• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.7
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• pp.590-600
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• 2012

In this research, generalized sizing methods were studied that can be applied to an aircraft which uses solar cell or fuel cell as energy sources. To consider multiple propulsion systems and energy resources, multiple power paths were modeled and the weight of consumable and non-consumable energy was reflected in the weight change calculation for each mission segments. In the constraint analysis, power to weight ratio was selected instead of thrust to weight ratio and used in the sizing process of balancing power and energy.

• Proceedings of the Korea Inteligent Information System Society Conference
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• 2007.11a
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• pp.499-506
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• 2007

전장환경에서 헬기는 헬기생존체계의 다양한 센서를 통하여 수집한 데이터를 기반으로 헬기에 대한 위협을 식별한다. 헬기의 성공적인 임무 수행 및 생존을 위하여 헬기에 대한 위협을 반복적으로 확인할 수 있는 시뮬레이터의 구현은 필수적이다. 본 논문에서는 (1) 헬기의 센서가 수신하는 위협요소를 정의하는 온톨로지 생성기, (2) 전장환경과 유사한 위협을 다양한 분포로 생성하는 위협자료 생성기 및 (3) 다양한 전장 시나리오에서 센서들이 수집한 데이터를 통합하여 위협의 방향과 정도를 사용자에게 실시간으로 보여주는 그래픽 표시기를 개발한다. 구현한 헬기의 다중센서 위협 시뮬레이터를 이용하여 다양한 위협에 대한 탐지 및 분류 정확도를 측정한다.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.7 no.1
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• pp.158-163
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• 2003

When the number of disks array systems that contain multiple disk drives, system performance is limited by a bottleneck at a centralized controller at a communication path than uses a bus. A redundant array of inexpensive disks(RAID) consists of many disks to enable high performance and large capacity. We evaluate a scalable architecture called Autonomous network, in which the controller functions are distributed to all disk drives and each disk has autonomy in processing its tasks. Disks drives enable better scalability and more effective utilization of system resources than with a hierarchical system. Autonomous network provided high read/write performance throughput in proportion to the number of disks.

• Aerospace Engineering and Technology
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• v.7 no.2
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• pp.95-102
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• 2008

COMS Satellite is automatically able to recover from any defined failure thanks to a full redundancy. This study assesses the effects of gyro failure on the COMS mission and analyzes the mechanism of Gyro Failure Detection, Isolation and Recovery about failure detection means, isolation and recovery actions and their consequences. At last, it checks the FDIR behavior from an injected failure on COMS simulator.

• Journal of Ocean Engineering and Technology
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• v.11 no.3
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• pp.180-190
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• 1997

잠수함이 저심도 조건에서 특수임무 수행시, 표면파도 및 조류등 외란의 영향하에서 요구심도 및 위치 유지를 위한 강인한 자동항법장치 설계는, 첨단 군용 잠수함 개발에 필수적이다. 본 연구는 잠수함 조종 운동역학계에 기초하여, 정확한 심도 및 피치 운동 제어를 위해 선형 행렬 부등식을 이용한 혼합 $H_2/H_{\infty}$ 설계법을 사용, 다중 목적 함수로 표현된 잠수함의 조종성능들을 개선하였다. 또한, 제어기 설계법의 타당성을 수치 시뮬레이션을 통하여 검증하였다. 결과적으로 본 제어법은 각종 외란 및 계의 불확실성하에서 잠수정의 만족스러운 과도 상태 응답과 일정 심도 유지 및 피치 각도 변동 최소화에 적합한 강인한 방법임이 검증되었다.

