• 융합보안논문지
• /
• 제17권3호
• /
• pp.95-101
• /
• 2017

유도무기체계는 어떤 장비보다도 신뢰성이 가장 중요시 된다. 그러나 제작비용이 고가여서 생산수량이 적고, 배치 후 운용 데이터 획득까지 장기간이 소요되어 주로 개발단계의 신뢰성 예측자료가 활용된다. 개발단계의 신뢰성 예측은 실제 운용환경을 모두 반영하는데 한계가 있어 실제 운용환경에서의 신뢰성 분석이 필요하였다. 본 연구에서는 국내개발 유도무기에 대한 실제 운용 데이터를 활용하여 수명분포를 추정하고, 최소제곱법과 최우추정법을 적용하여 신뢰도 값을 추정하였다. 또한, 개발단계에서 예측된 신뢰도 값과 실제 운용신뢰도 값을 비교하였다. 본 연구 결과로 볼 때 실제 유도무기의 신뢰도는 예측된 값보다 높게 나타났으며, 이는 최신 설계기술의 적용 및 향상된 부품의 신뢰도 값이 예측 데이터에 반영되지 못한 것으로 판단된다. 본 연구를 통해 국내개발 유도무기에 대한 실제 운용 신뢰도를 확인할 수 있었으며, 향후 개발될 유도무기의 신뢰도 분석 연구 활동에 기여 할 것으로 기대된다.

• 한국안전학회지
• /
• 제30권2호
• /
• pp.63-69
• /
• 2015

Recoilless weapons, which lead strong back blast and impulse noise more than 160 dB, have been used in compliance with the regulation of the safety zone for the safe operations. However, the safety zone regulations for the newly developed weapons should be prepared since the existing guidelines do not provide any information concerning the reason for the safety zone. In this study, the outdoor launch tests were performed to collect the data such as noise, pressure and temperature of the back blast. An assessment method using data obtained from launch tests has been proposed to determine the safety zone. The safety zone has been determined with consideration for the following criteria: Impulse noise, temperature and pressure of the back blast and blast angle. As a results, new safety zones for them have been established for the recoilless weapon developed by ADD (Agency for Defense Development). We expect that this research can be used as a guideline for establishing a new safety zone regulation of similar weapon to be developed.

• 한국군사과학기술학회지
• /
• 제24권6호
• /
• pp.638-644
• /
• 2021

Infrared guided weapons act as threats that greatly degrade the survivability of combat aircraft. Infrared weapons detect and track the target aircraft by sensing the infrared signature radiated from the aircraft fuselage. Therefore, in this study, we analyzed the infrared signature and susceptibility of supersonic aircraft according to omni-directional detection angle. Through the numerical analysis, we derived the surface temperature distribution of fuselage and omni-directional infrared signature. Then, we calculated the detection range according to detection angle in consideration of IR sensor's parameters. Using in-house code, the lethal range was calculated by considering the relative velocity between aircraft and IR missile. As a result, the elevational susceptibility is larger than the azimuthal susceptibility, and it means that the aircraft can be attacked in wider area at the elevational situation.

• 한국군사과학기술학회지
• /
• 제22권6호
• /
• pp.745-753
• /
• 2019

Recently, with the development of long-range / high-altitude guided weapon system for defense against ballistic missile, test range and firing altitude for guided weapons are increasing. Due to the increase in the test range and the intercepting altitude, it is expected to increase the range of safety area required for the firing test. Comparing to the foreign countries which have many desert or non-residence, in the domestic circumstances where the population is concentrated and distributed, it is more important to predict the falling area and to set the safety area for safely carry out the long-range / high-altitude intercept test. In this paper, we consider the following three points. The first is the booster fall trajectory modeling, the second is the shroud fall trajectory modeling, and finally, the debris dispersion modeling for the missile intercept. Especially, the AUTODYN model was used to predict debris falling area which produced in the high-speed guided missile intercepting test.

• 한국항공우주학회지
• /
• 제37권10호
• /
• pp.1010-1016
• /
• 2009

본 본문에서는 항공기 탑재비행시험을 통한 무기체계 개발시험에 대하여 기술하였다. 국방과학연구소에서는 항공기를 운용하며, 각종 항공/유도 무기체계의 핵심 탑재장비와 센서 개발을 위하여 항공기 탑재비행시험을 수행하고 있다. 탑재비행시험 플랫폼으로는 KTX-1/XKO-1 항공기를 사용하며, 외부연료탱크 형상의 탑재시험체를 제작하여 시스템 연동을 위해 항공기를 수정하였다. 항공기 탑재비행시험을 통하여 각종 탐색기와 항법시스템 그리고 유도무기 핵심 탑재장비에 대한 개발시험을 수행하였다.

