• 한국군사과학기술학회지
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• 제26권5호
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• pp.409-421
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• 2023

In the air power, UAVs have played a large and diversified role in performing missions from simple to high-level complex ones. In particular, the suppression of enemy air defenses(SEAD) is very dangerous for a pilot so it is expected that the manned-unmanned teaming(MUM-T) system with tailless stealthy unmanned aerial vehicle(UAV) will greatly enhance effectiveness of the mission while ensuring the pilot safe. This paper describes simulation studies of remote airborne control(RAC) environment for performing the SEAD mission by MUM-T, by which the air force pilot remotely controls tailless UAVs individually or small UAVs in swarm. Through this simulation, air force pilot can derive the concept of MUM-T mission operation with various UAVs in the future, and it can be used to upgrade the MUM-T system by verifying the effectiveness of the mission.

• 한국군사과학기술학회지
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• 제25권1호
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• pp.9-22
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• 2022

A fighter performing a reconnaissance mission is equipped with a pod that drives optical/infrared sensors for acquiring and identifying target information on the lower part of the fuselage. Due to the nature of the reconnaissance mission, the fighter performs high speed evasive maneuvers, and the resulting load should be considered importantly for the development of the pod. This paper concerns a numerical investigation into the inertial and aerodynamic loads of the airborne pod of high performance aircrafts. For the aerodynamic load analysis, the pylon and pod shapes are added to the fighter 3D model, and the commercial software was used for static and dynamic analysis. Considering the practical mission conditions, the common/extreme conditions were established respectively in the static and dynamic situations of pods and the driving torque could be tripled under dynamic conditions. In the analysis of inertia load, a 3-DOF model considering roll and turning maneuvers was derived by the Lagrangian method, and then the numerical integration method was applied to the analysis. As a results, it was conformed that the inertia load was generally induced at a low level compared to the aerodynamic load, but depending on the unbalance mass condition of the pod, the inertia load cannot be negligible.

• 한국국방경영분석학회지
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• 제23권1호
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• pp.1-13
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• 1997

This research investigates a kill probability model for the performance evaluation of guided missile system, and also develops the user interface implementation for the output of the model based on the visual object-oriented programming application. This paper describes in detail the methodology for the kill probability attained by a missile warhead detonating near an airborne target. The major simulation events used in this research are missile guidance homing point, burst points, and kill mechanism(direct kill, blast kill and fragment kill). For the user interface, we also design and implement the visualization system that can show the graphic style of the kill probability attained by the model. This research will bridge the gap between the sophisticated kill probability model and users who want to see the results interactively with visualization, which can benefit many of other military systems. Some examples are shown, but these will be improved to be better with visual simulation which can visualize all the simulation process of the model.

• International Journal of Aeronautical and Space Sciences
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• 제15권3호
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• pp.309-319
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• 2014

This paper mainly focuses on the conceptual design and stealth performance of the three-surface military aircraft. A three-dimensional (3-D) digital mock-up of the three-surface strike fighter with stealth feature was designed and the schemes of carrying missiles were analyzed in CATIA. Based on physical optics principle and the Method of Equivalent Currents (MEC), a numerical simulation of the RCS feature of the aircraft was carried out with RCSPlus which is a software designed by Beihang University. The paper contributes to the RCS feature analysis of the whole plane and different parts on X-band, S-band and UHF-band and a comparison of RCS feature to Su-37 and T-50 military aircraft is drawn. On X-band, the pitch angle of the incident wave was $0^{\circ}$, and the result shows: (1) Compared with Su-37 aircraft, the forward scattering RCS of the three-surface strike aircraft was reduced to 14.9%, the side scattering RCS to 9.6% and the back scattering RCS to 40.2%. (2) Compared with T-50 aircraft, the forward scattering RCS was reduced to 38.61%, and the side scattering RCS to 67.26%. This paper should be useful for researchers in conceptual design and stealth technology of the military aircraft.

• 한국군사과학기술학회지
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• 제15권2호
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• pp.161-168
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• 2012

In this paper, we have experimentally studied on phase characteristics of airborne radome for ELINT directional finding system, because it is difficult to find theoretical solutions for phase error of the radome. Especially, we described the millimeter wave band radome that was fabricated with cyanate-ester material and its thickness was 2mm. We presented the phase error about millimeter band radome. That phase error is about 30 degrees for parallel and perpendicular polarization in the K-Ka band. That is reasonable value for the ELINT directional finding system.

