• Title/Summary/Keyword: rotational

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Sliding Mode Control of Rotational Inverted Pendulums Using Output Feedback Compensator (출력 피드백을 이용한 회전형 역진자의 슬라이딩 모드 제어)

  • Ha, Jong-Heon;Choi, Joeng-Ju;Kim, Jong-Shik
    • Proceedings of the KSME Conference
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    • 2000.04a
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    • pp.469-474
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    • 2000
  • A sliding mode control method using the parameterization of both the hyperplane and the compensator for output feedback and reduced observer is presented for rotational inverted pendulums. This control strategy overcomes the problem of unattainable velocity state which is resulted from severe noise of analogue sense and constructs numerical algorithms designs of dynamic output feedback sliding mode hyperplane and controller. The result of the experiment shows the superior performance compared with the LQ controller and the robustness with respect to both tapping disturbances and certain initial conditions.

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Three-dimensional Laminar Flow Past a Rotating Cylinder (회전하는 원형 실린더 주위의 층류 유동장에 관한 수치적 연구)

  • Lee, Yong-Suk;Yoon, Hyun-Sik;Doo, Jeong-Hoon;Ha, Man-Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.33 no.11
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    • pp.827-833
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    • 2009
  • The present study numerically investigates three-dimensional laminar flow past a rotating circular cylinder placed in a uniform stream. For the purpose of a careful analysis of the modification of flow by the effect of the rotation on the flow, numerical simulations are performed at a various range of rotational coefficients ($0{\leq}{\alpha}{\leq}2.5$) at one Reynolds number of 300. As ${\alpha}$ increases, flow becomes stabilized and finally a steady state beyond the critical rotational coefficient. The 3D (three dimensional) wake mode of the stationary cylinder defined at this Reynolds number has been disorganized according to ${\alpha}$, which were observed by the visualization of 3D vortical structures. The variation of the Strouhal number is very weak when the wake pattern is changed according to the rotational coefficient. As ${\alpha}$ increases, the lift increases, whereas the drag decreases.

Effect of Centrifugal Casting Parameters on The Distribution of Primary Si Particles of B390 Aluminum Alloy (B390 알루미늄 합금의 초정Si 입자분포에 미치는 원심주조 공정인자의 영향)

  • Park, Jeong-Wook;Kim, Heon-Joo
    • Journal of Korea Foundry Society
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    • v.28 no.1
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    • pp.25-30
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    • 2008
  • To develop a functionally graded microstructure of cylindrical liner, effect of centrifugal casting parameters such as pouring temperature of hyper-eutectic Al-Si alloy melt, mold pre-heating temperature, and rotational frequency of mold on distribution of primary Si particles across wall thickness were investigated. Segregation tendency of Si particles toward inner side of cylindrical liner increased as the increase of rotational frequency of mold, pouring temperature of melt and mold pre-heating temperature. Especially, distribution density of primary Si particles within 1.5 mm from inner surface of cylindrical liner was above 35% under the centrifugal casting condition of $750^{\circ}C$ melt pouring temperature, $300^{\circ}C$ mold pre-heating temperature, and 2500 rpm mold rotational frequency.

A Study on the Slippage between a Moving Web and a Roller (이송중인 웹과 롤러의 슬립에 관한 연구)

  • Kwon, Soon-Oh;Shin, Kee-Hyun
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.1542-1547
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    • 2003
  • Air entrainment can become a significant problem in a web handling process. The development of air film between a web and an idle roller can cause a reduction of traction and traction coefficient, by which a slip is occurrred. Computational and experimental study was carried out to describe the slippage of an idle roller for given operating conditions, tension and web velocity. An extended mathematical model to find out a slip condition was developed by using the models of air film height, dynamic traction coefficient, and torque balance of a rotational roller. And by using the extended model, a mechanism to define the slippage between the roller and the moving web was suggested. The results of simulation and experiment showed that the extended dynamic model could properly characterize the rotational motion of the idle roller by considering dynamic traction coefficient. By examining the rotational motion of the idle roller with web dynamics(speed), the mechanism to define al slip condition between the roller and the web was found to be effective.

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Swing-up control of the 2-link rotational pendulum (2축 회전진자의 스윙업제어)

  • 양동훈;유기정;고영길;홍석교
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.371-371
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    • 2000
  • A strategy for the swing-up control according to states of the 2-link rotational pendulum is proposed. The proposed controller consists of two modes of control such as divergence mode and stabilization mode. When the controller is in divergence mode, control input is generated using sinusoidal and signum function to make the first and second links reach the bottom and top positions, respectively. After the controller finishes divergence mode, stabilization mode is initiated to keep the pendulum around the top position using pole-placement method. Dynamic models including actuator dynamics are obtained using coordinate changes at each control mode. Simulation results are given to show the effectiveness of the proposed method.

