• 제목/요약/키워드: Ground-test simulation

검색결과 337건 처리시간 0.029초

Ungrounded System Fault Section Detection Method by Comparison of Phase Angle of Zero-Sequence Current

  • Yang, Xia;Choi, Myeon-Song;Lee, Seung-Jae;Lim, Il-Hyung;Lim, Seong-Il
    • Journal of Electrical Engineering and Technology
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    • 제3권4호
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    • pp.484-490
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    • 2008
  • In this paper, an integrated fault section detection and isolation strategy is proposed based on the application of the Distribution Automation System(DAS) utilizing advanced IT and communication technologies. The Feeder Remote Terminal Unit(FRTU) has been widely used to collect data in the Korean distribution system. The achieved data is adopted in this method for detecting multiple fault types. Especially in the case of single phase-to-ground fault, the fault section is detected by comparison of the zero-sequence current phase angle. The test results have verified the effectiveness of the proposed method in a radial distribution system through extensive simulations in Matlab/Simulink. Furthermore, a communication-based demo system identical to the simulation model has been developed, and it can be applied as an online monitoring and control program for fault section detection and isolation.

정지비행 로터 블레이드에 부착된 탭의 공기역학적 효과 (AERODYNAMIC EFFECTS OF THE TAB ON A HOVERING ROTOR BLADE)

  • 강희정;김도형;김승호
    • 한국전산유체공학회지
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    • 제18권3호
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    • pp.60-66
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    • 2013
  • Numerical simulation was performed for the rotor blade with fixed tab in hover using an unstructured mesh Navier-Stokes flow solver. The inflow and outflow boundary conditions using 1D momentum and 3D sink theory were applied to reduce computational time. Calculations were performed at several operating conditions of varying collective pitch angle and fixed tab length. The aerodynamic effect of fixed tab length was investigated for hovering efficiency, pitching moment and flapping moment of the rotor blade. The results show that it affects linearly increasing on the pitching moment of the rotor blade but does not affect on the flapping moment. The required power is less than 45kw for ground rotating test in hover. Numerical simulations also show that the vortex generate not only from the tip of the rotor blade but also from the fixed tab on the rotor blade.

Comparison of Sensitivity Analysis Methods for Building Energy Simulations in Early Design Phases: Once-at-a-time (OAT) vs. Variance-based Methods

  • Kim, Sean Hay
    • KIEAE Journal
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    • 제16권2호
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    • pp.17-22
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    • 2016
  • Purpose: Sensitivity analysis offers a good guideline for designing energy conscious buildings, which is fitted to a specific building configuration. Sensitivity analysis is, however, still too expensive to be a part of regular design process. The One-at-a-time (OAT) is the most common and simplest sensitivity analysis method. This study aims to propose a reasonable ground that the OAT can be an alternative method for the variance-based method in some early design scenarios, while the variance-based method is known adequate for dealing with nonlinear response and the effect of interactions between input variables, which are most cases in building energy simulations. Method: A test model representing the early design phase is built in the DOE2 energy simulations. Then sensitivity ranks between the OAT and the Variance-based methods are compared at three U.S. sites. Result: Parameters in the upper rank by the OAT do not much differ from those by the Main effect index. Considering design practices that designers would chose the most energy saving design option first, this rank similarity between two methods seems to be acceptable in the early design phase.

분당선 한강 하저터널의 방재시스템 (Preventing disaster system of the subaqueous tunnel under the Han river in the Bundang railway)

  • 김용일;황낙연;윤영훈;지홍근;장성욱;김동현
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2004년도 추계학술대회 논문집
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    • pp.308-327
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    • 2004
  • As use of tunnels and subways increase there also are accidents proportionate to it. Daegu Subway Station fire, Hongjimoon tunnel fire led people to be conscious of disaster protection and as a result, there is a trend to adopt standards for fire protection. Accordingly, this thesis is focused on investigating various fire and water protection related issues for subaqueous tunnel under Ran river. The thesis developed evacuation and disaster prevention plan as fire level increases and have identified the suitability of disaster prevention through evacuation and fire simulation, countermeasure of a water leakage during construction and operation considering the subaqueous tunnel. And we selected EPB shield TBM equipment considering the ground condition and effect of boring hole, and accomplished reasonable water protection design through setting goals using event-tree method, as well as examining model test of boring hole and flooding in heavy rain. Also included structured total system consist of water leakage sensing system, water protection gate, pumping system and fire protection system to respond systematically in emergency.

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이차 연소를 위한 가스발생기의 압력 제어기법 연구 (Control law design of gas generator for secondary combustion)

  • 박익수;이재윤;최호진;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.565-568
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    • 2010
  • 가스 발생기의 유량을 조절하기 위한 압력제어 법칙을 제안하였다. 고체 연료의 연소속도 모델과 가스발생기의 연소가스 보존방정식을 이용하여 내부 압력에 관한 동적 모델링을 하였고, 모델의 타당성을 검증하기 위하여 내탄도 해석 및 시험결과와 비교하였다. 비교 결과 모델은 연소압력을 매우 정확히 모의할 수 있는 모델임이 밝혀졌고, 같은 모델을 이용하여 고전 제어기법을 적용하여 제어 가능성과 문제점을 시뮬레이션을 통해 식별하였다. 고전 제어기가 보여준 시변 시스템에서의 성능저하를 극복하기 위하여 비선형 적응형 제어 기법을 제안하였으며, 수치 시뮬레이션 결과 우수한 추종 성능을 보였다.