• Proceedings of the Korea Information Processing Society Conference
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• 2018.05a
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• pp.78-79
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• 2018

이중화 시스템은 가용성 및 신뢰성 향상을 위한 방안의 하나로 시스템의 고장으로 인한 임무중지나 성능 감소를 방지하기 위한 시스템이다. 이중화 구조 중 하나인 마스터-슬레이브 구조를 갖는 시스템에서는 슬레이브 모듈이 마스터 모듈의 상태를 모니터링하고 있다가 이상 감지 시 슬레이브 모듈에서 마스터 모듈로 전환되는 기능을 가지고 있다. 본 논문에서는 네트워크 시스템 구성 시 항시 시스템 fail 를 감지하고 무중단 데이터 전송을 수행하기 위한 네트워크 이중화 구성 방안에 대해 소개 한다.

• Journal of Korea Society of Industrial Information Systems
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• v.22 no.5
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• pp.39-49
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• 2017

A Space Launch Vehicle (SLV) for Launching Satellites Consists of Multi-stage Rockets for the Purpose of Efficient Flight and Accomplishes the Launch Mission through Flight Events such as Stage Separation, Engine Start and Stop. In this Process, the SLV is Supposed to Undergo the Processes of the Powered Flight Section in which the Engine Generates Thrust and the Ballistic Flight Section in which there is no Thrust Repeatedly. Because it is Difficult to Express these Flight Characteristics of the SLV as a Single Dynamics Model, much Research on Tracking Algorithms using Multiple Models has been Undertaken. In case of using the Multiple Model Tracking Algorithm, it is Expected to Improve the Tracking Performance of the SLV. However, it is Difficult to Select Proper Dynamics Models to be used and the Calculation Amount Increases due to the use of Multiple Models. In this Paper, we Propose a Method to Track the SLV with Diverse Flight Characteristics Efficiently by only Two Kalman Filters using Constant Acceleration Model and Adaptive Singer Model.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.11
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• pp.963-971
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• 2012

In this paper, development of optimal design tools for wing structure is described including multi load spectra condition and fatigue analysis. Two dimensional CFD result are used for calculating aerodynamic force. Design variables are composed of a number of rib and spar, positions, and thickness of each structural member. The mission profile for fatigue analysis is composed based upon the results of CFD analysis, the flight-by-flight spectra method, the excessive curves for gust loads. Minor's rule was used to deal with multi-load condition. Stress analysis and fatigue analysis are performed to calculate objective functions. Particle Swarm Optimization(PSO) algorithm was used to apply to problems which have dozens of design variables.

• The Journal of the Korea Contents Association
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• v.5 no.5
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• pp.1-9
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• 2005

In this paper, we suggest multi colony interaction ant reinforcement learning model. This method is a hybrid of multi colony interaction by elite strategy and reinforcement teaming applying Temporal Difference(TD) learning to Ant-Q loaming. Proposed model is consisted of some independent AS colonies, and interaction achieves search according to elite strategy(Intensification, Diversification strategy) between the colonies. Intensification strategy enables to select of good path to use heuristic information of other agent colony. This makes to select the high frequency of the visit of a edge by agents through positive interaction of between the colonies. Diversification strategy makes to escape selection of the high frequency of the visit of a edge by agents achieve negative interaction by search information of other agent colony. Through this strategies, we could know that proposed reinforcement loaming method converges faster to optimal solution than original ACS and Ant-Q.

• Journal of the Korea Society for Simulation
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• v.20 no.3
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• pp.101-109
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• 2011

M&S in the field of national defense is a battle system has been highly spotlighted for obtaining weapon systems, analyzing and experimentation of battle effects to reduce costs, time, and risks. It is classified as Campaign, Mission, Engagement, and Engineering levels by detail of description. In engagements, many situations on the battle field which are really unpredictable are required to be considered on the view of diverse tactics. Thus, engagement simulation is in demand to use for forecasting real-world battle situations by inserting various components which consists of real engaging situations into virtual local battle field. While developing the engagement simulation, adopting the concept of agent-based simulation gives it benefits which are improved autonomy, composability, and reusability of entities. It means reducing the time, cost and effort to develop the simulations. This paper concentrates on the framework of multi-agent based engagement simulation using Cougaar Architecture.