• Title/Summary/Keyword: ABS Brake

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Development of ABS ECU for a Bus using Hardware In-the-Loop Simulation

  • Lee, K.C.;Jeon, J.W.;Nam, T.K.;Hwang, D.H.;Kim, Y.J.
    • 제어로봇시스템학회:학술대회논문집
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    • 2003.10a
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    • pp.1714-1719
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    • 2003
  • Antilock Brake System (ABS) is indispensable safety equipment for vehicles today. In order to develop new ABS ECU suitable for pneumatic brake system of a bus, a Hardware In-the-Loop Simulation (HILS) System was developed. In this HILS, the pneumatic brake system of a bus and antilock brake component were used as hardware. For the computer simulation, the 14-Degree of Freedom (DOF) bus dynamic model was constructed using the Matlab/Simulink software package. This model was compiled and downloaded in the simulation board, where the Power PC processor was used for real-time simulation. Additional commercial package, the ControlDesk was used to monitor the dynamic simulation results and physical signal values. This paper will focus on the procedure and results of evaluating the ECU in the HILS simulation. Two representative cases, wet basalt road and $split-{\mu}$ road, were used to simulate real road conditions. At each simulated road, the vehicle was driven and stopped under the help of the developed ECU. In each simulation, the dynamical behavior of the vehicle was monitored. After enough tests in the laboratory using HILS, the parameter-tuned ECU was equipped in a real bus, which was driven and stopped in the real test field in Korea. And finally, the experiment results of ABS equipped vehicle's dynamic behavior both in HILS test and in test fields were compared.

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Braking Efficiency Calculation of Antiskid Brake System of a Fixed-Wing Aircraft (Dynamometer 시험을 통한 ABS 효율 계산)

  • Lee, Ki-Chang;Jeon, Jeong-Woo;Hwang, Don-Ha;Kom, Yong-Joo;Gu, Dae-Hyun
    • Proceedings of the KIEE Conference
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    • 2005.10b
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    • pp.222-224
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    • 2005
  • In the development of Antiskid Brake System(ABS) for a fixed-wing aircraft, the braking efficiency is the most essential parameters to evaluate the ABS, especially in slippery road conditions. The braking distance and landing distance of the aircraft depends on it. Since the ABS has been designed and implemented as a subsystem of the aircrafts, the braking performance was evaluated under dynamometer test, where the dynamometer emulates the aircraft mass. Under simulated wet road conditions, the dynamometer starts to be braked. This paper suggests practical braking efficiency calculation methods and the results and finally compares each method.

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Fatigue Damage Analysis of the Caliper Housing under ABS Mode (ABS 작동에 의한 캘리퍼하우징에 미치는 피로손상평가)

  • 김정엽;모종운
    • Transactions of the Korean Society of Automotive Engineers
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    • v.4 no.4
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    • pp.156-163
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    • 1996
  • The brakes are the most important safety-critical accident avoidance components of a motor vehicle. They must perform safely under a variety of operating conditions and must have enough strength not to fail during the life of a vehicle. Recently, anti-lock brake systems are used on more and more passenger cars. The ABS brakes modulate brake line pressure to prevent brakes from locking during braking. In this study, finite element analysis, material test for FCD45, measurement of stress and cumulative fatigue damage analysis were performed to evaluate fatigue damage of the caliper housing under ABS mode.

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The Integrated Circuit Design of Automobile ABS Interface (자동차용 ABS 인터페이스의 IC 설계)

  • Jung, Kyung-Jin;Lee, Sung-Pil;Kim, Chan;Jeon, Eui-Seok
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2003.11a
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    • pp.7-10
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    • 2003
  • ABS interface IC for automobiles was designed and their electrical properties were investigated. The voltage regulator was designed to operate in the temperature range from $-20^{\circ}\;to\;120^{\circ}C$ for automobile environment. ABS and brake signal were separated using the duty factor of same frequency or different frequencies. UVLO circuit and constant current circuit were applied for the elimination of noise.

