• 품질경영학회지
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• 제41권3호
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• pp.487-494
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• 2013

Purpose: In this study, we propose the precision guided munitions verification methodology using the statistical analysis method has been proposed. and it can be applied to the precision guided munitions quality assurance work. Methods: This modeling is based on Failure Mode and Effects Analysis, Statistical Process Control, Defense Quality Managerment System, Production Readiness Review, Manufacturing Readiness Assesment and so on. Results: The Process Control Modeling that has the following procedures ; searching the critical to quality, statistical analysis by process, verify process. Moreover, the effectiveness of the methodology is verified by applying to the precision guided munitions. Conclusion: To achieve a analysis methods of statistical process control and verify process for precision guided munitions.

• 한국항공우주학회지
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• 제35권3호
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• pp.225-230
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• 2007

• 시스템엔지니어링학술지
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• 제2권2호
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• pp.39-44
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• 2006

With the advent of low cost, miniature and high-g hardened inertial sensors and actuators, many kind of smart munitions are becoming practical such as 1D or 2D TCM, SFM, Range Extended GPS guided munitions and so on. They have more complicated trajectory control algorithm than conventional munitions'. Therefore it is necessary to study the complicated operation algorithm of smart munitions with M&S in advance of developing them. The purpose of this paper is to introduce a practical M&S method to study an operation concept of smart munitions using PRODAS and Matlab.

• Journal of Positioning, Navigation, and Timing
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• 제7권3호
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• pp.127-138
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• 2018

Spoofing attacks including meaconing can provide a bogus position to a victim GPS receiver, and those attacks are notably difficult to detect at the point of view on the receiver. Several countermeasure techniques have been studied to detect, classify, and cancel the spoofing signals. Based on the countermeasure techniques, we have developed an anti-spoofing equipment that detects and mitigates or eliminates the spoofing signal based on raw measurements. Although many anti-spoofing techniques have been studied in the literatures, the evaluation test system is not deeply studied to evaluate the anti-spoofing equipment, which includes detection, mitigation, and elimination of spoofing signals. Each study only has a specific test method to verify its anti-spoofing technique. In this paper, we propose the performance evaluation test system that includes both spoofing signal injection system and its injection scenario with the constraints of stand-alone anti-spoofing techniques. The spoofing signal injection scenario is designed to drive a victim GPS receiver that moves to a designed position, where the mitigation and elimination based anti-spoofing algorithms can be successively evaluated. We evaluate the developed anti-spoofing equipment and a commercial GPS receiver using our proposed performance evaluation test system. Although the commercial one is affected by the test system and moves to the designed position, the anti-spoofing equipment mitigates and eliminates the injected spoofing signals as planned. We evaluate the performance of anti-spoofing equipment on the position error of the circular error probability, while injecting spoofing signals.

• 한국정보통신학회논문지
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• 제23권4호
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• pp.365-373
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• 2019

본 논문은 정밀 유도무기에 장착되어 목표물 명중 확률을 좌우하고, 비용적인 측면에서 유도무기의 가장 큰 부분을 차지하는 적외선 영상탐색기에 대한 성능 대비 개발비용 최적화에 대한 연구이다. 탐색기 개발 비용의 주요항목인 해상도와 그에 따른 탐지성능에 영향을 미치는 인자들을 분석함으로써, 설계 단계에서 해상도 별 탐지성능과 개발 비용과의 상관관계를 분석하는 연구를 수행하였다. 다양한 신호 대 클러터 비 조건에서 해상도 별 표적탐지 확률을 설계 시 중요인자로 정의하고, 개발비용 선정의 기준이 되는 해상도 별 탐지성능 분석을 수행하였으며, 탐지성능 확보를 위한 최적의 해상도와 그에 따른 투입비용에 대한 관계를 도출하였다. 다양한 클러터 환경에 따른 사례연구를 통하여 제안한 분석 방식이 탐지성능 만족을 위하여 요구되는 개발비용 예측에 효과적임을 검증하였으며, 유도무기 운용 환경에서 성능대비 최적화된 개발비용을 설계단계에서 미리 도출할 수 있는 연구 자료로 활용하고자 한다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.303-306
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• 2006

A roll rate estimation method is proposed using the GPS measurement for spinning vehicles such as guided munitions and smart bombs. Before designing the roll rate estimator, the carrier phase and the carrier frequency deviation caused by spinning have been observed. Based on the observation, the spinning frequency is estimated using I and Q value from the correlator. The proposed method is evaluated through computer simulations using a software defined receiver and a GPS IF signal generator.