• 한국군사과학기술학회지
• /
• 제27권2호
• /
• pp.213-221
• /
• 2024

Aircraft's operational effectiveness is reduced due to threats from enemy anti-aircraft weapons, which is a weak point. In particular, guided missiles, which pose a threat to aircraft, are rapidly developing due to technological advancements in seekers, and are classified as one of the important technologies in weapon systems. Missile approach warning equipment installed to ensure aircraft survivability detects guided missiles and provides relevant information to respond. Tests were conducted domestically to verify the detection level of missile approach warning equipment, and test results were presented under various test conditions.

• 한국군사과학기술학회지
• /
• 제21권5호
• /
• pp.649-657
• /
• 2018

It is essential that weapons which are mounted on aircraft need to prove its reliability and safety during its developments. A guided missile should have high reliability and safety throughout various tests which are including ground tests, captive flight tests, detailed technical tests and operational tests. In these various tests, it is vital that software of each component in the guided missile should be easily updated in order to correct algorithms or errors. In this paper, we propose a software update technique based on MDTP(mass data transfer protocol) which are defined in MIL-STD-1760. The proposed techniques have the following advantages: First, software of each unit in a weapon can be updated through a test equipment without disassemble a guided missile. Second, development periods for a software update can be reduced by reusing MDTP. Third, we can easily maintenance of the software because it is based on standard. We proved its efficiency and validity through experiments. Therefore, the proposed technique should be effectively utilized for software update of a weapon mounted on an aircraft during development processes.

• 한국군사과학기술학회지
• /
• 제24권1호
• /
• pp.133-143
• /
• 2021

In government procurement programs, cost estimation and analysis support funding decisions and are the basis for other major decisions, too. Such estimating and analyzing the cost of the weapon systems are crucial in execution of the defense budget. However, existing cost estimations and analyses have focused on domestic R&D projects, thus those are not valid in application to foreign weapon acquisitions. This study aims at foreign weapon systems that are acquired from Direct Commercial Sales. Because the data for price estimation of a foreign weapon is usually not available, we suggest a price estimation model based on performance factors of the weapon. In this study, the proper price of the weapon system is estimated using the parametric cost estimating model. Using the data of helicopter-launched anti-tank guided missiles worldwide, we analyze the effect of each performance factor on the weapon system price by regression analysis, and use step-wise and ridge regression analysis to remove multi-collinearity. This study hopefully contributes to more reasonable decision making on proper price of weapons.

• 한국항해항만학회지
• /
• 제34권2호
• /
• pp.97-103
• /
• 2010

It has been recognized that the risk from the vulnerability of GPS can lead to the extreme damage in the infrastructure of the civil and military in recent years. As an example, the intentional interference to GPS signal, named GPS jamming, was really performed to misguide GPS guided weapons during Iraq war in 2003, and the fact has also followed by the serious issues on GPS in civilian community. In the modernized military society, the navigation warfare(NAVWAR) based on the GPS jamming has been emerged and introduced as a military operation. The intentional interference to the future global navigation satellite system(GNSS) involving GPS must be also an important issue to civilian users in near future. This study is focused on the fundamental research prior to the research on "Potential principle of NAVWAR" under NAVWAR of the future warfare. In this paper, we would study on the investigation of NAVWAR based on electronic warfare(EW) and analyze characteristics of the jamming against GNSS's receivers. Then the general mechanism on GNSS jamming is proposed.

• 융합보안논문지
• /
• 제8권2호
• /
• pp.87-94
• /
• 2008

본 논문에서는 유도무기체계의 관성항법장치 기술에 대한 사항과 발전추세에 대해 연구하였다. 항법장치는 여러 곳에 일반적으로 많이 사용되고 있다. 그중 관성항법장치는 무기체계에 부착되어 사용됨에 따라 많은 관심들을 가지고 장치의 개발과 발전을 위한 연구가 가속화되고 있다. 따라서 본 논문에서는 유도무기체계 관성항법장치의 개발동향, 기능 및 구성, 종류, 작동기술에 대해 연구하였다.