• Title/Summary/Keyword: linear acceleration

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HYBRID ROLL CONTROL USING ELECTRIC ARC SYSTEM CONSIDERING LIMITED BANDWIDTH OF ACTUATING MODULE

  • Kim, H.J.;Lee, C.R.
    • International Journal of Automotive Technology
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    • v.3 no.3
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    • pp.123-128
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    • 2002
  • This paper presents the design of an active roll control system for a ground vehicle and an experimental study using an devised electric-actuating roll control system. Based on a three degree of freedom linear vehicle model, the controller is designed using lateral acceleration and rollrate feedback. In order to investigate the feasibility of an active control system, experimental work is carried out using a hardware-in-the-loop (Hil) setup which has been constructed by the devised electric-actuating system and the full vehicle model including tire characteristics. The performance is evaluated by an experiment using the Hil setup with limited bandwidth. Finally, in order to enhance the control performance in the transient region, a hybrid control strategy is proposed and evaluated.

In-plane Vibration Analysis for an Axially Moving Membrane (축방향으로 움직이는 박막의 면내 진동해석)

  • 정진태;신창호;김원석
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.12 no.3
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    • pp.221-227
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    • 2002
  • The longitudinal and lateral in-plane vibrations of an axially moving membrane are investigated when the membrane has translating acceleration. By extended Hamilton's principle, the governing equations are derived. The equations of motion for the in-plane vibrations are linear and coupled. These equations are discretized by using the Galerkin approximation method after they are transformed into the variational equations, j.e., the weak forms so that the admissible functions can be used for the bases of the in-plane deflections. With the discretized equations for the in-plane vibrations, the natural frequencies and the time histories of the deflections are obtained.

Design of dynamic Characteristic of Seat using Estimated Biomechanical Model (인체 진동 모델을 이용한 시트 동적 설계)

  • 조영건;윤용산;박세진
    • Journal of KSNVE
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    • v.10 no.5
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    • pp.811-818
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    • 2000
  • This paper deals with the design of a car seat for enhancing dynamic ride quality using a Biomechanical Model that was developed from the measured whole-body vibration characteristic. For evaluation of seat ride quality, the z-axis acceleration of floor as an input of biomechanical model was measured on a driving passenger car at highway and national road. Form the floor signal and the estimated biomechanical model, overall ride value evaluated by parameter study of seat stiffness and damping. The result shows that overall ride value decreases as the seat damping increases and the sear stiffness decreases. A lot of polyurethane foams were manufactured and tried to evaluate dynamic ride quality of a seat. It is found that stiffness and damping of a seat show a linear relationship, which means the stiffness and damping are not independent each other, So the optimal seat parameters within practically achievable space are determined.

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Optimum Path Planning for Mechanical Manipulators (기계적 로보트팔을 위한 최적 경로 설계)

  • Kim, Tae-San;Bae, Jun-Kyung;Park, Chong-Kug
    • Proceedings of the KIEE Conference
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    • 1988.07a
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    • pp.941-944
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    • 1988
  • To assure a successful completion of an assigned task without interruption, the hand of mechnical manipulator often travels along a preplanned path. This paper presents a method of obtaining a time sechdule of velocities and acceleration along the path, under the constraints. Because of the involvement of a linear performance index and a largr number of nonlinear constraints, the "method of approximate programming (AMP)" is applied. To overcome the false solutions AMP is modified. To reduce the computing time, a "direct approximate programming algorithm (DAPA)" is developed.

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Implementation of Cruise Control System using Fuzzy Logic Controller (퍼지 로직 컨트롤러를 이용한 차량 정속 주행 시스템의 구현)

  • Kim, Young-Min;Lee, Joo-Phil;Chong, Hyung-Hwan;Yim, Young-Doe;Lee, Joon-Tark
    • Proceedings of the KIEE Conference
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    • 1997.07b
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    • pp.491-494
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    • 1997
  • In this paper, we suppose a fuzzy logic controller for cruise control of vehicle. Generally, fuzzy logic controller is known as a controller which can be coped with a non-linear and a complex system. The proposed fuzzy logic controller consists of three input variables; that is, a desired speed, a current vehicle speed, and a current acceleration, and one output variable, throttle angle. The supposed fuzzy logic controller is for engine speed control system is implemented on 80586 microprocessor with DT-2801.

