• 제목/요약/키워드: Integrated Defense

검색결과 407건 처리시간 0.025초

DMRUT-MCDS: Discovery Relationships in the Cyber-Physical Integrated Network

  • Lu, Hongliang;Cao, Jiannong;Zhu, Weiping;Jiao, Xianlong;Lv, Shaohe;Wang, Xiaodong
    • Journal of Communications and Networks
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    • 제17권6호
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    • pp.558-567
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    • 2015
  • In recent years, we have seen a proliferation of mobile-network-enabled smart objects, such as smart-phones and smart-watches, that form a cyber-physical integrated network to connect the cyber and physical worlds through the capabilities of sensing, communicating, and computing. Discovery of the relationship between smart objects is a critical and nontrivial task in cyber-physical integrated network applications. Aiming to find the most stable relationship in the heterogeneous and dynamic cyber-physical network, we propose a distributed and efficient relationship-discovery algorithm, called dynamically maximizing remaining unchanged time with minimum connected dominant set (DMRUT-MCDS) for constructing a backbone with the smallest scale infrastructure. In our proposed algorithm, the impact of the duration of the relationship is considered in order to balance the size and sustain time of the infrastructure. The performance of our algorithm is studied through extensive simulations and the results show that DMRUT-MCDS performs well in different distribution networks.

Dilution of Precision 정보를 이용한 INS/GPS 결합시스템 위치오차 개선 (Improving INS/GPS Integrated System Position Error using Dilution of Precision)

  • 김현석;백승준;조윤철
    • 한국항행학회논문지
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    • 제21권1호
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    • pp.138-144
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    • 2017
  • 본 논문에서는 INS/GPS결합 시스템에서 GPS가 기만신호 또는 지형지물에 의한 가시선이 제한되어 위성의 기하학적 배치가 저하되는 조건을 고려하였고, 통합항법 성능을 향상시키기 위한 방법을 제안하였다. 먼저 GPS의 DOP에 측정 공분산 이 연동되는 가변 공분산 확장 칼만필터(VCEKF)를 제시하였다. 그리고 몬테칼로 시뮬레이션을 통하여 EKF와 VCEKF를 사용한 통합항법 시스템의 항법성능을 분석하였다. DOP 값이 낮은 경우보다 DOP값이 높을 경우에 VCEKF가 확정 공분산을 사용하는 EKF보다 우수한 추정 성능을 보임을 확인할 수 있었다.

국방연구개발 사업에 EVMS 적응방안 연구 (A Study oil the Application of EVMS in Defense R&D Programs)

  • 최석철;김종필
    • 한국군사과학기술학회지
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    • 제8권1호
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    • pp.62-68
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    • 2005
  • In this paper, we review the general technique of Earned Value Management System(EVMS) which is the integrated management for cost, schedule and performance, and suggest an application of the integrated management of cost and schedule in the research and development(R&D) programs for defense acquisition.

TICN 전술백본망을 위한 라우팅 프로토콜 분석 (Analysis of Routing Protocol for Tactical Backbone of TICN)

  • 장동기;권태욱
    • 한국군사과학기술학회지
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    • 제13권4호
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    • pp.650-658
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    • 2010
  • Recently Korea Army developed the TICN which is the next army tactical communication system. The TICN will support ability from under environment, strategy maneuver communication system of integrated army dimension overcome and NCW. If the IER(Information Exchange Requirement) phases 3 of the future application system, the analysis that a transmission ability of the TICN is the uncapable is govern. The TICN tactical backbone's ability is very important. Therefore, network efficiency index in application and analysis of the standard protocol for the data transmission guarantee are obliged. For the TICN tactical backbone, this paper analyzes of routing protocol efficiency index and compares to superiority of the OSPF(v2) and integrated IS-IS protocols in the tactical environment. Conclusively we proposed that integrated IS-IS protocol is more suitable for TICN backbone routing protocol.

기동헬기 통합시현 및 경고 기능 설계 (Design to Integrated Display and Caution Function for KHP)

  • 김성우;고은경;이병화
    • 한국항공우주학회지
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    • 제45권6호
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    • pp.481-489
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    • 2017
  • 상황인식은 비행 또는 항공기를 유지하는 작업에서 진행 상황을 파악하는데 필요한 모든 사항을 인식하는 것을 의미한다. 상황인식은 환경에 대한 정보를 단순히 인지하는 것 이상을 기본으로 하며 정보의 의미를 통합된 형태로 제공하는 것이 중요하다. 한국형 기동헬기는 통합된 형태의 상황인식을 위하여 통합 상황시현 및 우선순위 기반 청각 신호경고를 시각 신호와 동조하여 조종사에게 제공한다. 통합 상황시현 및 효율적인 경고 제공으로 운용자 과실을 줄이고 운용자에게 임무의 핵심작업 및 이벤트에 집중할 수 있게 한다. 본 논문은 한국형 기동헬기에서 구현한 통합 상황시현 및 경고 설계를 소개한다.

