• 한국컴퓨터정보학회논문지
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• 제13권7호
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• pp.127-138
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• 2008

무기체계 연구개발 프로세스를 위한 형상/정보관리시스템은 오랜 연구개발 과정에서 생산되는 문서, 도면, 구성품정보, 구조정보 등에 대한 동시공학 및 협업적 업무를 지원해야 한다. 본 논문에서는 웹 환경에서 운영되는 무기체계 연구개발 형상/정보관리시스템을 구현하기 위한 CBD (Component Based Development) 개발 및 모델링 방법론에 관한 논문으로서 기존의 연구에서는 일반적인 MVC 모델을 사용한 3계층의 시스템 아키텍처를 구성하는 반면 본 논문에서는 J2EE 환경하의 EJB 구조를 기반으로 한 4계층 시스템 아키텍처를 정의하였다. 본 논문에서는 4계층 시스템 아키텍처를 통하여 모델 계층과 제어 계층을 각각 두 단계로 세분화하여 컴포넌트의 속성을 구체화할 수 있는 방안을 제시하였으며, 컴포넌트 기반으로 시스템 개발 업무를 수행하여 각 개발 단계별 표현 모델에 대한 시스템 결과물을 산출하여 실제 시스템을 구현하였다.

• 한국전자통신학회논문지
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• 제17권4호
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• pp.663-670
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• 2022

본 연구는 한국형 합동 전술데이터링크 체계 사업의 사례를 통해 무기체계 소프트웨어 개발 및 관리 매뉴얼에서 규정하고 있는 무기체계 소프트웨어 신뢰성 시험이 정의되기 전에 획득한 소프트웨어 자산을 안정적으로 무기체계에 통합하는 방안을 제시한다. 이를 위하여 무기체계 소프트웨어 신뢰성 시험에 대한 개요와 한국형 합동 전술데이터링크체계 사업의 특성에 따른 신뢰성시험 적용의 문제점을 기술하고, 각 문제점에 대한 사업의 결정안과 이를 통한 기대 효과를 기술한다.

• 품질경영학회지
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• 제45권3호
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• pp.349-364
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• 2017

Purpose: The purpose of this study is to analyze quality control strengthening pilot project in development stages of weapon systems which ensures zero-defect. In order to achieve that, we propose collaboration support system between related organizations. Methods: First, we analyze how quality control methods has been developed from reviewing the preliminary study in commercial and defense industry. Then, we suggest improvement plans for quality control in defense industry and propose a pilot study which able to improve the recognized problems. Results: The results of this study ensures the participants in defense industry recognize the importance of quality control and form a consensus by sharing a case study. Finally, we propose the standardized work process by utilizing manual and manpower dispatching. Conclusion: As a result, this study clarifies the scope and role of relevant organizations to achieve the defense quality assurance in the total life cycle(TLC). Also, this paper guides the collaboration system between the relevant organization which differs from the commercial industry currently divided into development-production-quality.

• 한국통신학회논문지
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• 제35권11B호
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• pp.1715-1724
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• 2010

본 논문은 미군의 국방정보체계에 대한 상호운용성 평가모델로 개발된 LISI(Level of Information System Interoperability) 모델을 기반으로 국방과학연구소에서 한국군 환경에 적합하도록 개선시킨 한국군의 LISI 모델의 제한사항을 분석하고 대안을 제시한다. 한국군의 LISI 모델은 국방 상호운용성의 유일한 평가기관인 국군지휘통신사령부(이하 "국통사") 예하의 "합동 상호운용성 기술센터"에서 획득규정에서 정의한 모든 체계(정보체계, 무기체계, 비무기체계)의 상호운용성 평가시 적용하고 있다. 그러나, LISI 모델은 기본적으로 정보체계간 상호운용성을 평가하는 모델로 개발되었으므로 NCW 환경에서 요구되는 정보체계와 무기 및 비무기체계를 포함하는 복합체계 상호운용성 평가에 미흡하기 때문에 최근 미군은 SOSI(System of Systems Interoperability) 모델을 연구개발하고 있다. 따라서 미군의 LISI 모델을 벤치마킹하여 개선시킨 한국군의 LISI 모델은 국방정보체계는 물론 우기 및 비무기체계의 상호운용성을 평가하는 도구로 사용하기에는 근본적인 제한사항을 가질 수밖에 없으며, 이러한 제한사항을 보완하기 위해 국방부와 관련기관에서 연구를 통하여 개선대책을 제안하고 있다. 본 논문은 LISI 모델의 응용(P), 기반(I), 데이터(D) 분야 평가기준 및 평가가 완료된 단위체제간의 비교평가 절차에 대한 제한사항을 분석하고, 이를 극복하기 위한 정책적 대안을 제시한다.

