• Title/Summary/Keyword: Lateral actuator

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Design of Braille cell Setting Actuators for the Application in the Braille Mouse Concept

  • Nobels, Tiene;Allemeersch, Frank;Hameyer, Kay
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • v.4B no.1
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    • pp.12-19
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    • 2004
  • Refreshable Braille displays have already been developed in the past, but they remain quite bulky and expensive. Small displays contain only a single or a few Braille cells, with pins pushing into the fingertips. However, they are not as successful as larger displays because the skin is more sensitive to lateral movement than to orthogonal pressure. This, paper presents the design of linear electromagnetic actuators, which allows a considerable reduction in size and cost for such refreshable Braille displays. Different actuator concepts are compared. A new actuator is proposed and optimised by means of finite element simulations, which are verified with measurements on a prototype.

Active Control Experiments on High-speed Elevator Vibrations (고속 엘리베이터 능동진동제어 실험)

  • Kim, Ki-Young;Kwak, Moon-K.;Baek, Kwang-Hyun
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.21 no.4
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    • pp.325-332
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    • 2011
  • This paper is concerned with the active control experiments on elevator vibrations by means of the active roller guide. To this end, a roller guide was designed using a voice-coil actuator and linear guide. A simple proportional control algorithm combined with the band-pass filter was implemented using the DSP. Based on the initial experiments, a new control system which can handle lateral and front-back vibrations of elevator was built and tested using the elevator test tower. The experimental results show that the elevator vibrations are reduced by the active control technique.

Kalman Filter Based Resilient Cyber-Physical System and its Application to an Autonomous Vehicle (칼만필터를 이용한 사이버 물리 시스템의 자율 복원성 확보 기법 및 자율주행차량 적용 연구)

  • Kim, Jae-Hoon;Kim, Dong-Gil;Lee, Dong-Ik
    • IEMEK Journal of Embedded Systems and Applications
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    • v.14 no.5
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    • pp.239-247
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    • 2019
  • Recently, successful attacks on cyber-physical systems have been reported. As existing network security solutions are limited in preventing the system from malicious attacks, appropriate countermeasures are required from the perspective of the control. In this paper, the cyber and physical attacks are interpreted in terms of actuator and sensor attacks. Based on the interpretation, we suggest a strategy for designing Kalman filters to secure the resilience and safety of the system. Such a strategy is implemented in details to be applied for the lateral control of autonomous driving vehicle. A set of simulation results verify the performance of the proposed Kalman filters.

Empirical Modeling of Steering System for Autonomous Vehicles

  • Kim, Ju-Young;Min, Kyungdeuk;Kim, Young Chol
    • Journal of Electrical Engineering and Technology
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    • v.12 no.2
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    • pp.937-943
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    • 2017
  • To design an automatic steering controller with high performance for autonomous vehicle, it is necessary to have a precise model of the lateral dynamics with respect to the steering command input. This paper presents an empirical modeling of the steering system for an autonomous vehicle. The steering system here is represented by three individual transfer function models: a steering wheel actuator model from the steering command input to the steering angle of the shaft, a dynamic model between the steering angle and the yaw rate of the vehicle, and a dynamic model between the steering command and the lateral deviation of vehicle. These models are identified using frequency response data. Experiments were performed using a real vehicle. It is shown that the resulting identified models have been well fitted to the experimental data.

The Implementation of Attitude Control for A Radiocontrolled Airplane (무인 비행기의 자세제어 구현)

  • Kim, Jong-Hun;Yang, Seung-Hyun;Lee, Seok-Won;Jung, Cha-Keun
    • Proceedings of the KIEE Conference
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    • 2001.07d
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    • pp.2234-2236
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    • 2001
  • This paper describes an implementation of a radiocontrolled airplane attitude control. To obtain the model of motion, stabilizing and control coefficients, we derive the related paramaters from aerodynamics, propulsion, gravity, wind correction and atmosphere. In this model, after separating longitudinal axis and lateral axis, we can get longitudinal axis model and lateral axis model by using actuator and dynamic characteristics of engine. From these two models, we experiment two divided parts-linear part, and nonlinear part.

