• Title/Summary/Keyword: Real-Time Hardware-In-the-Loop Simulation

Search Result 128, Processing Time 0.021 seconds

A Strategy to Evaluate Semi-Active Suspension System using Real-Time Hardware-in-the-Loop Simulation (실시간 Hardware-in-the-Loop 시뮬레이션을 이용한 반능동 현가시스템 특성 평가)

  • Choi, G.J.;Noh, K.H.;Yoo, Y.M.;Kim, H.
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.9 no.6
    • /
    • pp.186-194
    • /
    • 2001
  • To meet the challenge of testing increasingly complex automotive control systems, the real-time hardware-in-the-loop(HIL) simulation technology has been developed. In this paper, a strategy for evaluation of semiactive suspension systems using real-time HIL simulation is presented. A multibody vehicle model is adopted to simulate vehicle dynamic motions accurately. Accuracy of the vehicle simulation results is compared to that of the real vehicle field test and proven to be very accurate. The controller and stepping motor to adjust semi-active damper stage are equipped as external hardwares and connected to the real-time computer which has vehicle dynamic model. Open and closed loop test methods are used to evaluate a controlled suspension system and the system's operations are verified it is found that the proposed evaluation methods can be used well for the verification of semi-active suspension systems.

  • PDF

HILS(Hardware-In-the-Loop Simulation) Development of a Steering HILS System (전동식 동력 조향 장치 시험을 위한 HILS(Hardware-In-the-Loop Simulation) 시스템 개발)

  • 류제하;노기한;김종협;김희수
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.7 no.9
    • /
    • pp.105-111
    • /
    • 1999
  • The paper presents development of a Hardware-In-the-Loop simulation (HILS) system for the purpose of testing performance, stability, and reliability of an electronic power steering system(EPS). In order to realistically test an EPS by the proposed HILS apparatus, a simulated uniaxial dynamic rack force is applied physically to the EPS hardware by a pnumatic actuator. An EPS hardware is composed of steering wheel &column, a rack & pinion mechanism, andas motor-driven power steering system. A command signal for a pneumatic rack-force actuator is generated from the vehicle handling lumped parameter dynamic model 9software) that is simulated in real time by using a very fast digital signal processor. The inputs to the real-time vehicle dynamic simulation model are a constant vehicle forward speed and from wheel steering angles driven through a steering system by a driver. The output from a real-time simulation model is an electric signal that is proportional to the uniaxial rack force. The vehicle handling lumped parameter dynamic model is validated by a fully nonlinear constrained multibody vehicle dynamic model. The HILS system simulation results sow that the proposed HILS system may be used to realistically test the performance stability , and reliability of an electronic power steering system is a repeated way.

  • PDF

A real time simulation for IR Guided Missile (적외선 유도탄의 실시간 시뮬레이션)

  • Kim, T.Y.;Kim, Y.J.;Lee, J.H.
    • Proceedings of the KIEE Conference
    • /
    • 1993.07a
    • /
    • pp.421-423
    • /
    • 1993
  • A real time simulation is an effective tool for use in design, performance evaluation, and testing of the vehicle dynamic system. An alternate approach is to use a computer system designed specifically to provide an integrated simulation environment in which all aspects of hardware-in-the-loop simulation task have been taken into account.

  • PDF

Real-time and Power Hardware-in-the-loop Simulation of PEM Fuel Cell Stack System

  • Jung, Jee-Hoon
    • Journal of Power Electronics
    • /
    • v.11 no.2
    • /
    • pp.202-210
    • /
    • 2011
  • Polymer electrolyte membrane (PEM) fuel cell is one of the popular renewable energy sources and widely used in commercial medium power areas from portable electronic devices to electric vehicles. In addition, the increased integration of the PEM fuel cell with power electronics, dynamic loads, and control systems requires accurate electrical models and simulation methods to emulate their electrical behaviors. Advancement in parallel computation techniques, various real-time simulation tools, and smart power hardware have allowed the prototyping of novel apparatus to be investigated in a virtual system under a wide range of realistic conditions repeatedly, safely, and economically. This paper builds up advancements of optimized model constructions for a fuel cell stack system on a real-time simulator in the view points of improving dynamic model accuracy and boosting computation speed. In addition, several considerations for a power hardware-in-the-loop (PHIL) simulation are provided to electrically emulate the PEM fuel cell stack system with power facilities. The effectiveness of the proposed PHIL simulation method developed on Opal RT's RT-Lab Matlab/Simulink based real-time engineering simulator and a programmable power supply is verified using experimental results of the proposed PHIL simulation system with a Ballard Nexa fuel cell stack.

A Study on the Development of HWIL Simulation Control System for High Maneuver Guided Missile System (고기동 유도무기를 위한 HWIL 시뮬레이션 제어 시스템 개발 연구)

  • Kim, Woon-Sik;Lee, Byung-Sun;Kim, Sang-Ha
    • The Journal of Korean Institute of Communications and Information Sciences
    • /
    • v.35 no.11B
    • /
    • pp.1659-1666
    • /
    • 2010
  • The High maneuver missiles use various interfaces and high speed guidance and control loop. Hardware-in-the-Loop(HWIL) simulation control system, therefore, should have high performance computing power and hardware interface capabilities, and should be developed using IT technology with which real time operating system, embedded system, data communication technology, and real time hardware control are integrated. This paper suggests the control system design techniques, such as a system hardware configuration, a job distribution algorithm for high performance multi-processors, a real time calculation and control mechanism, inter-processor communication mechanism, and a real time data acquisition technique, to perform the HWIL simulation for high maneuver missile system.