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A Study on the Antiabrasion of the Aircraft Carbon Disk Brake (항공기의 탄소 디스크 브레이크의 내마모성에 관한 연구)

  • Lee, Jang-Hyun;Yum, Hyun-Ho;Hong, Min-Sung
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.6
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    • pp.968-975
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    • 2012
  • ABS(Anti-skid Brake System) had been developed on purpose of most effect at breaking in limited runway. An aircraft has a large amount of kinetic energy on landing. When the brakes are applied, the kinetic energy of the aircraft is dissipated as heat energy in the brake disks between the tire and the ground. The optimum value of the slip during braking is the value at the maximum coefficient of friction. An anti-skid system should maintain the brake torque at a level corresponding to this optimum value of slip. This system is electric control system for brake control valve at effective control to prevent slip and wheel speed or speed ratio. In this study we measured the thickness of the carbon disk before and after to find its wear and it shows that carbon disk brake has higher stiffness and strength than metal disk at high temperature. In addition, thermal structural stability and appropriate frictional coefficient of the carbon disk brake prove its possible substitution of metal disk brake.

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

  • 류제하;김호수
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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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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Development of Real-time Simulator for Vehicle Electric Brake System (차량 전자 제동 시스템을 위한 실시간 시뮬레이터 개발)

  • Cheon, Se Young;Choi, Seong Woong;Yang, Soon Yong
    • Journal of Drive and Control
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    • v.16 no.1
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    • pp.22-28
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    • 2019
  • This paper develops ABS braking real - time simulator to develop vehicle braking system by simulation. Recently, real-time simulation is widely used in the development of vehicles to decrease development time. In the field of electronic braking, real-time simulation is actively underway. In order to simulate electronic braking model in real time, a vehicle model, a hydraulic model, and a control S/W model are required. These models must be calculated in one platform. Therefore, in this paper, a vehicle model composed of CarSim and a hydraulic model composed of SimulationX using S/W in actual ABS controller was developed as a Simulink model base and linked with Matlab real time model. Using this real-time model, design effects of the electronic braking controller were simulated according to road surface condition to verify its operability.

Design of a Simulator and a Controller for ABS of Airplane

  • J.W. Jeon;J.H. Shin;Lee, K.C.;D.H. Hwang;Park, D.Y.;Kim, Y.J.
    • 제어로봇시스템학회:학술대회논문집
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    • 2001.10a
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    • pp.162.3-162
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    • 2001
  • The essence of ABS(Anti-skid Brake System) control is to continuously adjust brake pressure to maintain optimum brake torque. This optimum level should balance tire and runway friction its peak value, yielding maximum braking deceleration. It influences not only the deceleration and the taxing distance of an aircraft, but also the strength and the fatigue life of the landing gear. In this paper, an ABS control algorithm is developed with a dynamics model of 5-DOFD(Degree of Freedom). The algorithm is verified by simulations and the simulation results are presented. The dynamics model is simulated by the computer.

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Antl-Lock Brake System Control for Buses Based on Fuzzy Logic and a Sliding-Mode Observer

  • Park, Jong-Hyeon;Kim, Dong-Hee;Kim, Yong-Ju
    • Journal of Mechanical Science and Technology
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    • v.15 no.10
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    • pp.1398-1407
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    • 2001
  • In this paper an anti-lock brake system (ABS) for commercial buses is proposed based on a fuzzy-logic controller and a sliding-mode observer of the vehicle speed. The brake controller generates pulse width modulated (PWM) control inputs to the solenoid valve of each brake, as a function of the estimated wheel slip ratio. PWM control inputs at the brakes significantly reduce chattering in the brake system compared with conventional on-off control inputs. The sliding-mode observer estimates the vehicle speed with measurements of wheel speed, which is then sed to compute the wheel slip ratio. The effectiveness of the proposed control algorithm is validated by a series of computer simulations of bus driving, where the 14-DOF bus model is used.

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Experimental Research on Finding Best Slip Ratio for ABS Control of Aircraft Brake System (항공기용 제동장치의 ABS 제어를 위한 최적 슬립율 결정에 관한 시험적 연구)

  • Yi, Miseon;Song, Wonjong;Choi, Jong Yoon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.20 no.5
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    • pp.597-607
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    • 2017
  • The general control method for Anti-lock Brake System(ABS) is that the wheel slip ratio is observed and the braking force is controlled in real time in order to keep the wheel slip ratio under the value of the best slip ratio. When a wheel runs on the state of the best slip ratio, the ground friction of the wheel approaches the highest value. The value of best slip ratio, theoretically, is known as the value between 10 and 20 % and it is dependant on the ground condition such as dry, wet and ice. It is an important parameter for the braking performance and affects the braking stability and efficiency. In this thesis, an experimental method is suggested, which is a reliable way to decide the best slip ratio through dynamo tests simulating aircraft taxiing conditions. The obtained best slip ratio is proved its validity by results of aircraft taxiing tests.