• 제목/요약/키워드: load simulator

검색결과 319건 처리시간 0.022초

고속 엘리베이터 시스템용 시뮬레이터 개발 (Development of Simulator for High-Speed Elevator System)

  • 류형민;김성준;설승기;권태석;김기수;심영석;석기룡
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제51권2호
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    • pp.77-82
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    • 2002
  • This Paper describes the dynamic load simulator for high-speed elevator system, which can emulate 3-mass system as well as equivalent 1-mass system. In order to implement the equivalent inertia of entire elevator system the conventional simulators have generally utilized the mechanical inertia(flywheel) with large radius, which makes the entire system large and heavy. In addition, the mechanical inertia should be replaced each time in order to est another elevator system. In this paper, the dynamic load simulation methods using electrical inertia are Presented so hat the volume and weight of simulator system are greatly reduced and the adjustment of inertia value can be achieved easily by software. Experimental results show the feasibility of this simulator system.

발전기 부하추종성 시험용 주파수 Simulator 설계에 관한 연구 (A Study on Frequency Simulator Design for Load Following Test of Generator)

  • 곽월환;이강완;오창수
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 추계학술대회 논문집 전력기술부문
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    • pp.138-142
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    • 2004
  • Recently over dropped frequencies of power system were recorded when power system was unbalanced between generation and demand. Therefore load following characteristic analysis of thermal and combined cycle power plant generators is necessary for low frequency condition analysis of power system. Frequency simulator supplies simulated frequency to the online generator for prescribed goal. This simulator needs to minimize effects to power system and requires stability first. This paper introduces design and manufacturing case of frequency simulator for load following characteristic analysis of generators.

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항공기 조종면 부하재현장치의 운동 특성 해석 (Dynamic Characteristic Analysis of Aerodynamic Load Simulator English)

  • 남윤수
    • 대한기계학회논문집A
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    • 제25권3호
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    • pp.478-485
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    • 2001
  • A dynamic load simulator(DLS) which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of aircraft actuation system. By setting up load actuator as counter acting with the control surface driving actuator and designing an appropriate force control system for load actuator, DLS can be mechanized. Obtaining an accurate mathematical model for the DLS is the first step to successfully design an aerodynamic load replicati on system. Two theoretical models are presented and tested for their validities with the experimental results, which turns out to be not successful. An alternative way of using system identification approaches in investigated to develop a good nominal model for DLS dynamics, and suitable uncertainty bounds for this nominal model are proposed with the consideration of experimental results.

RAS: Request Assignment Simulator for Cloud-Based Applications

  • Rajan, R. Arokia Paul;Francis, F. Sagayaraj
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제9권6호
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    • pp.2035-2049
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    • 2015
  • Applications deployed in cloud receive a huge volume of requests from geographically distributed users whose satisfaction with the cloud service is directly proportional to the efficiency with which the requests are handled. Assignment of user requests based on appropriate load balancing principles significantly improves the performance of such cloud-based applications. To study the behavior of such systems, there is a need for simulation tools that will help the designer to set a test bed and evaluate the performance of the system by experimenting with different load balancing principles. In this paper, a novel architecture for cloud called Request Assignment Simulator (RAS) is proposed. It is a customizable, visual tool that simulates the request assignment process based on load balancing principles with a set of parameters that impact resource utilization. This simulator will help to ascertain the best possible resource allocation technique by facilitating the designer to apply and test different load balancing principles for a given scenario.

추진인버터 시험을 위한 실시간 부하 시뮬레이터에 관한 연구 (Study on Real-Time Load Simulator for Testing Propulsion Inverter Test)

  • 김길동;신정렬;이우동;한석윤;박기준
    • 한국철도학회논문집
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    • 제7권1호
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    • pp.1-8
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    • 2004
  • A newly-built inverter has to undergo a series of stress tests in the final stage of production line. This can be achieved by connecting it to a dynamometer consisting of a three-phase machine joined by a rigid shaft to a DC load machine. The latter is controlled to create some specific load characteristic needed for the test. In this paper a test method is proposed, in which no mechanical equipment is needed. The suggested test stand consists only of a inverter to be tested and a simulator converter. Both devices are connected back-to-back on the AC-side via smoothing reactors. The simulator operates in real-time as an equivalent load circuit, so that the device under test will only notice the behaviour of a three-phase machine under consideration of the load. In oder to prove rightness of the suggested test method, the simulation and actural experiment carried out emulation for a 2.2kW induction motor.

