• 제목/요약/키워드: Full-vehicle Dynamics Model

검색결과 63건 처리시간 0.026초

7 DOF 차량 모델을 이용한 자동차 현가장치 동력학 해석 및 시뮬레이션에 관한 연구 (Dynamics Analysis and Simulation of a Passive Suspension System Using 7 DOF Full Car Model)

  • 노태수;정길도;홍동표
    • 한국자동차공학회논문집
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    • 제5권2호
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    • pp.31-41
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    • 1997
  • Equations of motion for a 7 DOF full car model is developed in detail and used for the design of LQR based active suspension system. The frequency response to road disturbance input and the motion of a car passing unequal bumps were used to analyzed the dynamic characteristics of the 7 DOF full car with passive or active suspensions. The resulting linear equations of motion may be usefull in designing other types of active suspension.

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상용차용 ABS ECU의 성능분석을 위한 HILS 시스템 개발 (Development of HILS System for Performance Analysis of the ABS ECU for Commercial Vehicles)

  • 황돈하;이기창;전정우;김용주;조정목;조중선
    • 제어로봇시스템학회논문지
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    • 제8권10호
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    • pp.898-906
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    • 2002
  • Antilock Brake System (ABS) is designed to prevent wheels from being locked-up under emergency braking of a vehicle. Therefore it improves directional stability of the vehicle, shortens stopping distance, and enhances maneuvering during braking, regardless of road conditions. Hardware In-the-Loop Simulation (HILS) is an effective tool for design Performance evaluation and test of vehicle subsystems such as ABS, active suspension, and steering systems. This paper describes a HILS model for ABS/ ASR(Acceleration Slip Regulation) system applications. A fourteen degrees-of-freedom vehicle dynamics model is simulated in an alpha-chip processor board. The proposed HILS system is tested with a basic ABS control algorithm. The design and implementation of HILS system for the ABS ECU(Electronic Control Unit) development of commercial vehicle are presented. The results show that the proposed HILS system can be used to test the performance, stability, and reliability of a vehicle under braking.

The effects of the circulating water tunnel wall and support struts on hydrodynamic coefficients estimation for autonomous underwater vehicles

  • Huang, Hai;Zhou, Zexing;Li, Hongwei;Zhou, Hao;Xu, Yang
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제12권1호
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    • pp.1-10
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    • 2020
  • This paper investigates the influence of the Circulating Water Channel (CWC) side wall and support struts on the hydrodynamic coefficient prediction for Autonomous Underwater Vehicles (AUVs) experiments. Computational Fluid Dynamics (CFD) method has been used to model the CWC tests. The hydrodynamic coefficients estimated by CFD are compared with the prediction of experiments to verify the accuracy of simulations. In order to study the effect of side wall on the hydrodynamic characteristics of the AUV in full scale captive model tests, this paper uses the CWC non-dimensional width parameters to quantify the correlation between the CWC width and hydrodynamic coefficients of the chosen model. The result shows that the hydrodynamic coefficients tend to be constant with the CWC width parameters increasing. Moreover, the side wall has a greater effect than the struts.

날갯짓 비행 로봇의 세로방향 비행 동역학 모델링 및 안정성 해석 (Longitudinal Flight Dynamic Modeling and Stability Analysis of Flapping-wing Micro Air Vehicles)

  • 김중관;한종섭;김호영;한재흥
    • 제어로봇시스템학회논문지
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    • 제21권1호
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    • pp.1-6
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    • 2015
  • This paper investigates the longitudinal flight dynamics and stability of flapping-wing micro air vehicles. Periodic external forces and moments due to the flapping motion characterize the dynamics of this system as NLTP (Non Linear Time Periodic). However, the averaging theorem can be applied to an NLTP system to obtain an NLTI (Non Linear Time Invariant) system which allows us to use a standard eigen value analysis to assess the stability of the system with linearization around a reference point. In this paper, we investigate the dynamics and stability of a hawkmoth-scale flapping-wing air vehicle by establishing an LTI (Linear Time Invariant) system model around a hovering condition. Also, a direct time integration of full nonlinear equations of motion of the flapping-wing micro air vehicle is conducted to see how the longitudinal flight dynamics appear in the time domain beyond the reference point, i.e. hovering condition. In the study, the flapping-wing air vehicle exhibited three distinct dynamic modes of motion in the longitudinal plane of motion: two stable subsidence modes and one unstable oscillatory mode. The unstable oscillatory mode is found to be a combination of a pitching velocity state and a forward/backward velocity state.

다물체동역학기법을 이용한 고급버스의 전차량 시뮬레이션과 시험의 매칭 (Matching Simulations with Tests of Cruise Bus Using Multi-body Dynamics Technology)

  • 최소해;박성준;이정한;유완석;손정현
    • 한국자동차공학회논문집
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    • 제18권6호
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    • pp.14-22
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    • 2010
  • In this study, a large bus is tested for measuring the steering response based on the slarom test and step steer test. A full car model by using ADAMS/Car is established for computer simulation. For bus modeling, user defined templates are made and used in the simulation. Simulation results according to the slarom and step steer test are compared to the physical experiments, in which several sensors are installed to measure vehicle responses. The results obtained from the comparison show a good agreement with regard to the vehicle velocity and steering angle.