Development of Brake Controller for fixed-wing aircraft using hardware In-the-Loop Simulation

  • Lee, Ki-Chang;Jeon, Jeong-Woo;Hwang, Don-Ha;Kim, Yong-Joo
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 2005.06a
    • /
    • pp.535-538
    • /
    • 2005
  • Today, most fixed-wing aircrafts are equipped with the antiskid brake system. It can modulate braking moments in the wheels optimally, when an aircraft is landing. So it can reduce landing distance and increase safeties. The antiskid brake system for an aircraft are mainly composed of braking moment modulators (hydraulic control valves) and brake control unit. In this paper, a Mark IV type - fully digital - brake controller is studied. For the development of its control algorithms, a 5-DOF (Degree of Freedom) aircraft landing model is composed in the form of matlab/simulink model at first. Then, braking moment control algorithms using wheel decelerations and slips are made. The developed algorithms are tested in software simulations using state-flow toolboxes in matlab/simulink model. Also, a real-time simulation systems are made, which use hydraulic brake systems of a real aircraft, pressure control valves and its controller as hardware components of HIL(Hardware In-the-Loop) simulation. Algorithms tested in software simulations are coded into the controller and the real-time landing simulations are made in very severe road conditions. The real-time simulation results are presented.

  • PDF

Development of Hardware In-the-Loop Simulation System for Testing Power Management of DC Microgrids Based on Decentralized Control (분산제어 기반 직류 마이크로그리드 전력관리시스템의 HIL 시뮬레이션 적용 연구)

  • To, Dinh-Du;Le, Duc-Dung;Lee, Dong-Choon
    • The Transactions of the Korean Institute of Power Electronics
    • /
    • v.24 no.3
    • /
    • pp.191-200
    • /
    • 2019
  • This study proposes a hardware-in-the-loop simulation (HILS) system based on National Instruments' PXI platform to test power management and operation strategies for DC microgrids (MGs). The HILS system is developed based on the controller HIL prototype, which involves testing the controller board in hardware with a real-time simulation model of the plant in a real-time digital simulator. The system provides an economical and effective testing function for research on MG systems. The decentralized power management strategy based on the DC bus signaling method for DC MGs has been developed and implemented on the HILS platform. HILS results are determined to be similar to those of the off-line simulation in PSIM software.

A Simulation Technique of the Shipboard INS Transfer Alignment Environments using Hardware-In-the-Loop Simulation (HILS를 이용한 함정의 관성항법장치 전달정렬 환경 모의 기법)

  • Kim, Woon-Sik;Yang, Tae-Soo;Kim, Sang-Ha
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.14 no.2
    • /
    • pp.181-188
    • /
    • 2011
  • A simulation technique, which simulate dynamic motion and communication environments of ship in the lab, is needed in order to reduce the testing cost when we evaluate the transfer alignment performance of shipboard INS. Hardware-In-the-Loop Simulation(HILS) can be used as an effective test method for those system because it can provide flexible and realistic simulation environments, various test scenario, and repeated test environment in the lab without additional cost and person. This paper presents the methods for implementing the real time HILS environment for testing transfer alignment performance of shipboard INS. It includes real time executive for controlling realtime simulation and calculating the ship motion, communication method for interfacing between the systems, and coordinate transformation method for converting real ship coordinate attitude data to lab coordinate attitude data.

Closed-loop controller design, stability analysis and hardware implementation for fractional neutron point kinetics model

  • Vyawahare, Vishwesh A.;Datkhile, G.;Kadam, P.;Espinosa-Paredes, G.
    • Nuclear Engineering and Technology
    • /
    • v.53 no.2
    • /
    • pp.688-694
    • /
    • 2021
  • The aim of this work is the analysis, design and hardware implementation of the fractional-order point kinetics (FNPK) model along with its closed-loop controller. The stability and closed-loop control of FNPK models are critical issues. The closed-loop stability of the controller-plant structure is established. Further, the designed PI/PD controllers are implemented in real-time on a DSP processor. The simulation and real-time hardware studies confirm that the designed PI/PD controllers result in a damped stable closed-loop response.

Evaluation of electronic stability controllers using hardware-in-the-loop vehicle simulator

  • Emirler, Mumin Tolga;Gozu, Murat;Uygan, Ismail Meric Can;Boke, Tevfik Ali;Guvenc, Bilin Aksun;Guvenc, Levent
    • Advances in Automotive Engineering
    • /
    • v.1 no.1
    • /
    • pp.123-141
    • /
    • 2018
  • Hardware-in-the-loop (HiL) simulation is a very powerful tool to design, test and verify automotive control systems. However, well-validated and high degree of freedom vehicle models have to be utilized in these simulations in order to obtain realistic results. In this paper, a vehicle dynamics model developed in the Carsim Real Time program environment and its validation has been performed using experimental results. The developed Carsim real time model has been employed in the Tofas R&D hardware-in-the-loop simulator. Experimental and hardware-in-the-loop simulation results have been compared for the standard FMVSS No. 126 test and the results have been found to be in good agreement with each other. Two electronic stability control (ESC) algorithms, named the Basic ESC and the Integrated ESC, taken from the earlier work of the authors have been tested and evaluated in the hardware-in-the-loop simulator. Different evaluation methods have been formulated and used to compare these ESC algorithms. As a result, the Integrated ESC system has been shown superior performance as compared to the Basic ESC algorithm.