• 제목/요약/키워드: Hardware in the loop system

검색결과 364건 처리시간 0.028초

전력 HILs를 활용한 스마트 인버터의 LVRT 시험 (Low Voltage Ride Through Test for Smart Inverter in Power Hardware in Loop System)

  • Sim, Junbo
    • KEPCO Journal on Electric Power and Energy
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    • 제7권1호
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    • pp.101-105
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    • 2021
  • Encouragement of DER from Korean government with several policies boosts DER installation in power system. When the penetration of DER in the grid is getting high, loss of generation with break-away of DER by abnormal grid conditions should be considered, because loss of high generation causes abnormal low frequency and additional operations of protection system. Therefore, KEPCO where is Korean power utility is preparing improvement in regulations for DERs connected to the grid to support abnormal grid conditions such as low and high frequencies or voltages. This is called 'Ride Through' because the requirement is for DER to maintain grid connection during required periods when abnormal grid conditions occur. However, it is not easy to have a test for ride through capability in reality because emulation of abnormal grid conditions is not possible in real power system in operation. Also, it is not easy to have a study on grid effect when ride through capability fails with the same reason. PHILs (Power Hardware In the Loop System) makes it possible to analyze power system and hardware performance at once. Therefore, this paper introduces PHILs test methods and presents verification of ride through capability especially for low voltage grid conditions.

브레이크HILS를 이용한 능동 요모멘트 제어 알고리즘의 평가 (Evaluation of A Direct Yaw Moment Control Algorithm by Brake Hardware-In-The -Loop Simulation)

  • 류제하;김호수
    • 한국자동차공학회논문집
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    • 제7권8호
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    • pp.172-179
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    • 1999
  • This paper presents a simple but effective DYC algorithm which enhances vehicle lateral stability by using an anti=lock brake system (ABS). In the proposed algorithm, only the front outer wheel is controlled during cornering maneuver instead of controlling all four wheels because the wheel has the largest role in DYC and it is easy and simple to control the only one wheel. An ABS Hardware - In -The -Loop Simulation ( HILS) system that may be used to realistically test real vehicle dynamic behavior in a lab is used for evaluating the proposed DYC algorithm in severe situations where a vehicle is destabilized without DYC . The HILS results show that the proposed DYC algorithm has the potential of maintaining vehicle stability in some dangerous situations.

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굴삭기용 Hardware In the Loop System(HILS) 개발 (Development of Hardware In the Loop System(HILS) for Hydraulic Excavator)

  • 임태형;조현철;안태규;양순용;이홍선
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 추계학술대회 논문집
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    • pp.468-473
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    • 2004
  • This paper deal with basic concept of Hardware In the Loop System(HILS) for hydraulic excavator. Hydraulic excavator has many nonlinearities because of P-Q diagram, dead zone and saturation of valve, single acting cylinder, heavy manipulator. So, actual test is needed when new component or control algorithm is developed but many restrictions exist. Hydraulic circuit of excavator is too complex to model mathematically but dynamic equation of manipulator has made good progress in previous studies. Basic concept of HILS and AMESim model of hydraulic components is contained in this paper.

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HARDWARE IN THE LOOP SIMULATION OF HYBRID VEHICLE FOR OPTIMAL ENGINE OPERATION BY CVT RATIO CONTROL

  • Yeo, H.;Song, C.H.;Kim, C.S.;Kim, H.S.
    • International Journal of Automotive Technology
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    • 제5권3호
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    • pp.201-208
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    • 2004
  • Response characteristics of the CVT system for a parallel hybrid electric vehicle (HEV) are investigated. From the experiment, CVT ratio control algorithm for the optimal engine operation is obtained. To investigate the effect of the CVT system dynamic characteristics on the HEV performance, a hardware in the loop simulation (HILS) is performed. In the HILS, hardwares of the CVT belt-pulley and hydraulic control valves are used. It is found that the engine performance by the open loop CVT ratio control shows some deviation from the OOL in spite of the RCVs open loop control ability. To improve the engine performance, a closed loop control of the CVT ratio is proposed with variable control gains depending on the shift direction and the CVT speed ratio range by considering the nonlinear characteristics of the RCV and CVT belt-pulley dynamics. The HILS results show that the engine performance is improved by the closed loop control showing the operation trajectory close to the OOL.

디지털 조속기의 성능 시험을 위한 HILS 시스템 개발에 관한 연구 (A Study on the Development of HILS System for Performance Test of Digital Governor)

  • 장민규;조성훈;전일영;안병원;박영산;배철오;이성근;김윤식
    • 한국정보통신학회:학술대회논문집
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    • 한국해양정보통신학회 2003년도 춘계종합학술대회
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    • pp.317-319
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    • 2003
  • HILS(Hardware In-the Loop Simulation)은 임베디드(Embedded) 시스템의 개발과 시험에 많이 이용된다. 임베디드(Embedded) 시스템은 시스템의 운전 환경에서 쉽고, 철저하게 그리고 반복해서 시험할 수 없을 때 사용된다. HILS는 빠르고 경제적으로 제품을 개발하는데 유효하다. 또한 생산품이 생산을 시작한 후에 심각한 문제점들이 발견될 가능성을 상당히 줄여주어 생산품 개발 시간동안에 설계 최적화와 하드웨어/소프트웨어 디버깅을 실행하는데 도움을 준다. 본 연구는 Digital Governor의 성능을 확인하기 위해 스팀터빈 플랜트와 동기 발전기를 포함한 시뮬레이터를 HIL(Hardware In-the Loop Simulator)로 구현하였으며, 실시간으로 시스템의 응답을 확인할 수 있도록 소프트웨어로 구성하였다.