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A Study on the 3-DOF Attitude Control of Free-Flying Vehicle (자유 비행체의 3자유도 자세제어에 관한 연구)

  • 박덕기;박문수;김병두;정원재;조성민;홍석교
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.92-92
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    • 2000
  • Helicopter offer the signigicant advantage over traditional air vehicles, in that the provide extended maneuverability, such as vertical climb, hovering, longitudinal and lateral flight, hovering turns and bank turns. But helicopter have the strong cross couplings and nonlinearities for each lateral, longitudinal and rotational motion mutually. However, it is possible to ignore this couplings for the hovering condition, so using this properties we can control the attitude of helicopter. That is, by implementing the dynamic of each rotational axis(roll, pitch, yaw) of independent mutually, 3-DOF(degree of Freedom) attitude control for the helicopter is possible. In this paper, we identify decoupled input-coutput relations of each three rotational axis about the helicopter mounted on the 3-DOF gimbal by experiment, and on these basis implement 3-DOF attitude controller using the PID control method.

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Experimental Investigation for Rotational Error Motion Simulation of Inherently Compensated Aerostatic Journal Bearing (자성보상형 공기정압 저널베어링의 회전운동정밀도 시뮬레이션을 위한 실험적 고찰)

  • Shim, Jongyoup;Hwang, Jooho;Park, Chun-Hong
    • Journal of the Korean Society for Precision Engineering
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    • v.32 no.2
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    • pp.135-140
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    • 2015
  • It is an important thing for a designer to simulate and predict the performance of a spindle and a rotary table. In addition to the general performance such as static stiffness, the error motion performance information is beneficial to the designer in many cases. However for an aerostatic bearing the fluid film physical status should be calculated in order to simulate those performances and the calculation time is another obstacle for a simple performance simulation. In this paper the investigation on experiment and simulation is performed in order to find a more effective simulation method for the rotational error motion.

Free Vibrations of Tapered Beams with General Boundary Conditions and Tip Masses (끝단 질량과 일반적인 단부조건을 갖는 변단면 보의 자유진동)

  • 오상진;이병구;박광규;이종국
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.11a
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    • pp.802-807
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    • 2003
  • The purpose of this paper is to investigate the free vibration characteristics of tapered beams with translational and rotational springs and tip masses at the ends. The beam model is based on the classical Bernoulli-Euler beam theory. The governing differential equation for the free vibrations of linearly tapered beams is solved numerically using the corresponding boundary conditions. Numerical results are compared with existing solutions by other methods for cases in which they are available. The lowest three natural frequencies are calculated over a wide range of non-dimensional system parameters: the translational spring parameter, the rotational spring parameter, the mass ratio and the dimensionless mass moment of inertia.

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A Numerical Study on the Flowfield of a Cyclone Separator for Oil Droplets (오일입자 원심분리기 유동장의 수치해석적 연구)

  • Kim, Sang-Dug
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.23 no.4
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    • pp.36-41
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    • 2015
  • The cyclone separator is a simple device, which causes the centrifugal separation of materials such as droplets or particles in a fluid stream. The cyclone separator utilizes the energy obtained from fluid pressure and linear motion to create rotational fluid motion. This rotational motion leads the materials suspended in the fluid to separate from the fluid quickly due to the centrifugal force. The rotation is produced by the tangential or involuted introduction of fluid into the vessel. These materials may be droplets of fuel in blow-by gas through an engine. Droplets suspended in the feed liquid may separate according to size, shape, or density. And the change of part dimension in a cyclone separator can yield the its performance variation. The current study shows the influence of design parameters on the performance of a cyclone separator for blow-by gas.

Rotational Diffusion of Rhodomine 6G Molecule -Effect of Dielectric Friction in Alcohol Solvents- (Rhodamine 6G 분자의 회전 확산 -알코올 용매에서의 유전 마찰 효과-)

  • 고동섭
    • Korean Journal of Optics and Photonics
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    • v.4 no.3
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    • pp.338-346
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    • 1993
  • The rotational reorientation times of rhodamine 6G molecule were measured using a time-correlated single photon counting method. To explain the deviation of observed rotational reorientation times in alcohol solvents from the prediction of hydrodynamic model, the contribution of dielectric friction was considered. And the values of transition dipole moments in ground and excited states were estimated through the dielectric friction and the static spectroscopic data.

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