• Journal of the Korea Institute of Information and Communication Engineering
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• v.23 no.4
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• pp.365-373
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• 2019

An Image Infra-Red(IIR) seeker is widely used for precision guided munitions to provide intelligent and precise target detection in terms of high kill probability. However, there have been issues in determining the performance versus cost trade-offs due to high cost of seeker comparing to other units of the munitions. In this paper, performance/cost evaluations have been carried out to find the most cost-effective solution for developing the IIR seekers. The relationships between the critical parameters and cost are investigated to determine the optimal point which represents the low cost with high performance. It is expected that the presented approach will be able to be used for guidelines to select the appropriate IIR seeker for the given operating conditions and can be useful to estimate the cost effectiveness of the precision guided munitions at early design stage.

• Journal of Aerospace System Engineering
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• v.18 no.4
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• pp.1-9
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• 2024

In this study, we researched control compensation techniques to enhance control robustness against external forces and responsiveness to output dead zones in direct-actuated voice coil actuators for small guided missiles. An aircraft's wings must optimally control the command angle while managing various nonlinear external forces such as drag, lift, and thrust during flight. The small direct -drive voice coil actuator, when applied, benefits from small current requirements in no-load situations but suffers from diminished control robustness due to rapid increases in control current during external force applications. To address this issue, we designed and implemented a system that compensates for errors by accumulating additional output, thus improving the actuator's responsiveness in control scenarios with external forces. This was verified through experimental results.

• International Journal of Aeronautical and Space Sciences
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• v.18 no.4
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• pp.697-708
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• 2017

The complex battlefield environment makes it difficult to intercept maneuvering targets for guided missiles. In this paper, a finite-time convergent (FTC) guidance law based on the second-order sliding mode (SOSM) control theory is proposed to achieve the requirements of stability, accuracy and robustness. More specifically, a second-order sliding mode observer (SMOB) is used to estimate and compensate for the total disturbance of the controlled system, while the target acceleration is extracted from the line-of-sight (LOS) angle measurement. The proposed guidance law can drive the LOS angular rate converge to zero in a finite time, which means that the missile will accurately intercept the target. Numerical simulations with some comparisons are performed to demonstrate the superiority of the proposed guidance law.

• Journal of the Korean Society of Systems Engineering
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• v.7 no.1
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• pp.23-30
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• 2011

본 논문은 대형복합 시스템인 국방 유도무기체계를 MBSE(Model Based Systems Engineering) 방법론에 적용한 사례 연구에 대하여 다룬다. MBSE 방법론 적용을 위해 시스템 엔지니어링 설계 프로세스를 적용한다. 이를 통해 MBSE 방법론 적용의 유용성을 공유하고, MBSE 적용 지침으로 활용될 수 있도록 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.375-378
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• 2011

A valve's high response for controlling thruster is essential for rapid turning during initial short moment after launching. The actuator for controlling the valve is simultaneously used in controlling canard of a guided missile. This paper explain development process for the electromechanical actuator interlocked with canard by arranging in following order, design, analysis, manufacture, test and evaluation.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.364-367
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• 2011

The development of the DCS thrust unit during the attitude control thruster of the launch vehicle and guided missile is introduced. The DCS thrust unit using solid propellants based on a two-axis control is designed and through the thermo-structural and flow analysis is designed in detail. The performance of the thrust unit based on the detail design is demonstrated through a combustion test.

• 제어로봇시스템학회:학술대회논문집
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• 1988.10a
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• pp.597-602
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• 1988

In this paper, we consider conventional and modified proportional navigation guidance(PNG) laws for a random maneuvering target. By means of Lyapunov function approach, we show that an ideal missile guided by the conventional PNG law can always intercept a random maneuvering target if some specified initial conditions are satisfied and the navigation constant is chosen sufficiently high. In addition, we propose a modified PNG law. At the final phase of pursuit, the proposed guidance law has a better acceleration profile than the conventional PNG law.

• Journal of the Korean Society of Propulsion Engineers
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• v.5 no.3
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• pp.52-59
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• 2001

In this study, a technique has been developed to analyze the performance of the launching system using a gas generator of solid propellant. The physical model which described the thermodynamic behaviors of all launching devices from gas generator to canister and the dynamic behavior of missile was established, applying the empirical coefficients in the heat loss model. The processes of combustion, flow, and heat transfer inside the chamber of gas generator and the launching system were simulated by numerical method. The theoretical analysis guided the optimal design of gas generator and system, which made the launching system satisfy the requirements of good performance and high reliability.

• Journal of the Korea Institute of Military Science and Technology
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• v.15 no.4
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• pp.390-397
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• 2012

According to sailing condition, an exciting force for luminairie of naval vessels was measured and analyzed. A naval combat service support boat and P${\bigcirc}{\bigcirc}$(patrol killer guided missile) were selected as a target naval vessel. Due to their small size and fast speed, they received excessive vibration than other bigger naval vessels like destroyer. The vibration of luminairie was measured on their cruising and maximum speed. This could analyze exciting force for luminairie of naval vessels. Using this analyzed data, the validity of military standard for naval vessel was verified.

• Review of KIISC
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• v.12 no.6
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• pp.41-53
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• 2002

선진/주변국에서는 C4ISR/PGM(Command, Control, Communication, Computer, Intelligence, Surveillance and Reconnaissance/Precision Guided Missile)체계를 미래전의 핵심으로 인식하여 막대한 예산을 투입, 체계를 구축하고 체계의 극대화를 위해서 상호운영성, 표준화 등에 관심을 경주하고 있다. 그러나 이러한 모든 체계는 네트워크로 연결됨에 따라 미래 전의 신종 위협으로 등장한 컴퓨터 바이러스, 웜(worm), 트로이 목마(Trojan Horse), 논리폭탄(Logic bombs), 트랩도어(Trap doors), 칩핑(chipping), 나노 머신으로 분류되는 초소형로봇, EMP/HPM(Electro Magnetic Pulse/High Powered Microwave)등에 대한 취약점을 지니게 되며 이에 대한 대비책도 강구하고 있다. 본 연구에서는 미래 디지털 전쟁의 핵심인 C4ISR/PGM복합체계를 소개하고, 미래전의 특성 및 C4ISR와 PGM체계의 역할에 대해 소개하며, 특히 비대칭 전력으로 선진/주변국에서 강력하게 추진하고 있는 사이버전 현황 및 발전 추세를 제시하고, 정보전의 한계와 문제점도 제시한다.