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합성환경 하에서의 수중운동체 HILS/MILS 구현 기법 연구 (A Study on Implementation of an Underwater Vehicle HILS/MILS System in Synthetic Environment)

  • 남경원
    • 한국군사과학기술학회지
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    • 제5권2호
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    • pp.132-148
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    • 2002
  • In this paper, development procedures of an Underwater Vehicle HILS/MILS System in SE(Synthetic Environment) are described. As this System is developed, we can obtain the more powerful tool which can be used to test and verify operational logics and algorithms of an Underwater Vehicle as well as its hardware in various tactical situations.

부유시스템을 이용한 유도탄 조종루프 진동저감 성능확인 시험기법 (A Test Technique for Performance Evaluation of a Filter and Control Loop on the Missile Vibration using Floating System)

  • 김경환;박범수;이현;김상재;정재욱
    • 한국군사과학기술학회지
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    • 제21권5호
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    • pp.623-629
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    • 2018
  • The acceleration and the angular velocity that include natural frequencies of a missile detected by Inertial Measurement Unit(IMU) are transmitted to the control loop of a missile. The control loop command that is calculated using above signals can cause the resonance of the missile while it flies. Hence it is common to adapt the filter and the control loop for attenuating or eliminating the undesired signals such as natural frequencies. This paper introduces the new test technique using a floating system for performance evaluation of the designed filter and the control loop prior to a flight test. The proposed scheme can check out the degradation property of vibration in the filter and the control loop, while the conventional hardware-in-the-loop simulation(HILS) scheme cannot.

전동식 동력 조향 장치 연구를 의한 HILS 시스템 개발 (A Development of Hardware-in-the Loop Simulation System For a Electric Power Steering System)

  • 박동진;윤석찬;한창수
    • 대한기계학회논문집A
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    • 제24권12호
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    • pp.2883-2890
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    • 2000
  • In this study, a Hardware-In-The-Loop-Simulation(HILS) system for developing a Electric-Power-Steering(EPS) system is designed. To test a EPS by HILS system, a mathematical vehicle model with a steering system model has been constructed. This mathematical model has been constructed. This mathematical model has been downloaded to the Digital-Signal-Processor(DSP) board. To realize the lateral force acting on the front wheel in a real car. the steering wheel angle sensor and vehicle velocity have been used for input signal. The force sensor has been used for a feedback signal. The full vehicle states could by simulated by the HILS system. Consequently, the HILS system could by used to analyze control-parameters of a EPS that contributes to the maneuverability and stability of a vehicle. At the same time, the HILS system can evaluate the whole performance of the vehicle-steering system. Also the HILS system could do test could not be executed in real vehicle. The HILs system will useful for developing the control logic for the EPS system.

자동변속기용 임베디드 시스템 성능 시험을 위한 Hardware-in-the Loop 시뮬레이터 구축 (Development of Hardware-in-the-Loop Simulator for Testing Embedded System of Automatic Transmission)

  • 장인규;서인근;전재욱;황성호
    • 제어로봇시스템학회논문지
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    • 제14권3호
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    • pp.301-306
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    • 2008
  • Drivers are becoming more fatigued and uncomfortable with increase in traffic density, and this condition can lead to slower reaction time. Consequently, they may face the danger of traffic accidents due to their inability to cope with frequent gear shifting. To reduce this risk, some drivers prefer automatic transmission (AT) over manual transmission (MT). The AT offers more superior drivability and less shifting shock than the MT; therefore, the AT market share has been increasing. The AT is controlled by an electronic control unit (ECU), which provides better shifting performance. The transmission control unit (TCU) is a higher-value-added product, so the companies that have advanced technologies end to evade technology transfer. With more cars gradually using the ECU, the TCU is expected to be faster and more efficient for organic communication and arithmetic processing between the control systems than the l6-bit controller. In this paper, the model of an automatic transmission vehicle using MATLAB/Simulink is developed for the Hardware in-the-Loop (HIL) simulation with a 32-bit embedded system, and also the AT control logic for shifting is developed by using MATLAB/Simulink. The developed AT control logic, transformed automatically by real time workshop toolbox, is loaded to a 32-bit embedded system platform based on Freescale's MPC565. With both vehicle model and 32-bit embedded system platform, we make the HIL simulation system and HIL simulation of AT based on real time operating system (RTOS) is performed. According to the simulation results, the developed HIL simulator will be used for the performance test of embedded system for AT with low cost and effort.

자동추력 제어시스템 개발 및 검증 (Development and Validation of Automatic Thrust Control System)

  • 김종섭;조인제;이동규
    • 제어로봇시스템학회논문지
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    • 제16권9호
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    • pp.905-912
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    • 2010
  • Modern version of advanced supersonic fighter have ATCS (Automatic Thrust Control System) to maximum flight safety, fuel efficiency and mission capability the integrated advanced autopilot system such as TFS (Terrain Following System), GCAS (Ground Collision Avoidance System) and AARS (Automatic Attitude Recovery System) and etc. This paper addresses the design and verification of ATCS based on advanced supersonic trainer in HILS (Hardware In the Loop Simulator) with minimum hardware modification to reduce of development cost and maintain of system reliability. The function of ATCS is consisted of target speed hold mode in UA (Up and Away) and angle of attack hold mode in PA (Power Approach). The real-time pilot evaluation reveals that pilot workload is minimized in cruise and approach flight stage by ATCS.