실물실험에 의한 순환공기 바이패스 공조시스템의 성능분석 (The Performance Analysis of a Return Air Bypass Air Conditioning System by a Simulator Experiment)

  • 신현준;김보철;김정엽
    • 에너지공학
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    • 제11권2호
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    • pp.130-135
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    • 2002
  • 바이패스 공조시스템은 냉각코일과 가열코일의 공기통과여부에 따라 크게 외기바이패스, 혼합공기 바이패스와 순환공기 바이패스 공조시스템으로 구분할 수 있다. 이 중에서 순환공기 바이패스 공조시스템은 다른 두 방식과 달리 공조되지 않은 외기가 시스템 내부로 직접 유입되지 않으므로 실내온습도 조절면에서 가장 효율적인 시스템이다. 먼저, 수치계산을 통하여 부하변동에 따른 순환공기 바이패스 공조시스템과 단일덕트 정풍량공조시스템의 실내온습도 구현능력을 비교, 평가하였다. 또한 제안 시스템의 성능분석을 위해 실물실험동을 건립하여 그 실험결과를 수치계산결과와 비교하였다. 실험을 통하여 실현열비가 0.7(현열부하만 변동)인 경우, 실내 최대현열부하에 대한 부분부하시의 실내 현열부하의 비(DSL; Design Sensible Load)가 70% 이내에서는 수치계산, simulator 실험 모두 실내상대습도는 ASHRAE STANDARD 62-1999에서 지정하는 60% 이하로 유지됨을 알 수 있었다. 결론적으로, 바이패스 공조시스템은 실내의 온습도를 정해진 범위의 부하변동내에서는 바이패스 댐퍼의 조작만으로 쾌적한 상태로 유지시킬 수 있으며, 환기회수가 많은 장손의 경우, 순환공기 바이패스에 의해 양질의 실내공기질(IAQ; Indoor Air qualify)을 확보할 수 있다.

건설차량 주행용 동력 전달계의 실시간 시뮬레이터에 관한 연구 (A Study on Real Simulator of Running Power Train for Construction Vehicle)

  • 이일영;김진원;윤소남;양경욱
    • 한국자동차공학회논문집
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    • 제4권2호
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    • pp.90-105
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    • 1996
  • A real tine simulator of running power train for a construction vehicle was developed. The simulator mainly consists of following two parts; (1) running power train part and (2) running load generation part. An optimal servo control algorithm was adopted for designing the multi-variable digital control system of the simulator. By experiments investigating response characteristics under step-wise variation or pre-determined scenario of target vehicle velocity and target load torque, it was verified that the simulator could reproduce physical situations at and actual vehicle with excellent similarity.

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대부하 6자유도 운동 시뮬레이터의 실시간 제어기 설계에 관한 연구 (Study on real time controller design of heavy load 6-DOF mition simulator)

  • 김영대;강석종;이상범;박정호
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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    • pp.13-16
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    • 1989
  • The paper, introduce the real time controller Design method of heavy load 6-DOF motion simulator. And also, introduce the Geometric design of 6-DOF Motion generation, real time control A algorithm and the configuration method of real time controller H/W and S/W.

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교육용 전력 시스템 해석 소프트웨어 개발 (Development of Educational Simulator for Power System Analysis)

  • 추성호;이주원;이우남;김현홍;박종배;신중린
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2007년도 추계학술대회 논문집 전력기술부문
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    • pp.187-189
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    • 2007
  • This paper presents the development method of educational simulator for Power System Analysis. The developed simulator can be made the students to model, analysis of power systems by drawing the system and performing the load flow, fault analysis by themselves under window environment. The simulator has developed by using the language based on XML(extensible Markup Language). Therefore, we determine that this simulator is useful to educate the load flow and fault analysis.

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