통합된 상용 툴을 이용한 전투기급 항공기 개념설계 (Conceptual Design of Fighter-class Aircraft Using Integrated Commercial Tools)

  • 이성진;남화진;박영근;오장환;이대열
    • 한국군사과학기술학회지
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    • 제17권2호
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    • pp.189-196
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    • 2014
  • Automated design program using commercial process integration and optimization program was developed for conceptual design of fighter-class aircraft. Wind tunnel test data and performance analysis results were compared for the verification of analysis tool of this program, and the usefulness of the tool was found. After integration with radar cross section analysis tool, the correlation with configuration design variables of wing, tail and performance parameters was identified by design of experiment, and the optimized configuration for weight and RCS was derived from optimization of empty weight and average frontal RCS value. After parameter definition of fuselage, the program can be implemented for full aircraft configuration.

무인기 항공전자 체계의 아키텍처 개발 동향연구 (A Study on the Trend of an Avionics System Architecture Development for UAV)

  • 김성우;심재익;이왕국;이우진;원대연
    • 한국군사과학기술학회지
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    • 제17권4호
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    • pp.436-447
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    • 2014
  • The major elements of avionics system architecture are requirements, Real Time Operating System, message communication, memory, and data format etc. Herein describes a state-of-the-art development trend for the avionics system architecture, system requirements and data bus among the major elements of avionics system. While, domestic technology has been tried to Integrated Modular Avionics(IMA) system based on the Avionics Full Duplex Switched Ethernet(AFDX) technology during Light Attack Helicopter(LAH) project in Korea, but not yet proved as the product case in Full Scale Development Phase. The avionics system architecture considering the domestic inexperience of the IMA system architecture are suggested for the Next-generation Corps Unmanned Aircraft System.

무기체계의 고장 이력 데이터를 활용한 소프트웨어 신뢰도 분석 모델 적용 사례 연구 (The Case Study on Application of Software Reliability Analysis Model by Utilizing Failure History Data of Weapon System)

  • 조일훈;황성국;이익도;박연경;이정훈;신창훈
    • 한국신뢰성학회지:신뢰성응용연구
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    • 제17권4호
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    • pp.296-304
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    • 2017
  • Purpose: Recent weapon systems in defense have increased the complexity and importance of software when developing multifunctional equipment. In this study, we analyze the accuracy of the proposed software reliability model when applied to weapon systems. Methods: Determine the similarity between software reliability analysis results (prediction/estimation) utilizing data from developing weapon systems and system failures data during operation of weapon systems. Results: In case of a software reliability prediction model, the predicted failure rate was higher than the actual failure rate, and the estimation model was consistent with actual failure history data. Conclusion: The software prediction model needs to adjust the variables that are appropriate for the domestic weapon system environment. As the reliability of software is increasingly important in the defense industry, continuous efforts are needed to ensure accurate reliability analysis in the development of weapon systems.

고 세장비 일체형 복합재 날개 제작 연구 (A Study on Manufacture of Integrated Composite Wing with High Aspect Ratio)

  • 주영식;전우철;변관화;조창민;한진욱
    • 한국항공우주학회지
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    • 제41권2호
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    • pp.127-133
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    • 2013
  • 본 논문에서는 일체형 복합재 날개 제작에 대한 연구를 수행하였다. 날개는 피벗구조 형태 및 양항비가 큰 고 세장비 구조를 가지고 있다. 날개는 가벼워야할 뿐만 아니라 구조성능 요구조건을 만족하는 충분한 강도 및 강성이 요구되므로 탄소섬유 복합재를 적용하여 설계하였다. 제작비용을 줄이기 위해 구성 부품을 일체형으로 설계하여 구조 부품수를 감소시키고, 오토클레이브를 사용하여 날개를 일체성형으로 제작하였다. 제작공정별 시편시험을 수행하여 재료물성을 확인하였으며, 부분품시험을 통하여 일체성형에 따른 구조성능을 검증하였다.

국방품질성숙도지수의 개발 및 평가에 관한 연구 (A Study on the Development & Evaluation of Defense Quality Maturity Index)

  • 정영권;조현기;유한주
    • 품질경영학회지
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    • 제47권3호
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    • pp.479-496
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    • 2019
  • Purpose: The purpose of this research is to develop defense quality evaluation model in order to improve the problem of private sector quality evaluation model and propose the total integrated defense quality management model which enables to evaluate not only large defense industry, but also small-medium industry. Methods: This paper consider the characteristics on ISO 9001 Quality Management System, single PPM, PASS and defense quality and develop defense quality maturity model and index which enables to measure the current quality management level and characteristics and to evaluate operational characteristics in each maturity level for domestic defense industry. Results: From 176 DQMS certified defense industry, the defense quality maturity level is 68,2, C grade. The large defense industry shows, 80.9, A grade; medium industry 69.7, C grade; small-medium industry shows 54.1, D grade. Through the classified types of industries, the current level of quality management of defense industries was diagnosed and the areas to be supplemented for the total quality management were identified. Conclusion: Developed DQMI can be used as the basic information for spreading quality management activities in the defense industry by diagnosing the overall quality management of existing defense industries and quantifying the ambiguity of non-metric measurements and measurement standard that were presented as the threshold of the defense quality management system certification process.