Estimation of Hydrodynamic Derivatives of Full-Scale Submarine using RANS Solver

  • Nguyen, Tien Thua;Yoon, Hyeon Kyu;Park, Youngbum;Park, Chanju
    • 한국해양공학회지
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    • 제32권5호
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    • pp.386-392
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    • 2018
  • It is necessary to predict hydrodynamic derivatives when assessing the maneuverability of a submarine. The force and moment acting on the vehicle may affect its motion in various modes. Conventionally, the derivatives are determined by performing captive model tests in a towing tank or applying a system identification method to the free running model test. However, a computational fluid dynamics (CFD) method has also become a possible tool to predict the hydrodynamics. In this study, virtual captive model tests for a full-scale submarine were conducted by utilizing a Reynolds-averaged Navier-Stokes solver in ANSYS FLUENT version 18.2. The simulations were carried out at design speed for various modes of motion such as straight forward, drift, angle of attack, deflection of the rudder, circular, and combined motion. The hydrodynamic force and moment acting on the submarine appended rudders and stern stabilizers were then obtained. Finally, hydrodynamic derivatives were determined, and these could be used for evaluating the maneuvering characteristics of the submarine in a further study.

차량의 조종 안정성 향상을 위한 전륜 범프 스터어 최적화 (Optimization of front Bump Steer for Improving Vehicle Handling Performances)

  • 서권희;이윤기;박래석;박상서;윤희석
    • 한국정밀공학회지
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    • 제17권2호
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    • pp.80-88
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    • 2000
  • This paper presents a method to optimize the bump steer characteristics (the change of toe angle with vertical wheel travel) with respect to hard points in the double wishbone front suspension of the four-wheel-drive vehicle using the design of experiment, multibody dynamics simulation, and optimum design program. Front and rear suspensions are modeled as the interconnection of rigid bodies by kinematic joints and force elements using DADS. The design variables with respect to the kinematic characteristics are obtained through the experimental design sensitivity analysis. An object function is defined as the area of absolute differences between the desired and experimental toe angle. By the design of experiment and regression analysis, the regression model function of bump steer characteristics is extracted. The design variables that make the toe angle optimized are selected using the optimum design program DOT. The lane change simulations and tests of the full vehicle models are implemented to evaluate the improvement of vehicle handling performances by the optimization of front bump steer characteristics. The results of the lane change simulations show that the vehicle with optimized bump steer has the weaker understeer tendency than the vehicle with initial bump steer.

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자기부상열차/가이드웨이 동적상호작용 해석 (Analysis of Dynamic Interaction Between Maglev Vehicle and Guideway)

  • 김기정;한형석;양석조
    • 대한기계학회논문집A
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    • 제37권12호
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    • pp.1559-1565
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    • 2013
  • 고가가이드웨이를 주행하는 상전도흡인식 자기부상열차(EMS-Type Maglev)는 가이드웨이의 유연성으로 인하여 전자석 현가시스템과 동적 상호작용을 일으켜 부상공극에 영향을 미친다. 특히, 전체 건설비를 줄이기 위하여 경량화 가이드웨이를 지향하면서 시스템 설계단계부터 차량과 가이드웨이 사이의 동적상호작용 해석에 의한 심도 있는 부상공극 분석이 더욱 필요하다. 본 논문에서는 보다 정교한 차량/가이드웨이 동적상호작용 해석모델이 제안된다. 제안된 모델은 가상시제 기반의 3 차원 전체차량, 모달합성법에 의한 유연 가이드웨이 및 피드백 제어기가 포함된 부상전자석의 동적 모델들이 하나로 통합된 것이다. 제안된 모델을 도시형 자기부상열차에 적용하여 차량의 속도와 레일조도가 부상공극 및 가이드웨이에 미치는 영향을 분석하였다.

Handling Quality Improvements of Fly-By-Wire Helicopter using Combined Model Following Controller with Decoupler

  • Lee, Jangho;Kim, Eung-Tai;Ryu, Hyeok;Shim, Hyunchul
    • International Journal of Aeronautical and Space Sciences
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    • 제18권2호
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    • pp.378-387
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    • 2017
  • The combined model following control (MFC)-decoupler system is employed for a full authority fly-by-wire utility helicopter to enhance handling qualities. The MFC, which governs the vehicle to follow the prescribed model, is widely employed for modern helicopters. However, it may not be sufficient as helicopters often suffer significant cross coupling. The coupled responses between control axes of a helicopter increase the pilot's work load and may degrade handling qualities. As the decoupler is introduced to the MFC, the combined MFC-decoupler effectively solves the coupling problems and enhances handling qualities. The proposed system is verified via the handling qualities prediction using the mathematical dynamics model. The analysis results are confirmed through the piloted simulation.

우등버스용 MR 댐퍼의 실험적 모델링 (Experimental Modeling of MR Damper for Cruise Bus)

  • 손정현;전철웅
    • 대한기계학회논문집A
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    • 제35권8호
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    • pp.863-867
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    • 2011
  • 본 논문에서는 우등버스용 MR 댐퍼의 특성 시험 결과를 분석하고, 비선형 히스테리시스 특성을 모델링할 수 있는 실험적 모델링이 제시된다. MR 댐퍼의 인가전류에 따른 실험적 모델을 구성하고, 매트랩의 최적설계 툴 박스를 이용하여 계수를 규명한다. 우등버스의 전차량 시뮬레이션을 통하여 차량동역학 해석용 MR 댐퍼의 실험적 모델의 유용성을 검증한다.