• 한국국방경영분석학회지
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• 제3권2호
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• pp.119-134
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• 1977

The goal of this study is to determine which is the better bomb; a general purpose bomb or a special bomb, from the point of view of cost-effectiveness of air munitions. What we call the special bomb is a laser guided bomb which adds a guidance control unit on the head of a general purpose bomb. Althrough their characteristics of explosion are the same, their effectivenesses are very defferent due to their probability of hitting the targets. Now, in order to measure their relative a effectiveness, we could select various enemy targets such as runway, radar, and then Ive could also calculate requirments of both bombs and firghter aircraft sorties according to the desired damage level of each target, Following above steps, we can derive the total costs and compare effectiveness. As a results of this study, when the attrition rate of aircraft is under $1.1\%$, the general purpose bomb is better than the laser guided bomb. Above $1.1\%$ attrition rate, we could say that luser guided bomb is the most economical bomb.

• 한국군사과학기술학회지
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• 제13권6호
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• pp.1019-1025
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• 2010

This paper describes on methods in test and evaluation of the guided rocket munitions of the domestic new generation multiple launcher rocket system. We modified and refer to the present model of air-to-air missile(AAM) and surface-to-air missile(SAM). Also we suggested a method of surface-to-surface missile(SSM) based on the characteristics of the guided rocket in test and evaluation(T&E). According to this study, the suggested activity of T&E should be observed methods compatible with each item on the established model. Therefore, we expect that the proposed research material will be a good guide to the study of a surface-to-surface missile(SSM) installed GPS/INS integration navigation guidance & control systems in the future.

• 항공우주시스템공학회지
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• 제17권4호
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• pp.75-86
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• 2023

유도무기체계는 기만체계와 함께 창과 방패로 비유되며 발전을 해왔다. 새로운 공격체계가 나타나면 이에 대한 방어체계가 개발되고, 다시 이것을 무력화하기 위한 공격체계가 개발되어 왔다. 이제는 기만체계의 한계로 인해, 유도무기가 공격체계 뿐만 아니라, 방어체계의 주력이 되었다. 또한, 너무빠른 유도무기체계를 방어하기 위한 방법으로 우주공간의 체계를 이용하는 방식으로 확대 되어졌다. 유도무기체계는 아음속 수준에서 시작하여 초음속, 그리고 극초음속으로 발전하여 속도가 유도무기의 한 분야가 되어버릴 정도로 중요한 요소가 되었다. 우주공간이라는 개념이 유도탄전의 범위에 포함이 되었고, 위성체계가 유도탄전의 필수요소가 되어 버렸다. 이러한 유도무기체계와 위성체계와의 상관성을 중심으로 현대 유도탄전의 특징과 유도무기체계의 발전방향에 대해 분석해 보도록 한다.

• 한국군사과학기술학회지
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• 제11권6호
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• pp.21-29
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• 2008

Korean army currently considers the development of the advanced MLRS(Multiple Launcher Rocket System) as a new alternative, which responses on the renovation of the artillery and future battle field environment. Therefore, This study suggests that the development methods of MLRS based on the analysis of the future battle field environment, world wide development trends of the MLRS and operation states of the domestic MLRS. According to this study, the development methods of new generation MLRS should be included a 230/130mm combined launcher competible with conventional 227mm on the vehicle, advanced FCS(Fire Control System), GPS/INS integration navigation system, Pod of ammunitiom, ammunition carrring vehicle and guided rocket munitions, etc.