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Utilization of wheel derailment test facilities (차륜탈선 시험설비의 활용방안)

  • Ham, Young-Sam;You, Won-Hee
    • Proceedings of the KSR Conference
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    • 2011.05a
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    • pp.1128-1133
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    • 2011
  • This is a testing equipment system to analyze variation of creep force according to wheel-rail tread profile, running speed of vehicle, vertical and lateral force, wheel/rail contact point, attack angle and so on. The creep force affect vehicle derailment, especially climbing derailment. This system is composed of main frame, wheelset and rail disks driver, hydraulic actuator, controller, environmental chamber, safety system and so on.

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Capacity of Concrete Filled Carbon Tube Columns Based on the Comparison of Ductility and Energy Dissipation Capacity (연성도 및 에너지 소산능력 비교에 따른 콘크리트충전 탄소섬유튜브 기둥의 성능)

  • Lee, Kyoung-Hun;Hong, Won-Kee;Lee, Young-Hak;Kim, Hee-Cheul
    • Journal of the Earthquake Engineering Society of Korea
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    • v.11 no.1 s.53
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    • pp.29-35
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    • 2007
  • Flexural capacity estimation test of concrete filled carbon tube (CFCT) column under the cyclic lateral load was carried out in this study. Thickness of carbon tube and winding angles of carbon fiber were chosen as test parameters and two types of column with square and circular sections were manufactured. To act axial and lateral load, three dynamic actuators were used and all specimens were made with actual size. Flexural stiffness, ability of deformation, energy dissipation capacity and ductility behavior. of CFCT column were analyzed with test data.

Development of the Virtual Driving Environment for the AWS ECU Test Platform of the Bi-modal Tram (저상굴절 궤도차량의 AWS ECU 테스트 플랫폼을 위한 가상 주행환경 개발)

  • Choi, Seong-Hoon;Park, Tea-Won;Lee, Soo-Ho;Moon, Kyung-Ho
    • Proceedings of the KSR Conference
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    • 2007.11a
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    • pp.283-290
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    • 2007
  • A bi-modal tram has been developed to offer an advanced transportation service compared with existing vehicles. The All-Wheel-Steering system is applied to the bi-modal tram to satisfy the required steering performance because the bi-modal tram has extended length and articulated mechanism. An ECU for the steering system is essential to steer wheels on 2nd and 3rd axles by the specific AWS algorithm with the prescribed driving condition. The Hardware-In-the-Loop Simulation(HILS) system is planned for the purpose of evaluating the steering system of the bi-modal tram. There are kinematic links with the hydraulic actuator to steer wheels on each 2nd and 3rd axles and also same steering mechanism as the actual vehicle is in the HILS system. Controlling the movement of hydraulic actuator which reflects the lateral steering reaction force on each wheel is the key to realize the HILS system, but the reaction force is continuously changed according to various driving conditions. Therefore, the simulation through the multi-body dynamics model is used to obtain the required forces.

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The NF-l6D VISTA Simulation System

  • Siouris, George M.
    • Transactions on Control, Automation and Systems Engineering
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    • v.4 no.2
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    • pp.114-123
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    • 2002
  • Called VISTA (Variable-stability In-flight Simulator Test Aircraft), the one-of-a-kind NF-l6D has a simulation system that can mimic several aircraft. Though housed in an F-l6 Fighting Falcon airframe, VISTA can also act like the F-15 Eagle or the Navy's F-14 Tomcat. More importantly, such flexibility allows for improved training and consolidation of some sorties. Consequently USAF Test Pilot School students will have an opportunity to learn how to test future integrated cockpits. In this paper we will use the multiple model adaptive estimation (MMAE) and the multiple model adaptive controller (MMAC) techniques to model the aircraft's flight control system containing the longitudinal and lateral-directional axes. Single and dual actuator and sensor failures will also be included in the simulation. White Gaussian noise will be included to simulate the effects of atmospheric disturbances.

A Mathematical Approach for Modal Frequency Analysis in Actuators (운동방정식 유도에 의한 액추에이터 모드 주파수 분석)

  • Lee, Kyung Taek
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.23 no.6
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    • pp.537-545
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    • 2013
  • In this paper, the vibration for actuators having lens module, confined to lateral and torsional directions of suspensions, is described by mathematically analyzing its suspension configuration and motion. In order to prove the accuracy of this result, it is compared to a finite element analysis. Also it is shown that modal frequencies can be modified by changing design parameters in mathematical motion expressions.