental results showed good agreement between them and proved the accuracy of numerical modeling.

• 천문학회보
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• 제39권1호
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• pp.75.1-75.1
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• 2014

Sunspot penumbrae show supersonic downflow patches along the periphery. These patches are believed to be the return channels of the Evershed flow. There was previous study to investigate their structure in detail using Hinode SOT/SP observations (M. van Noort et al. 2013) but their data sample was only two sunspots. To make general description it needs to check more sunspot sample. We selected 242 downflow patches of 17 sunspots using Hinode SOT/SP observations from 2006 to 2012. Height-dependent maps of atmospheric parameters of these downflows was produced by using HeLix which was height dependent LTE inversion code of Stokes profiles. The inversion code at high resolution allows for the accurate determination of small scale structures. The recovered atmospheric structure of three layers indicates that regions with very high downflow velocities contain very strong magnetic fields reaching up to 7kG. The higher downflow velocity patches have bigger patch size. Magnetic fields of downflow patches are more vertical while penumbra shows horizontal field and neighbor of downflow patches have opposite polarity. Temperature of downflow patches at highest layer have more strong value than penumbra at deepest layer. The direction of velocity of downflow patches at highest layer have two branches. These result shows that we can expect some heating precess in the middle of layer.

• 정보보호학회논문지
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• 제15권5호
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• pp.47-57
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• 2005

현재의 스마트카드는, 경제적인 이유 때문에 보안 문제가 발생할 수 있음에도 불구하고, 카드를 재사용할 수 있는 초기화 명령어와 패치 코드를 추가할 수 있는 패치 명령어가 들어있는 경우가 많다. 이러한 트랩도어 명령어들은 세련된 기법으로 만들어지고 일반에게 공개되지 않기 때문에 기존의 테스트 소프트웨어로 검출하는 것은 매우 어렵다. 지금까지 알려진 가장 효율적인 방법은 ITSEC에서와 같이 개발과정을 통제하고 소스 코드를 분석하는 것이다. 그러나 이러한 방법은 오랜 시간을 요구하고 비용이 많이 든다. 이에 본 논문에서는 시차 분석과 전력 분석을 이용하여 스마트카드의 트랩도어를 검출할 수 있는 새로운 방법을 제안한다. 그리고 실험에 의해 제안한 방법이 효율적이며 실질적인 접근 방법임을 보여준다.

• 한국전자통신학회논문지
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• 제14권2호
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• pp.303-308
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• 2019

스프링 프레임워크는 우리나라 공공기관의 웹서비스 개발도구의 표준이라 할 만큼 전자정부 프레임워크의 기반 기술로 많이 사용되고 있다. 그러나 최근 스프링 프레임워크를 이용한 애플리케이션에서 원격코드 실행 취약점(CVE-2018-1270)이 발견되었다. 본 논문은 스프링 프레임워크를 서버를 대상으로 발생한 취약점의 위험성을 해킹 시나리오 POC(Proof Of Concept)를 이용한 취약점 실험 분석 방법을 제안한다. 종국적 대응방안으로 버전 4.3.16와 버전 5.0.5 이상으로 패치를 제안한다. 아울러 제안한 해킹시나리오 취약점 실험분석이 보안 프로그램의 성능향상 및 새로운 인증체계의 구축을 위한 자료로 활용될 것으로 기대한다.

• Structural Engineering and Mechanics
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• 제52권1호
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• pp.137-147
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• 2014

The present paper deals with the first ply failure analysis of the laminated composite plates under various static and dynamic loading conditions. Static analysis has been carried out under patch load and triangular load. The dynamic failure analysis has been carried out under triangular pulse load. The formulation has been carried out using the finite element method and a computer code has been developed. The first order shear deformation theory has been applied in the present formulation. The displacement time history analysis of laminated composite plate has been carried out and the results are compared with those published in literature to validate the formulation. The first ply failure load for laminated composite plates with various lamination schemes under static and dynamic loading conditions has been calculated using various failure criteria. The failure index-time history analysis has also been carried out and presented in this paper.

• 대한기계학회논문집
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• 제18권7호
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• pp.1808-1817
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• 1994

Unsteady aerodynamic analysis of an aircraft is done using a frequency domian 3-D panel method. The method is based on an unsteady linear compressible lifting surface theory. The lifting surface is placed in a flight patch, and angle of attack and camber effects are implemented in upwash. Fuselage effects are not considered. The unsteady solutions of the code are validated by comparing with the solutions of a hybrid doublet lattice-doublet point method and a doublet point method for various wing configurations at subsonic and supersonic flow conditions. The calculated results of dynamic stability derivatives for aircraft are shown without comparision due to lack of available measured data or calculated results.