• 한국군사과학기술학회지
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• 제5권1호
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• pp.96-106
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• 2002

Many modern guided weapon systems employ sophisticated target sensors as well as powerful computing systems. Due to such advanced features, they are required to achieve better guidance accuracy, and at the same time other guidance objectives for better weapon effectiveness and survivability. In this paper, we overview some of the technical considerations in such advanced guidance algorithm development, and briefly look at some related research works. More specifically, we discuss impact angle control, time-varying nature of the guidance system, time-to-go estimation, guidance loop stability, effect of autopilot lag and physical limitations in control variables, parasitic paths in guidance loops, etc. We also briefly look at some advanced concepts such as integrated guidance and control loop design, target adaptive guidance, guidance law development based on dual control concept, and terminal evasive maneuver.

• 한국군사과학기술학회지
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• 제10권4호
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• pp.138-144
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• 2007

This paper introduces the design techniques of an IR module using the 2-D array un-cooled type infrared detector which is applied to the individual combat weapon. Considering the size and weight of the hand carried weapon system, we used a very small-sized detector and applied an adaptive temperature control algorithm so that the operation consumed with low power can be possible. We applied the AR(Auto Regressive) filter to improve the signal-to-noise ratio in a thermal image processing step. We also applied the plateau equalization and boundary enhancement techniques to improve the visibility for human visual system.

• 제어로봇시스템학회논문지
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• 제12권7호
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• pp.713-718
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• 2006

Supersonic jet fighter aircraft have several different weapon loading configuration to support air-to-air combat and air-to-ground delivery of weapon modes. Especially, asymmetric loading configurations could result in decreased handling qualities for the pilot maneuvering of the aircraft. The design of the T-50 lateral-directional roll axis control laws change from beta-betadot feedback structure to simple roll rate feedback structure and gains such as F-16 in order to improve roll-off phenomena during pitch maneuver in asymmetric loading configuration. Consequently, it is found that the improved control law decreases the roll-off phenomenon in lateral axes during pitch maneuver, but initial roll response is very fast and wing pitching moment is increased. In this paper, we propose the lateral control law blending between beta-betadot and simple roll rate feedback system in order to decreases the roll-off phenomenon in lateral axes during pitch maneuver without degrading of roll performance.

• 대한안전경영과학회지
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• 제17권3호
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• pp.195-204
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• 2015

The live fire test has been playing a critical role in evaluating the goals-to-meet of the weapon systems which utilize the power of explosives. As such, the successful development of the test systems therein is quite important. The test systems development covers that of ranges and facilities including system-level key components such as mission control, instrumentation or observation, safety control, electric power, launch pad, and so on. In addition, proper operational guidelines are needed with well-trained test and operation personnel. The emerging weapon systems to be deployed in future battle field would thus have to be more precise and dynamic, smarter, thereby requiring more elaboration. Furthermore, the safety consideration is becoming more serious due to the ever-increasing power of explosives. In such a situation, development of live fire test systems seems to be challenging. The objective of the paper is on how to incorporate the safety and other requirements in the development. To achieve the goal, an architectural approach is adopted by utilizing both the system components relationship and safety requirement when advanced instrumentation technology needs to be developed and deteriorated components of the range are replaced. As an evaluation method, it is studied how the level of maturity of the test systems development can be assessed particularly with the safety requirement considered. Based on the concepts of both systems engineering and SoS (System-of-Systems) engineering process, an enhanced model for the system readiness level is proposed by incorporating safety. The maturity model proposed would be helpful in assessing the maturity of safety-critical systems development whereas the costing model would provide a guide on how the reasonable test resource allocation plan can be made, which is based on the live fire test scenario of future complex weapon systems such as SoS.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 22-24 Oct. 1991
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• pp.274-279
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• 1991

The development of a guided weapon system, such as a tactical missile, requires a performance analysis of a nonlinear system. Generally, the Monte Carlo analysis method is used for this purpose. The limitation of this method, a large number of simulations, for a nonlinear system performance analysis strongly motivated the development of a more efficient analytic technique. In this paper, the statisfical linearization methods is used for the performance analysis to the guided weapon system with the help of covariance analysis technique. Because the statistical linearization methods cannot be used to the look-up table nonlinear form such as aerodynamic coefficients, the second order polynomial representations is obtained from the table using the Lagrange interpolating polynomial and linearized statistically. Simple simulations about initial state conditions and random component in guidance command shows the results of this technique.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1992년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 19-21 Oct. 1992
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• pp.590-595
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• 1992

An integrated guidance scheme for guided weapon system is described in this paper. Against conventional guidance methods, this method combines an autopilot and a guidance law. The controller is designed using LQ regulator whose performance index is different from other optimal guidance laws. Since dynamics of the system is considered in the derivation, the controller performance is improved. By simulation, the suggested method shows better performance in minimum distance sense than conventional guidance schemes such as Bang Bang guidance or Pursuit Guidance. Since the suggested method provides smooth rudder deflection in contrast to the conventional method, the load on a energy source of the system can be greatly lessened.