• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.11
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• pp.911-920
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• 2018

In this study, we performed a study to track the angle between the guided weapon and the target by using the strap-down image seeker, and constructed a test bed that can simulate it visually. This paper describes a method to maintain high-performance feature distribution in the implementation of sparse feature tracking algorithm such as Lucas Kanade's optical flow algorithm for target tracking using image information. We have extended the feature tracking problem to the concept of feature management. To realize this, we constructed visual environment using Unity3D engine and developed image processing simulation using OpenCV. For the co-simulation, dynamic system modeling was performed with Matlab Simulink, the visual environment using Unity3D was constructed, and computer vision work using OpenCV was performed.

• The KIPS Transactions:PartD
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• v.12D no.3 s.99
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• pp.481-492
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• 2005

To guide the guiding robot for the visually impaired carefully, the digital map to be used to search a path must be detailed and has some information about dangerous spots. It also has to search not only safe but also short path through the position data by GPS and INS sensors. In this paper, as the difference of the ability that the visually unpaired can recognize, we have developed the localization tracking system so that it can make a movement path and verify position information, and the global navigation system for the visually impaired using the GPS and INS. This system can be used when the visually impaired move short path relatively. We had also verified that the system was able to correct the position as the assistant navigation system of the GPS on the outside.

• Journal of the Korea Society for Simulation
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• v.26 no.1
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• pp.13-19
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• 2017

6-DOF flight simulation program is most generally used M&S tool in domestic missile development procedure. The 6-DOF M&S method, however, cannot validate the performance of a imaging seeker-adopted missile in various conditions. A M&S tool for the analysis of the integrated-flight simulation is required since the tracking performance of the imaging seeker is highly dependent on the missile maneuvering, which introduces the displacement and rotation of the target in the seeker imagery. Through the development of the $3^{rd}$ generation anti-tank missile, Raybolt, the integrated-flight M&S tool was developed and applied to the missile configuration design. It integrates synthetic image generation S/W, imaging tracker, and flight simulation program and computes the main system performance criteria, hit probability by Monte-Carlo Simulation. In this paper, the issues in the $3^{rd}$ generation anti-tank missile configuration and the integrated-flight M&S method and results are described.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.15 no.4 s.97
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• pp.382-387
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• 2005

For successful guided-wave damage inspection, the appropriate signal processing of measured wave signals is very important. The objective of this paper is to introduce an efficient signal processing technique especially suitable for the guided-waves used for damage detection. The key idea of this technique is to model guided-waves by chirp functions of special form considering the dispersion phenomenon. To determine the parameter of the chirp functions simulating guided-waves, the matching pursuit algorithm is employed. The damage information in waveguides can be extracted by pulse-characterizing parameters. The effectiveness of present method is checked with the guided wave-based damage inspection.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2004.11a
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• pp.615-618
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• 2004

For successful guided-wave damage inspection, the appropriate signal processing of measured wave signals is very important. The objective of this paper is to introduce an efficient signal processing technique especially suitable for the guided-waves used for damage detection. The key idea of this technique is to model guided-waves by chirp functions of special form considering the dispersion phenomenon. To determine the parameter of the chirp functions simulating guided-waves, the matching pursuit algorithm is employed. The damage information in waveguides can be extracted by pulse-characterizing parameters. The effectiveness of present method is checked with the longitudinal wave-based damage inspection.

• Defense and Technology
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• no.12 s.178
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• pp.28-37
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• 1993

적의 어뢰공격을 받을 때 기만기로 방어하는 것은 대단히 유효한 수단이며, 최신 기만시스템은 어뢰의 유도장치에 대응하는 여러가지 기능을 구비하여 함정과 유사한 신호를 발생시켜 어뢰를 함정으로부터 다른 방향으로 유도해서 추적을 차단시킵니다.

• The Bulletin of The Korean Astronomical Society
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• v.35 no.1
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• pp.37.2-37.2
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• 2010

한국천문연구원에서는 이동형 레이저위성추적(SLR) 시스템을 개발하고 있다. 이동형 레이저위성추적 시스템의 광학부는 송신광학계, 수신광학계, 광신호유도계로 구성되어 있으며, 주야간에 운영되는 시스템의 특성상 광신호유도계는 특별한 구성과 기능을 갖는다. 본 연구에서는 주야간 위성추적을 위해 요구되는 광신호유도계의 구성과 기능을 소개하며, 또한 광신호유도 광학계의 광학설계에 대해서도 논한다.

• The Journal of the Acoustical Society of Korea
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• v.12 no.3
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• pp.34-42
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• 1993

수중운동 추적체계의 추적 성능은 표적에 부착된 핑거로부터의송신음향이 수중센서에 도달하기 까지의 시지연과, 해저에 부설된 각 센서가 시지연을 이용하여 기하학적으로 계산하는 LOP를 얼마나 정확하게 추출하느냐에 달려있다. 본 논문에ㅓ는 수중운동 추출하느냐에 달려있다. 본 논문에서는 수중운동 추적체계의 추적성능을 예측하기 위하여 먼저 CRLB를 이용한 시지연 예측오차의 기준경계식을 유도하고, 임의 표적운도에 이를 적용시켜 추적거리오차를 추출하였다. 시뮬레이션 결과, 표적이 원형 기동하는 경우보다 직선 기동하는 경우에 표적위치에 따라 오차의변화가 더 심하고, 수중운동 추적체계의 이론적 설계성능은 주파수 대역에 의해 영향을 가장 많이 받음을 확인하였다. 한편 4km*4km 범위의 수중센서 패턴을 사용하고 주파수 대역폭을 200Hz로 취한 경우 시간지연에 의한 수중운동 추적체계의 이론적 추적오차는 0.24m 이내로 시뮬레이션 되었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.3
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• pp.199-212
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• 2014

This paper describes an autonomous air combat guidance law using a Virtual Pursuit Point (VPP) in one-on-one close engagement for Unmanned Combat Aerial Vehicle (UCAV). The VPPs that consist of virtual lag and lead points are introduced to carry out tactical combat maneuvers. The VPPs are generated based on fighter's aerodynamic performance and Basic Fighter Maneuver (BFM)'s turn circle, total energy and weapon characteristics. The UCAV determines a single VPP and executes pursuit maneuvers based on a smoothing function which evaluates probabilities of the pursuit types for switching maneuvers with given combat states. The proposed law is demonstrated by high-fidelity real-time combat simulation using commercial fighter model and X-Plane simulator.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.24 no.8B
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• pp.1593-1600
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• 1999

This paper describes the acquisition modeling of an airborne target for target tracking simulation of infrared homing missiles. The modeling, of which key technologies are the sub-modeling for target infrared signature, atmospheric transmission, and receiver characteristics, shows the acquisition process of an airborne target under various tracking conditions determined by line-of-sight, distance, and atmospheric conditions. We confirm the validity of the modeling by applying it to simulations concerned with target tracking. The modeling gives a guideline to determine an optimum detector and a defection band for effective discrimination of the target among false targets.