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Experimental study on high gravity dam strengthened with reinforcement for seismic resistance on shaking table

  • Wang, Mingming;Chen, Jianyun;Fan, Shuli;Lv, Shaolan
    • Structural Engineering and Mechanics
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    • 제51권4호
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    • pp.663-683
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    • 2014
  • In order to study the dynamic failure mechanism and aseismic measure for high concrete gravity dam under earthquake, the comparative models experiment on the shaking table was conducted to investigate the dynamic damage response of concrete gravity dam with and without the presence of reinforcement and evaluate the effectiveness of the strengthening measure. A new model concrete was proposed and applied for maintaining similitude with the prototype. A kind of extra fine wires as a substitute for rebar was embedded in four-points bending specimens of the model concrete to make of reinforced model concrete. The simulation of reinforcement concrete of the weak zones of high dam by the reinforced model concrete meets the similitude requirements. A tank filled with water is mounted at the upstream of the dam models to simulate the reservoir. The Peak Ground Acceleration (PGA) that induces the first tensile crack at the head of dam is applied as the basic index for estimating the overload capacity of high concrete dams. For the two model dams with and without strengthening tested, vulnerable parts of them are the necks near the crests. The results also indicate that the reinforcement is beneficial for improving the seismic-resistant capacity of the gravity dam.

무인기용 직렬 하이브리드 동력시스템 운용 제어로직 (Operational Control Logic of Series Hybrid Power System for the Unmanned Aerial Vehicle)

  • 이보화;박부민;김근배
    • 한국추진공학회지
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    • 제25권1호
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    • pp.68-76
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    • 2021
  • 본 연구에서 대상으로 삼은 직렬 하이브리드 시스템은 무인기용으로 왕복엔진, 발전기, 배터리를 주 동력원으로 사용한다. 발전기는 왕복엔진의 구동축에 직결되며, 왕복엔진-발전기 세트의 운용 특성은 지상통합시험을 통해 확인하였다. 본 연구에서는 해당 시험 결과를 바탕으로 왕복엔진-발전기 출력과 배터리 출력을 효율적으로 사용하기 위한 제어로직을 제시하였고, 로직에 따른 왕복엔진-발전기와 배터리의 출력 변동은 시뮬레이션을 통해 확인하였다. 그 결과, 발전기 출력은 제시된 제어로직에 의해 배터리 출력과 함께 추진요구전력을 공급함을 확인하였다.

복합재 주익 무인항공기의 낙뢰보호 설계와 피격영역 해석 (Protection Design and Lightning Zone Analysis for Unmanned Aerial Vehicle with Composite Wings)

  • 우희채;김용태
    • 한국군사과학기술학회지
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    • 제26권3호
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    • pp.302-312
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    • 2023
  • This paper describes the analysis of lightning strike zoning, the indirect lightning data simulation and the protection design for lightning indirect effects of equipment by lightning strike for unmanned aircraft consisting of composite wings. Through the analysis of lightning strike zoning according to the external shape of unmanned aerial vehicles, the structure areas that should be protected during lightning strike is derived, and the protection requirements of lightning indirect effects for flight critical equipments and equipment that must be operated upon lightning strike was derived. Lightning protection levels according to the location of mounting equipment and surrounding structure materials for each equipment was derived, and the protection design of the unmanned aerial vehicle with composite structures was also proposed from direct effect of lightning. Later, the lightning protection technology will be verified by the ground test of lightning direct and indirect effects.

무인항공기 체계의 통합검증을 위한 무인항공기 체계통합실험실(UAV SIL) 개발 (Development of Unmanned Aerial Vehicle System Integration Laboratory(UAV SIL) for the Integrated Verification)

  • 심재익;우희채;김상진;정상준
    • 한국군사과학기술학회지
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    • 제27권1호
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    • pp.70-79
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    • 2024
  • This paper describes the results of the development of the the unmanned aerial vehicle system integration laboratory(UAV SIL) for the integrated verification. This UAV SIL is designed to test the robustness of the UAV system including the operational logics and the flight control system behaviors under many abnormal and emergency conditions such as data-link losses, airborne subsystem failures, engine shut down conditions, and ground control station faults. This paper presents how to build the UAV SIL and how to verify the in-development UAV system through the UAV SIL.

소형민수헬기 능동진동제어시스템 개발 (Development and Verification of Active Vibration Control System for Helicopter)

  • 김남조;곽동일;강우람;황유상;김도형;김찬동;이기진;소희섭
    • 한국항공우주학회지
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    • 제50권3호
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    • pp.181-192
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    • 2022
  • 헬기의 능동진동제어시스템(AVCS)은 주로터로부터 발생되는 진동을 제어하며, 수동형 진동저감장치 대비 저중량으로 우수한 진동저감 성능을 발휘한다. 본 논문에서는 FxLMS 알고리즘을 기반으로 타코미터 및 가속도 센서 신호를 통해 연산된 제어명령을 하중발생기(CFG)로 전달하여 소형민수헬기의 진동을 제어하는 소프트웨어 개발 및 검증 내용을 제시하였다. DO-178C /DO-331 표준에 따라 모델 기반 설계 기법을 통해 진동제어 소프트웨어를 개발하였으며, PILS 및 HILS 환경에서 실시간 작동 성능을 평가하였다. 특히, PILS 환경에서는 LDRA 기반 검증 커버리지를 통해 소프트웨어의 신뢰성을 향상시켰다. AVCS를 소형민수헬기에 적용하기 위해 지상/비행시험을 통해 대상 헬기 동적응답특성 모델을 획득하였다. 이를 기반으로 시스템 최적화 분석 및 비행시험을 통해 최적 성능을 발휘하는 AVCS 형상을 결정하고, STC 인증을 획득하였다.