• Proceedings of the KIPE Conference
• /
• 2006.06a
• /
• pp.501-503
• /
• 2006

최근 산업 분야에서 리니어모터는 고속, 고정밀도의 요구사항에 따라 회전 모터와 볼 스크류, 벨트를 이용한 직선구동방식보다 빠르고 정확하며, 효율이 높기 때문에 활발히 이루어지고 있다. 리니어모터 중에서 선형 브러시리스 직류 전동기(LBLDCM)는 다른 리니어모터에 비해 소형, 경량이 가능하고, 저속 및 고속의 운전이 용이하며, 기계 가공 정도보다는 엔코더 등과 같은 위치 결정 응용 분야에 적합하며 본 연구에서 사용된 LBLDCM은 코일 가동형으로 영구 자석에 의해 발생된 자계와 가동자 코일에 흐르는 전류 사이에 작용하는 힘을 이용하게 된다. 이와 같은 LBLDCM을 응용분야에 적용하기 위해서는 구동 중에 속도가 변하는 지점에서 발생하는 진동을 줄여야 하며 목표지점까지의 정확한 위치 제어가 필수적이다. 따라서, 본 연구에서는 다양한 속도 프로파일에 따른 진동에 대해 비교 분석한 후, 이동거리에 따른 적합한 속도 프로파일에 대해 알아보았고, 그 결과를 토대로, 목표지점까지의 위치 오차를 저감하면서 정밀한 위치 제어에 적합한 프로파일을 제시하였다.

• Journal of Industrial Technology
• /
• v.21 no.B
• /
• pp.117-123
• /
• 2001

In a modern control field, a control engineer who has theoretical backgrounds with some practical knowledge is demanded. That is to say, an engineer who can understand and operate the various parts such as modeling, simulation, system analysis, signal processing, statistics, and hardware is required. In order to prove the theoretical backgrounds and operate various hardwares, a lot of experimental devices for students are designed in universities. Since the conventional experimental devices are manufactured abroad and the prices of the devices are too high, it is difficult to have. If a low cost experimental device can be developed, it will be very useful for a control engineering education. In Ibis paper, an experimental rig which has two control inputs and three sensor outputs to control the end point of a flexible beam is designed and manufactured. This rig can be used for a control field education.

• Journal of Industrial Technology
• /
• v.19
• /
• pp.15-23
• /
• 1999

Active damping system is generally used for the vibration suppression and precise motion control for the flexible structure. This application can be easily found on the space structure and driving mechanism of optical storage devices. Although a control system using the flexible structure has many advantages over using rigid mechanism in driving energy saving, system weights, and etc., more complex and precise control strategies are required. A position control system using flexible structure and the concept of active damper is designed and manufactured, which is driven by slide DC motor and moving coil motor located at the tip of the flexible beam. Dynamic characteristics of this system are investigated by analytic and experimental ways. By the comparison of those two results, a nominal reference model for this system is proposed.

• Journal of Industrial Technology
• /
• v.20 no.B
• /
• pp.125-130
• /
• 2000

Heat dissipation technology using flow resonant phenomenon is a kind of new concept in heat transfer area. A vibration exciter is needed to generate air turbulence which has the natural shedding frequency of heat system. A mechanical vibrating device for the air flow oscillation is introduced, which is driven by a moving coil actuator. An analytical dynamic model for this mechanical vibration exciter is presented and its validity is verified by the comparison with experimental data. Values of some unknown system parameters in the analytic model are estimated through the system identification approach. Based on this mathematical model, a high bandwidth vibration phase, it turns out the high modal resonant characteristics of vibrating plate are the major barrier against obtaining a high bandwidth vibration exciter.

• The Transactions of the Korean Institute of Electrical Engineers B
• /
• v.48 no.1
• /
• pp.19-26
• /
• 1999

A moving-coil-type linear motor, designed and fabricated, is consisted of the NdFeB permanent magnets with high specific energy as the stator, a coil-wrapped nonmagnetic hollow rectangular structure and an iron core as a pathway for magnetic flux. The interaction between permanent magmet and armature fie1d, so called "push/pull effect", is to shift the airgap flux density variation due to the magnet alone by a certain amount. Thrust therefore is shift downward or upward. The push/pull effect was presented through the FEM analysis and the static tests. We compared the thrust obtained through the FEM analysis with the static tests. Finally, we present the linearity and correction coefficients of the thrust in consideration of the push/pull effects.l effects.