• 한국산학기술학회논문지
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• 제19권8호
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• pp.336-342
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• 2018

군용으로 사용하는 궤도장비 디젤엔진의 보조동력장치에 대한 소음저감은 소요군의 감성품질을 만족시키는 중요한 요소 중 하나이다. 본 연구에서 이러한 보조동력장치의 소음을 줄이기 위해 구조기인소음을 저감하는 방법과 공기기인소음을 저감하는 방법을 고안하여 시험을 수행하였다. 그 결과 구조기인소음 저감을 위해 소음기를 개선하였을 때 약 22 dB(A)의 소음저감 효과가 있었다. 공기기인소음 저감의 영향을 알아보기 위해 흡음재의 종류와 후방문 그릴의 형상에 따른 소음을 측정하였고 그 영향은 인간이 인지하지 못하는 수준인 3 dB(A) 미만의 소음저감 효과가 나타났다. 또한, 실제차량에 소음저감을 위한 방안들을 적용하여 시험한 결과 구조기인소음을 저감하였을 때 약 9 dB(A)의 소음저감 효과가 나타났으며 공기기인소음의 저감효과는 1 dB(A) 이하로 측정된 것을 확인하였다. 따라서 궤도장비의 APU 소음저감을 위해서는 공기기인소음을 저감하는 방법보다 구조물을 통해 전달되는 소음을 저감하는 방안이 효과적이라는 것을 확인하였다. 본 연구결과를 통해 추후 개발하는 타 군용 궤도장비의 소음을 저감하기 위한 기초자료로 사용될 것으로 기대된다.

• 한국통신학회논문지
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• 제42권1호
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• pp.172-180
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• 2017

우리군에서는 지상공간에서의 TICN과 우주공간에서의 차기위성을 연동한 미래전술네트워크 구축을 추진하고 있다. 그러나, 위성의 낮은 대역폭과 높은 운영비용에 의하여, 위성을 통한 모든 전술 정보의 유통에는 한계가 있다. 이를 극복하기 위하여, 공중망을 구축하는 연구가 활발히 진행되고 있다. 본 논문에서는 지상 노드의 단절에 대응하여 공중중계망과 지상전술망을 효과적으로 연동하기 위한 구조와 운영하는 방안을 제안한다. 그리고, 이의 효과도를 분석하기 위한 방안을 함께 제안한다. 효과도 분석 실험 결과는 공중중계망의 운영은 지상전술망의 장애상황에 효과적으로 대처 가능함을 보여준다.

• Journal of Platform Technology
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• 제8권2호
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• pp.32-43
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• 2020

무인 항공기 시스템은 주로 군사용 위주로 운용되어 왔으나, 민간 분야에서도 활발히 이용되고 있다. 민간 분야에서는 주로 저비용의 소형 무인 항공기 시스템을 이용하여 다양한 산업분야에서 이용되고 있다. 이러한 무인 항공기 시스템에서 운용되는 소프트웨어는 공통적인 기능들이 많이 존재한다. 하지만 이러한 특성에도 불구하고 하드웨어 장치가 변경되면 소프트웨어를 수정해야 하는 문제가 발생할 수 있다. 이러한 문제는 무인 항공기 시스템에서 상호 운용성, 모듈성, 이식성을 저하시킨다. 상기 문제들을 해결하기 위해 개방형 시스템 아키텍처가 제안되었으며, 본 논문에서는 다양한 개방형 시스템 아키텍처들 중 FACE(Future Airborne Capability Environment)를 기반으로 동작하는 무인 항공기 시스템 소프트웨어 구조를 제안한다. 본 논문에서 제안하는 소형 무인항공기 시스템은 소량 다품종으로 공급되는 민간 분야에서 다양한 플랫폼의 무인 항공기 시스템을 지원할 수 있으며, 소프트웨어에 대한 통합과 이식성이 뛰어난 장점을 가진다. 마지막으로 본 논문에서는 공개된 개발도구를 기반으로 하는 FACE 기반 무인 항공기 시스템 소프트웨어 개발 방법과 적합성 테스트에 대해 서술한다.

• 한국군사과학기술학회지
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• 제17권5호
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• pp.703-710
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• 2014

An Image-Based Target Tracker maintains LOS(Line Of Sight) to a target by controlling azimuth and elevation gimbals of an ISS(Inertially Stabilized System). Its controller produces the gimbals commands of the ISS using tracking errors provided by an image tracker. The control performance of the target tracker with PI controller generally used for tracking controller is limited because of bandwidth limitation by time delay yielded by image capture and processing of the image tracker. In this paper, tracking controller using target states estimator is proposed which can enhance the tracking performance under the highly dynamic maneuvering conditions of the ISS and the target. Simulation results show that the proposed method can improve the tracking performance than that with only PI controller.

• 한국경영과학회지
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• 제40권2호
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• pp.31-42
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• 2015

The purpose of airborne radars is to detect and identify approaching targets as early as possible. If the targets are identified as enemies, detection systems must provide defense systems with information of the targets to counter. Though many previous studies based on the detection theory of the target have shown various ways to derive detection probability of each radar, optimal arrangement of radars for effective detection, and determination of the search pattern, they did not reflect the fact that most military radar sites run multiple radars in order to increase the accuracy of identifications by radars. In this paper, we propose a model to analyze the probability of identification generated by the multiple radars using non-homogeneous absorbing markov chains. Our results are expected to help the military commanders counter the enemy targets effectively by using radars in a way to maximize the identification rate of targets.