• Convergence Security Journal
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• v.8 no.2
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• pp.87-94
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• 2008

In this paper, a study on the inertial navigation system technology in guided weapon system development. Navigation devices are being used more commonly in places. Inertial navigation devices attached to them are used as weapons systems have a lot of interest in the development of devices for research and development accelerated. Therefore, this paper will encourage the development of weapon systems Inertial navigation device trends, features and configuration, type, techniques for research work.

• Defense and Technology
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• no.3 s.229
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• pp.80-91
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• 1998

오늘날 기동하는 장갑부대 및 기계화부대등 고가의 군사자산 보호는 제5의 위협으로 상정한바 있는 지상공격기(항공기, 유도미사일, 무인항공기 등)의 다양한 공격위협과 교전할 수 있는 전천후 방공능력이 절실히 요구되고 있기 때문에 서방 선진국은 저고도용 지대공 미사일(스팅어, 스타버스트, 미스트랄, RBS-70, 이글라 등)개발과 단일 장갑 차량에 "복합 방공무기체계"를 경쟁적으로 개발 및 운용하고, 중단거리 기동 방공체계를 연구 개발중이다. 특히 고도로 유동적인 장차전의 전장환경에서 적은 최신 무기로 공중침투 공격을 감행할 것으로 예상된다. 따라서 이 글에서는 선진국의 "저고도 대공방어 무기체계"를 고찰하고자 한다.

• Journal of Advanced Navigation Technology
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• v.26 no.6
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• pp.456-463
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• 2022

The SAM(Surface-to-Air Missile) systems will be operated until disposing of it after production, the necessary test and evaluation should be performed during the development stage to ensure the operational performance after deployment. As development of technologies related to the electromagnetic wave field of missile system is required, so the verification of the electromagnetic environment has become more important. Therefore it is necessary to carefully review whether there are any weaknesses through the analysis of the SAM system when establishing the test and evaluation procedure. This paper describes the general electromagnetic test procedure for SAM system and discusses the matters that need to be supplemented. Also, methods for supplementation and review results were written.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.19 no.7
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• pp.1750-1758
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• 2015

This paper provides Bayesian methodology to estimate the reliability for guided weapons which are not continuously operating. The posterior distribution of subsystems and components becomes the next prior distribution. By analyzing the results of the sub-systems and components presented a method for estimating the reliability of the entire guided weapons. Bayesian methodology using existing test data of subsystems may be used to reduce the sample sizes.

• Journal of the Korea Society for Simulation
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• v.19 no.4
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• pp.179-188
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• 2010

The concern of Software Product Line(SPL) engineering is spreading widely because the program or product developers are able to satisfy the customer's demands quickly and give a way to handle maintenance efficiently. SPL is a reuse paradigm that reuse common parts and adopts variable parts optionally to form a differentiated product by analyzing domains. Purposes of this paper are to design an architecture which has a dynamic reconfiguration function and to develop basic components which are the basic unit of reconfiguration to raise the reuse level of the guided weapon system using the SPL. Initially we design an architecture and define basic components for developing a dynamic reconfigurable components based on SPL. Then we develop the composer for physical components and behavior components referenced by behavior models of OneSAF.

• Journal of the military operations research society of Korea
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• v.33 no.2
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• pp.17-29
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• 2007

This work describes a basic process of OMS/MP in guided weapons on board ship. The OMS/MP which provided basic data of ROC & RAM analysis must be prepared by user But data acquisition Quantified by specific operational environment of ship and related preparing instructions which are not established are now insufficient of reliable weapon systems acquisition. The OMS/MP is an important area that become measures of Acceptance Test and doctrine considering future battlespace environment From a development of the OMS/MP template that describe systematically and as quantitative of shipped guided weapons, combat developer oriented product development & reliable weapon system acquisition are ta be accomplished. This research developed OMS/MP preparation templete that presented quantified OMS/MP derivation and RAM target value calculation process which provide optimum weapon systems design concept to research developers

• Journal of the Korea Institute of Military Science and Technology
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• v.22 no.1
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• pp.124-134
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• 2019

As the types of North Korea's provocation are diverse and unexpectable in the costal area, ROK navy needs to develop countermeasures, such as costal defence guided rockets. Recently ROK navy developed the PKX-B which is equipped with the new 130 mm guided rocket. The most popular rockets are LOGIR for short range targets, 130 mm guided rocket for middle range targets and Spike-NLOS for long range targets. As various guided rockets are developed, it is required to develop a guided rocket analysis model and it's analysis methodology. In addition, these guided rockets can be installed on any platforms; ground vehicle, aircraft and warship. The paper proposes systematic methodology to estimate the operational effectiveness of costal defence guided rockets. A case study exploiting the ARENA simulation model is explained to demonstrate the implementation of the proposed methodology.

• Defense and Technology
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• no.5 s.243
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• pp.18-29
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• 1999

$C^4I$ 체계는 나토군의 효과적인 지휘통제로 정보수집/전파, 지휘결심, 타격명령/실시 등의 제반 절차가 실시간에 이루어지게 되므로 반응시간의 단축을 이루었으며, 정밀유도 무기체계의 유고 핵심시설에 대한 집중 타격은 유고의 군사력을 거의 초토화시킨 상태이다. 코소보 사태와 관련하여 나토군이 선보인 첨단 무기체계 및 신기술은 우리의 국방과학기술의 현주소를 깨닫고 시금석으로 삼을 수 있는 좋은 계기임에 틀림없다. 지금 우리는 기술패권주의 시대에 살고 있고, 이러한 시대에 살아남기 위해서 무엇보다 필요한 것은 최첨단 국방과학기술의 개발일 것이다

• Journal of the Korea Society for Simulation
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• v.26 no.1
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• pp.13-19
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• 2017

6-DOF flight simulation program is most generally used M&S tool in domestic missile development procedure. The 6-DOF M&S method, however, cannot validate the performance of a imaging seeker-adopted missile in various conditions. A M&S tool for the analysis of the integrated-flight simulation is required since the tracking performance of the imaging seeker is highly dependent on the missile maneuvering, which introduces the displacement and rotation of the target in the seeker imagery. Through the development of the $3^{rd}$ generation anti-tank missile, Raybolt, the integrated-flight M&S tool was developed and applied to the missile configuration design. It integrates synthetic image generation S/W, imaging tracker, and flight simulation program and computes the main system performance criteria, hit probability by Monte-Carlo Simulation. In this paper, the issues in the $3^{rd}$ generation anti-tank missile configuration and the integrated-flight M&S method and results are described.

• Journal of Aerospace System Engineering
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• v.16 no.5
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• pp.94-101
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• 2022

In this paper, we have obtained the acceleration coefficient of the IMU (Inertial Measurement Unit) to prove reliability by analyzing the characteristic of the MEMS IMU installed in guided weapon systems for overseas export and the operating environment of the guided weapon system. Additionally, based on designed life testing, we performed life tests on three the IMUs and demonstrated a target lifetime of 12 years.