• 한국군사과학기술학회지
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• 제15권4호
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• pp.458-466
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• 2012

We have developed a weapon effectiveness evaluation model for top-attack smart munitions(WEEM/TASM), which is a many on many Monte Carlo Model evaluating the effectiveness of top-attack smart munitions against armoured ground vehicles. In this model the battle is reduced to a one-sided battle situation in that the target vehicles are regarded as being stationary and passive. It can simulate the whole attack process of smart munitions from firing artillery dispenser to sensing and hitting processes after dispense. It can also calculate the probability of kill of each target and the numbers of rounds required to fulfill the degree of damage in statistical manners. In this paper, we describe the basis for our design concepts reflected in the model to simulate the weapon effectiveness of top-attack smart munitions and provide simulation results for an example case.

• 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.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 춘계학술대회논문집
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• pp.191-196
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• 2007

With the development of micro electronic circuits and optical equipment, the demand for developing smart munitions with the ability to autonomously search for and attack targets has increased. Since the electronic components within smart munitions are affected by high temperatures, pressure, and impulsive forces upon the combustion of gunpowder, stability and reliability need to be secured for them. Securing those stability and reliability requires soft recovery system which can decelerate smart munitions. A theoretical analysis of flow is performed for the secure recovery of bullets on the basis of Navier-Stokes equation for compressible fluids. The inner pressure on a pressure tube, the speeds of bullets, and the deceleration of munitions are calculated theoretically. Theoretical results are compared with the data from the experiment with soft recovery system set up at the laboratory.

• 한국소음진동공학회논문집
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• 제17권9호
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• pp.777-784
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• 2007

With the development of micro electronic circuits and optical equipment, the demand for developing smart munitions with the ability to autonomously search for and attack targets has increased. Since the electronic components within smart munitions are affected by high temperatures, pressure, and impulsive forces upon the combustion of gunpowder, stability and reliability need to be secured for them. Securing those stability and reliability requires soft recovery system which can decelerate smart munitions. A theoretical analysis of flow is performed for the secure recovery of bullets on the basis of Euler equation for compressible fluids. The inner pressure on a pressure tube, the speeds of bullets, and the deceleration of munitions are calculated theoretically. Theoretical results are compared with the data from the experiment with soft recovery system set up at the laboratory.

• 시스템엔지니어링학술지
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• 제2권1호
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• pp.42-47
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• 2006

Advanced military nations have developed anti-tank smart munitions to maximize the effectiveness of the tank combat. In this paper we introduced new munition models (KSTAM) for arrack on the top of the tank and analyzed those operation research. To understand the adaptation to the future tank munition we have performed a trade-off study using the proposed models for smart tank munitions which have been developed or are being developed in advanced nations.

• 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.

• 대한기계학회논문집A
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• 제38권3호
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• pp.323-328
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• 2014

정보통신기술과 타 산업분야 기술과의 융복합은 전통적인 제조업을 비롯한 의료, 건설 분야뿐 만이 아니라 국방 분야에서도 그 수요가 점점 증대되고 있어 민 군의 공통적인 기술 수요와 요구사항들이 새롭게 대두되고 있다. 미래 전장환경은 점차 네트워크를 근간으로 하는 NCW(Network Centric Warfare)로 전환될 것으로 예측되고 있다. NCW 는 C4I-ISR-PGM 의 사이클로 이루어지는 적의 탐지부터 타격까지를 의미하는 것이다. 이를 위하여는 정보통신 기술이 근간이 되어야 하며, 실제 전장을 모사할 수 있는 사이버 전장환경이 수반되어야 더욱 더 효과적이다. 본 논문에서는 최근에 연구개발이 본격화하고 있는 스마트 국방 IT 기술 개발 현황 및 향후 전망에 대해 제시하고자 한다.

• 한국군사과학기술학회지
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• 제12권5호
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• pp.615-621
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• 2009

Since GPS receivers and INS algorithms do not work properly in the spinning vehicles due to change of the GPS signal and excess of the measurement limitation of the gyroscope, conventional GPS/INS integrated navigation systems do not provide accurate navigation outputs. This paper proposes a design method for GPS/INS integrated navigation systems of spinning vehicles. A special GPS receiver with a signal tracking loop for changed GPS signal caused by spinning and an INS with a roll estimation method are configured and the conventional integration filter is combined. The proposed method was verified through comparison of the navigation results. The result of the proposed method for the spinning vehicle was similar to that of the conventional navigation system without spinning.

• Journal of Mechanical Science and Technology
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• 제20권11호
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• pp.1961-1971
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• 2006

A soft recovery system (SRS) is a device that stops a high speed projectile without damaging the projectile. The SRS is necessary to verify the shock resistant requirements of microelectronics and electro-optic sensors in smart munitions, where the projectiles experience over 20,000 g acceleration inside the barrel. In this study, a computer code for the performance evaluation of a SRS based on ballistic compression decelerator concept has been developed. It consists of a time accurate compressible one-dimensional Euler code with use of deforming grid and a projectile motion analysis code. The Euler code employs Roe's approximate Riemann solver with a total variation diminishing (TVD) method. A fully implicit dual time stepping method is used to advance the solution in time. In addition, the geometric conservation law (GCL) is applied to predict the solutions accurately on the deforming mesh. The equation of motion for the projectile is solved with the four-stage Runge-Kutta time integration method. A small scale SRS to catch a 20 mm bullet fired at 500 m/s within 1,600 g-limit has been designed with the proposed method.

• 한국항공우주학회지
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• 제39권9호
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• pp.839-847
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• 2011

이 논문에서는 포탄의 정밀도 향상을 위한 새로운 유도기법을 제안한다. 미사일 연구에서 널리 사용되고 있는 비례항법 유도기법은 몇 가지의 문제점 때문에 포탄에 적용하기는 힘들다. 비행 중 발생하는 시선각의 변화 때문에 탄착 오차가 없는 경우에도 가속도 명령을 생성하며, 가속도 명령에 의해 만들어지는 비행경로 또한 포탄에 적용이 불가능하다. 이러한 문제를 해결하기 위해 표적과 포탄의 탄착점 오차를 이용하여 유도 기법을 구성하였다. 기본 구성은 비례항법 유도기법과 유사하지만 시선각 변화 대신 경로 수정각을 사용한다. 경로 수정각은 현재 속도와 표적을 향하는 속도의 사이각이며 탄착점 오차로 추정할 수 있다. 탄착점 예측 속도와 정확도를 높이기 위해 신경회로망을 사용하였으며 비례항법 유도기법 결과와 비교하여 이 유도 기법의 적합성을 검증하였다.