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A Final-Phase Optimal Guidance Law for Highly-Maneuvering BTT Missiles (고기동 BTT 미사일의 최적 종말 유도 법칙)

  • Hong, Jin-Woo;Yeom, Joon-Hyung;Song, Seong-Ho;Ha, In-Joong
    • Proceedings of the IEEK Conference
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    • 2006.06a
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    • pp.853-854
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    • 2006
  • Due to a recently developed approach to autopilot controller design for highly-maneuvering BTT (bank-to-turn) missiles, we now can derive explicitly the final-phase optimal guidance (OG) law considering the autopilot dynamics through direct use of the well-known linear optimal control theory. The proposed OG law can decrease the miss distance (MD) remarkably with small acceleration and roll rate profile at the time of interception.

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A Vertical Line Following Guidance Law Design (수직면 직선추종유도법칙 설계)

  • Whang, Ick-Ho;Cho, Sung-Jin
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.59 no.7
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    • pp.1309-1313
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    • 2010
  • In this paper, we propose a novel guidance law for controlling an UAV(Unmanned Air-Vehicle) to follow a reference line in vertical plane. A kinematics model representing the relative motion of the UAV to the reference line is derived. And then LQR(Linear Quadratic Regulator) theory is applied to the model to derive the VLFG(Vertical Line Following Guidance) law. The resultant guidance law forms a gain-scheduling controller scheduled by a simple parameter $\sigma$ which is a function of the UAV's velocity, axial acceleration, gravity, and the slope of the reference line. Also derived is a stability condition for the $\sigma$ variation based on Lyapunov theory. Simulation results show that the proposed guidance law can be applied effectively to UAV guidance algorithm design.

A Numerical Calculation of Eddy Current Field by Applying FEM and BEM Alternately (유한요소법과 경계요소법의 교호적용에 의한 와전류장 해석)

  • Im, Jae-Won
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.49 no.7
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    • pp.457-461
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    • 2000
  • The finite element method (FEM) is suitable for the analysis of a complicated region that includes nonlinear materials, whereas the boundary element method (BEM) is naturally effective for analyzing a very large region with linear characteristics. Therefore, considering the advantages in both methods, a novel algorithm for the alternate application of the FEM and BEM to magnetic field problems with the open boundary is presented. This approach avoids the disadvantages of the typical numerical methods with the open boundary problem such as a great number of unknown values for the FEM and non-symmetric matrix for the Hybrid FE-BE method. The solution of the overall problems is obtained by iterative calculations accompanied with the new acceleration method.

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A Numerical Calculation of Open Boundary Problem by Applying FEM and BEM Alternately (유한요소법과 경계요소법의 교호적용에 의한 무한영역해석)

  • Im, Jae-Won
    • Proceedings of the KIEE Conference
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    • 1999.07a
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    • pp.130-132
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    • 1999
  • The finite element method (FEM) is suitable for the analysis of a complicated region that includes nonlinear materials, whereas the boundary element method (BEM) is naturally effective for analyzing a very large region with linear characteristics. Therefore, considering the advantages in both methods, a novel algorithm for the alternate application of the FEM and BEM to magnetic field problems with the open boundary is presented. This approach avoids the disadvantages of the typical numerical methods with the open boundary problem such as a great number of unknown values for the FEM and non-symmetric matrix for the Hybrid FE-BE method. The solution of the overall problems is obtained by iterative calculations accompanied with the new acceleration method.

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Identification of Structural Dynamic Systems (구조물의 동특성 추정방법에 관한 연구)

  • 윤정방;소봉정선
    • Computational Structural Engineering
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    • v.2 no.2
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    • pp.113-119
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    • 1989
  • Methods for identification of modal properties of linear structures are presented. The extended Kalman filtering technique is employed. The state equation is formulated by two different ways, namely by the time domain and frequency domain approaches. Verifications are carried out by using the simulated records of ground acceleration and structural response. Then the techniques are applied to the estimation of modal parameters of a scaled model for a 3-story building which is installed on a shaking table.

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