• Proceedings of the Korean Institute of Communication Sciences Conference
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• 1988.10a
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• pp.195-198
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• 1988

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.2
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• pp.181-190
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• 2014

The optimized flight path planning which is appropriate for UAV operation with high performance and multiplex sensors is required for efficient ISR missions. Furthermore, a mission visualization tool is necessary for the assessment of MoE(Measures of Effectiveness) prior to mission operation and the urgent tactical decision in peace time and wartime. A mission visualization and analysis tool was developed by combining STK and MATLAB, whose tool was used for UAV ISR mission analyses in this study. In this mission analysis tool, obstacle avoidance and FoM(Figure of Merit) analysis algorithms were applied to enable the optimized mission planning.

• Journal of the Korea Society for Simulation
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• v.23 no.4
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• pp.75-83
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• 2014

Most warship combat systems inquire human operator to control several sensor and another equipments as well as decision-modeling. For this reason, many researches with multi-agent based M&S (Modeling and Simulation) have been increasingly conducted. However there cannot find any researches of M&S based analysis for anti-submarine warfare that requires a high level of mission complexity between multiple platforms. In this research, we have been developed various combat platform models such as warship, submarine and helicopter, etc. In order to apply the multi-agent-based M&S technology to the anti-submarine warfare i.e. a HVU (High Value Unit) escort mission scenario. Then we have successfully analyzed the measures of effectiveness according to the different tactics and different situations. In future, the defence engineer maybe employ our methodology and tools to analyze actual tactical problem by simply inserting actual data into our agent model.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.9
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• pp.836-842
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• 2007

This paper describes the development of an automated operational orbit processing system (KGS automated Operational Orbit Processing System, KOOPS), which can determine, evaluate, update, and generate the orbit data automatically. Developed system can be applied to the multi satellite mission operations as a generic satellite orbit processing system in that the KOOPS has a capability to process various kinds of tracking data and assign pre and post processes according to the satellite system respectively. Results of applying the KOOPS to the KOMPSAT-1 and KOMPSAT-2 mission operations show that man power is greatly reduced and the efficiency and stability of the mission operations are significantly increased. The experiences to develop the KOOPS and operate multi satellite missions using this system can be applied to enhance the multi and generic flight dynamics system further.

• 한국항공운항학회:학술대회논문집
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• 2015.11a
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• pp.1-5
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• 2015

캔위성은 대기권 내에서 낙하하며 실제 위성을 모사하는 초소형위성으로 저렴한 비용과 용이한 접근성으로 인공위성 시스템 교육과 실험 등에 있어서 많은 주목을 받고 있다. 이러한 점을 착안하여 Argos는 촬영위성과 통신위성 2기로 구성된 캔위성 시스템을 개발하였다. Argos는 해당지역의 영상을 수집하고 위성 간 통신을 하는 것을 주 임무로 하였다. 또한 자세데이터, 위치데이터, 온도, 압력을 수집하고 지상국으로 전송 하는 것을 부 임무로 하였다. Argos는 실제 발사된 이후 제한적인 임무를 수행하였고, 위성간의 통신으로 임무데이터를 지상국으로 전송하였다. 본 논문에서는 광범위 데이터 수집의 역할을 하는 Argos의 개발과정과 운용결과를 소개하고자 한다.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2022.06a
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• pp.140-142
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• 2022

최근 신경망 기반 기술들의 발달에 따라, 신경망 기술들은 충분히 높은 임무 수행 성능을 달성하고 있으며 사물인터넷, 스마트시티, 자율주행 등 다양한 환경을 고려한 응용 역시 활발히 연구되고 있다. 하지만 이러한 신경망의 임무 다양성과 복잡성은 더욱 많은 비디오 데이터가 요구되며 대역폭이 제한된 환경을 고려한 응용에서 이러한 비디오 데이터를 효과적으로 전송할 방법이 필요하다. 이에 따라 국제 표준화 단체인 MPEG 에서는 신경망 기계 소비에 적합한 비디오 부호화 표준 개발을 위해 Video Coding for Machines (VCM) 표준화를 진행하고 있다. 본 논문에서는 신경망의 특징 부호화 효율을 개선하기 위하여 VCM 을 위한 다중 스케일 특징 압축 방법을 제안한다. COCO2017 데이터셋의 검증 영상을 기반으로 제안방법을 평가한 결과, 압축된 특징의 크기는 원본 이미지의 0.03 배이며 6.8% 미만의 임무 정확도 손실을 보였다.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2022.11a
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• pp.76-78
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• 2022

기계 소비(machine consumption)를 대상으로 하는 이미지 및 비디오의 압축 목표는 사람이 소비하는 것과 다를 수 있다. 예를 들어, 인간의 소비에는 이미지 및 비디오의 전체 캡처 영역이 필요하지만, 기계는 응용 프로그램에서 요구하는 이미지 또는 비디오의 일부만 사용할 수 있다. 이 논문에서는, 효과적인 기계 소비를 위한 영상 압축 방법 개발을 통한 다중 임무(task) 수행 성능 개선 및 압축률(bpp) 향상을 목적으로, 관심 객체(object of interest) 또는 관심 영역(region of interest)을 식별하기 위한 신경망 기반 영상 분석 작업을 수행하는 전처리 네트워크 구성 방법을 제안한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.5
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• pp.361-367
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• 2014

In this paper, task scheduling and load balancing methods of multifrontal solution methods of finite element structural analysis in a modern multicore machine are introduced. Many structural analysis problems have generally irregular grid and many kinds of properties and materials. These irregularities and heterogeneities lead to bottleneck of parallelization and cause idle time to analysis. Therefore, task scheduling and load balancing are desired to reduce inefficiency. Several kinds of multithreaded parallelization methods are presented and comparison between static and dynamic task scheduling are shown. To reduce the idle time caused by irregular partitioned subdomains, computational load balancing methods, Balancing all tasks and minmax task pairing balancing, are invented. Theoretical and actual elapsed time are shown and the reason of their performance gap are discussed.

• The Journal of the Convergence on Culture Technology
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• v.10 no.4
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• pp.757-761
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• 2024

The need to acquire a multi-mission modular ship to carry out the mosaic warfare of modern warfare is increasing. In such a modular ship, not only domestic R&D equipment/systems but also an manned/unmanned complex system purchased overseas must be mounted together. In order to successfully design/construction a multi-mission modular prototype battle ship and turn it into timely power, it is necessary to apply a new technology so that it can be installed flexibly in a limited space and time. However, the existing welding installation method not only limits flexibility in design/construction due to safety problems, but also has an inherent problem that the cost and time required to correct defects and supplements are excessive. Therefore, this study introduces the current status of next-generation installation devices developed/applied in the advanced navy and the field demonstration results applied to battle ships to provide flexibility in this respect.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.8
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• pp.50-57
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• 2003

Controlling rotorcraft to fly precisely through multiple, irregularly, and closely spaced waypoints is a common and practical mission. However, finding an optimal trajectory for this kind of mission is quite challenging. Usability of traditional approaches such as inverse control or direct methods to this kind of problem is limited because of either limitation on the specification of the constraints or requirement of extensive computation time. This paper proposes a method that can easily compute the full trajectory and control history for rotorcraft to pass through waypoints while satisfying other general constraints of states such as velocities and attitudes on each waypoint. The proposed method is applied to rotorcraft guidance problems of slalom and linear trajectory in the middle of general curved trajectory. The algorithm is test for various situations and demonstrates its usability.