• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.24 no.2
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• pp.59-64
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• 2024

The small tracking radar randomly changes the transmission period to avoid deceptive signals such as RGPO (Range Gaet Pull Off) operated on the target. Since the code repeats after a specific section, it becomes difficult to avoid a deceptive signal when the repetition is exposed. In this paper, a more realistic transmission pulse code is generated by adding random code generation through FPGA and system white noise. We present the research results of code generation that generates PRF that can avoid repetition while using pseudo-random code in EPROM using FPGA. Also, the result of designing random PRF pulse was confirmed by applying it to tracking radar.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.6
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• pp.445-451
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• 2018

This paper describes on introduction of CASE 4(Delta Wing) for EFD-CFD comparison workshop which is in charged of aerodynamic subcommittee of The Korean Society for Aeronautical and Space Science. The wind tunnel test will be performed later, angle of attack is set -5~20deg and mach number is set 0.7, 0.85, 1.2 to solve the transonic flow. The simulation test of grid dependency is conducted to determine the proper grid size of delta wing analysis. The tendency of lift and drag coefficient is determined according to the change of angle of attack based on the selected grid size.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.3
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• pp.28-39
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• 2018

In this study, numerical simulations were performed for steady and unsteady state characteristics of length effects on linear pintle nozzles using the overset grid method. Nozzles and pintles are created separately by an auto grid generation program to use the overset grid method. Appropriate turbulent models and numerical methods are selected for the validation of simulations. Pintle shapes are chosen from five types, with differences in the ratio of length and diameter. The longer the pintle length, the greater the thrust and thrust coefficient. The chamber pressure tendency of steady-state and unsteady-state are different for various pintle velocities. The thrust of the nozzle exit responds to changes in the nozzle throat in the unsteady-state, and the speed of pressure propagation wave generated by movement of the pintle is considered to predict the major factor of performance.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.2
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• pp.153-160
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• 2019

Electro-mechanical actuator system for aircraft has advantages in compactness and its lightweight, compared to the hydraulic actuator system. Hinge line actuator has low air resistance and is suitable for special purpose such as stealth. This paper describes design contents of 10,000 lbf-in class dual redundant hinge line electro-mechanical actuator system for performance test. The control structure was designed to minimize impact of torque fighting. A mathematical model is proposed to analyze and validate the performances of actuator by comparison with experiment results.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.1
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• pp.33-45
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• 2019

In this study, numerical simulations were performed to investigate the steady-state characteristics of a symmetric pintle nozzle by varying the position of the pintle and the altitude. The pintle nozzle shape was used in a linear pintle nozzle that had been analyzed prior to the study, and the boundary conditions of the chamber were considered to be according to the propellant burn-back characteristics. A software was used to perform a verification analysis of the square nozzle, pintle nozzle, and high-altitude conditions with an appropriate analytical technique. The pintle position had three different nozzle throat area conditions-: fully closed, half open, and fully open, and the altitude was set at 0, 5, and 20 km. The study compared the thrust, pintle drive load, and static stability at each condition.

• Journal of Advanced Navigation Technology
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• v.22 no.2
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• pp.70-75
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• 2018

The mounted store on an aircraft shall be subjected to an ground separation test to verify that a safe separation has been made before it is actually installed to the aircraft. In this study, ground ejection test was conducted with dummy missile to verify the stability of the drop on the land. Bomb rack unit essential to testing ground ejection test, operate at high pressure and produce a significant ejection force to push the missile away from any large orifice. Bomb rack unit modified their bombe pressure and orifice diameter to photograph the drop movement of dummy missile with high-speed camera and to analyze their drop displacement and speed. It is considered useful to provide the initial data for the ejection force analysis on aircraft with actual flight and to carry out the ground separation tests of aircraft with future developments.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.23 no.2
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• pp.51-59
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• 2023

The tracking radar system is installed and operated on the ground, ships, and aircraft, and requires a design to withstand electromagnetic interference with nearby electronic devices. In this case, radiation and immunity standards for cable connection must be satisfied to prevent malfunction of other equipment due to electromagnetic wave interference caused by cables connected to the tracking radar. The radiation standard must also be satisfied so that the electromagnetic wave noise generated and radiated from the tracking radar does not affect the peripheral device, so that the immunity standard for the electromagnetic wave emitted from the peripheral device must be satisfied. In this paper, we propose a design to satisfy MIL-STD-461G including CE, CS, RE, and RS, and explain design satisfaction through tests.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.23 no.2
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• pp.139-147
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• 2023

The compact tracking radar system is a pulsed radar tracking system that searches, detects, and tracks targets in real time against aircraft targets with a small RCS(Radar Cross Section) maneuvering at high speed. This paper describes the development of comprehensive performance test equipment to verify the performance of the radar system in a anechoic chamber environment. Describes the design and manufacture of comprehensive performance test equipment to meet requirements, including the generation of simulated target signals to simulate aircraft target signals to verify performance in the laboratory environment of radar systems. It also describes a GUI(Graphic User Interface) program to check performance through a test in conjunction with the tracking radar system. Verify the comprehensive performance test equipment implemented through the performance test.

• Proceedings of the Korea Contents Association Conference
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• 2014.11a
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• pp.471-472
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• 2014

무기-표적할당(Weapon-Target Allocation: WTA)은 방어 무기체계의 신속하고 정확한 교전결심을 지원하기 위한 핵심적인 기술로서, 다수의 표적이 아군을 위협하는 상황에서 다수의 표적을 효과적으로 요격할 수 있도록 제한적인 무기자산을 효율적으로 할당하는 최적의 해를 찾는 문제이다. 최적의 해에 대한 평가 기준은 무기-표적 쌍들에 대한 요격확률의 합으로 계산된다. 요격확률은 무기가 표적을 요격하는 시점에 따라서 달라지므로, 정밀한 교전결심을 위해서는 요격 시점을 고려하여 무기를 할당하는 것이 중요하다. 특히나 초고속표적을 대응할 때는 표적의 속도가 매우 빨라 요격할 수 있는 시간이 매우 짧기 때문에 더욱 중요하다. 이러한 요구사항에도 불구하고 기존 연구에서는 요격 시점을 고려한 무기할당에 대한 연구가 미진하였다. 본 논문에서는 요격 시점을 고려한 무기할당 알고리즘을 제안하고자 하며 알고리즘에 대한 성능으로 표적에 대한 요격률뿐만 아니라, 표적 출현부터 요격까지의 소요시간인 교전반응시간을 분석하여 신속대응에 대한 성능도 함께 제시한다.

• 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.