• Title/Summary/Keyword: HILS(Hardware in the loop simulation)

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The Study of Gateway Control Module Using SAE J1939 Protocol (SAE J1939 프로토콜기반 Gateway 제어모듈 개발에 관한 연구)

  • Ko, Youngjin;Kim, Doyeong
    • Transactions of the Korean Society of Automotive Engineers
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    • v.21 no.1
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    • pp.128-136
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    • 2013
  • This study presents the development of Gateway Control Module using SAE J1939 protocol for the commercial vehicles. Presently, the load rate of CAN bus is increased by the single network composition and addition of new ECUs for development of intelligent vehicles. Because the embedded system of the integrated network control function has the errors of the CAN bus caused by the increase of ECU, it is needed for development of commercial vehicles. Also, this study presents the development of smart functions that can diagnosis CAN bus errors, fault diagnosis of ECU and basic function that arbitrates CAN bus between ECUs of commercial vehicle. GCM was designed for 4channel separation about Gateway function as solution of load rate decrease and smart functions. HILS(Hardware in the loop simulation)system that can achieve simulation about CAN Messages of all systems on vehicle was applied to evaluate performance and verification of all functions and performance. The load rate on CAN bus was decreased at using functions what was delivery, block and process of GCM. Through this, it was enabled to organize systematic architecture for gateway.

Model and component based modeling and simulation of a supersonic propulsion system (모델 및 구성품 기반 초음속 추진기관 실시간 모델링 및 시뮬레이션)

  • Choi, J.H.;Park, I.S.;Lee, J.Y.;Kim, J.H.;Kim, I.S.;Yoon, H.G.;Lim, J.S.;Kim, C.B.;Park, J.M.
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.579-583
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    • 2011
  • The component based propulsion modeling and simulation of an air-breathing engine such as ramjet and scramjet is studied. The simulation model has been realized considering the characteristics of the air-breathing engine which is composed of air intake, combustor and nozzle including engine controller and fuel supply system. To estimate the engine performance and to verify the engine controller, real time based Hardware in the Loop System simulating actual environment is constructed.

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Digital Twin-Based Communication Optimization Method for Mission Validation of Swarm Robot (군집 로봇의 임무 검증 지원을 위한 디지털 트윈 기반 통신 최적화 기법)

  • Gwanhyeok, Kim;Hanjin, Kim;Junhyung, Kwon;Beomsu, Ha;Seok Haeng, Huh;Jee Hoon, Koo;Ho Jung, Sohn;Won-Tae, Kim
    • KIPS Transactions on Computer and Communication Systems
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    • v.12 no.1
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    • pp.9-16
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    • 2023
  • Robots are expected to expand their scope of application to the military field and take on important missions such as surveillance and enemy detection in the coming future warfare. Swarm robots can perform tasks that are difficult or time-consuming for a single robot to be performed more efficiently due to the advantage of having multiple robots. Swarm robots require mutual recognition and collaboration. So they send and receive vast amounts of data, making it increasingly difficult to verify SW. Hardware-in-the-loop simulation used to increase the reliability of mission verification enables SW verification of complex swarm robots, but the amount of verification data exchanged between the HILS device and the simulator increases exponentially according to the number of systems to be verified. So communication overload may occur. In this paper, we propose a digital twin-based communication optimization technique to solve the communication overload problem that occurs in mission verification of swarm robots. Under the proposed Digital Twin based Multi HILS Framework, Network DT can efficiently allocate network resources to each robot according to the mission scenario through the Network Controller algorithm, and can satisfy all sensor generation rates required by individual robots participating in the group. In addition, as a result of an experiment on packet loss rate, it was possible to reduce the packet loss rate from 15.7% to 0.2%.

Implementation and Design of HILS for Development of the ABS ECU for Commercial Vehicle (상용차용 ABS ECU 개발을 위한 HILS 시스템 설계 및 구현)

  • Hwang, D.H.;Cho, J.M.;Sim, W.J.;Park, D.Y.;Kim, Y.J.;Joh, J.S.
    • Proceedings of the KIEE Conference
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    • 2000.11d
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    • pp.609-611
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    • 2000
  • ABS(Antilock Brake System), Prevents the wheels from "locking" and improve steering during braking. Currently, safety and environmental issues are a major concern in the automotive industry. ABS has become the vital brake system HILS (Hardware In-the-Loop Simulation) is an effective tool for design. performance evaluation and test of developed vehicle subsystems such as ABS. suspension. and steering systems. This paper describes a HILS model for an ABS/ASR application Also the design and implementation of HILS system for development of the ABS ECU(Electronic Centre) Unit) for commercial vehicle are presented.

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Implementation of HILS System for Performance Test of the ABS ECU for Commercial Vehicles (상용차용 ABS ECU의 성능분석을 위한 HILS 시스템 구축)

  • Cho, J.M.;Hwang, D.H.;Park, D.Y.;Kim, Y.J.;Joh, J.S.;Park, S.K.
    • Proceedings of the KIEE Conference
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    • 2000.07d
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    • pp.2564-2566
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    • 2000
  • HILS(Hardware In-the-Loop Simulation) is an effective tool for design, performance evaluation and test of developed vehicle subsystems such as ABS(Antilock Brake System), suspension, and steering systems. This paper describes a HILS model for an ABS/ASR application. Also the implementation of HILS system for performance test of the ABS ECU(Electronic Control Unit) for commercial vehicles is presented.

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Performance Analysis of the Flight Control System for UAV using HILS System (HILS 시스템을 이용한 무인항공기 비행제어시스템의 성능분석)

  • Kim, Min-Soo;Baek, Soo-Ho;Choe, Yu-Hwan;Hong, Sung-Kyung
    • Proceedings of the KIEE Conference
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    • 2005.07d
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    • pp.2546-2548
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    • 2005
  • 본 논문에서는 무인항공기의 비행제어시스템 개발 및 성능분석을 위한 HILS(Hardware-in-the-Loop-Simulation) 시스템의 구축을 제안한다. 제안한 HILS 시스템은 실시간 시뮬레이션 컴퓨터(dSPACE DS1005), 3축 모션테이블, 자세 센서, 지상통제장치(GCS; Ground Control Station), 비행제어컴퓨터(FCC; Flight Control Computer)로 구성된다. 실제 신호와 유사한 신호를 발생시키기 위한 실시간 시뮬레이션 컴퓨터는 dSPACE가 담당하며, 이 신호는 비행운동을 재현을 위한 3축 모션테이블을 동작시키게 된다. 모션테이블 상에 위치하는 자세센서 값과 GCS의 명령은 FCC의 입력으로 사용된다. 구현된 HILS 시스템을 이용하여 UAV의 제어알고리즘 및 자세센서 성능 검증을 수행하였다.

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Implementation of OPLA-RT based HILS system for developing MMC control algorithm of offshore wind power (해상 풍력 연계 MMC 제어 알고리즘 개발을 위한 OPLA-RT 기반의 HILS 구축)

  • Shin, Dong-Cheol;Yoon, Jin-Woo;Lee, Dong-Myung
    • Proceedings of the KIPE Conference
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    • 2019.07a
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    • pp.414-415
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    • 2019
  • 본 논문은 HVDC(High Voltage Direct Current)에 적용된 MMC(Modular Multilevel Converter)의 제어 알고리즘 개발을 위한 HILS(Hardware In the Loop Simulation)을 위한 모델링 및 HILS 시스템 구축 예를 보인다. 전력 계통, MMC, 풍력 발전 등의 HILS 적용 MATLAB/SIMULINK 모델 및 FPGA(Field Programmable Gate Array)를 이용한 제어기 개발 내용을 보인다. 시뮬레이션 모델과 FPGA 제어기를 이용하여 구축한 OPAL-RT 기반의 실험 결과를 보인다.

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