• Title/Summary/Keyword: Servo Actuator

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Sensorless speed control of DC servo motor (DC 서보모터의 센서리스 속도 제어)

  • 김창세;오정석;하주식
    • 제어로봇시스템학회:학술대회논문집
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    • 1997.10a
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    • pp.203-206
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    • 1997
  • DC servo motors are widely used in many industrial fields as actuator of robot and driving power motors of electrical vehicle. Usually in the speed control systems, of motors, speed sensors are required and this fact results in the increased price and operating cost and the limited application of the motors. In this paper, a new speed control method for DC servo motor is proposed. In the scheme, the rotational speed is estimated by the measurement values of the armature voltage and current, instead of measurement by sensor. Optimal control theory is applied to design of the controller in construction of real system. This paper also report on the results of experiments to prove the validity of the proposed method.

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Dual Servo Control for Aperture Type Near Field Storage Head (개구형 근접장 헤드장치의 간극제어를 위한 이중 서보 제어)

  • Lee, Sung-Q;Kim, Eun-Kyoung;Park, Kang-Ho
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.16 no.5 s.110
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    • pp.479-484
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    • 2006
  • This paper presents an active control of the aperture type near-field storage head. In order to achieve a fast and accurate control, a dual servo control algorithm is applied. Based on the big difference in time constants of two actuators, they are used independently. With the combination fine and coarse actuator, the disk is rotated up to 10 rpm speed until the gap is controlled within 100 nm. From the experimental results, the feasibility and the performance of active dual servo gap control is proved.

Design of the Robust Servo Control System for Steel Making Plant using Disturbance Observer Algorithm (DOB를 이용한 제철설비용 강인 서보 제어시스템 구현)

  • Kim, Dong-Sam;Heo, Yun-Je;Jeong, Wan-Gyun
    • Proceedings of the KIEE Conference
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    • 2003.11c
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    • pp.693-696
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    • 2003
  • Among many servo control systems in steel making plant, AGC system in hot rolling mill is very important to get a accurate strip thickness for good quality. AGC (Auto Gauge Control) system controls the roll gap to maintain the required thickness by using the variation of roll force and the measure of output thickness. In this paper, a simulator of AGC system which unifies both hydraulic servo control system and AGC algorithm is suggested. After proving the concurrence of algorithms between the simulator and real system, main actuator system is added. Instead of usual PI system used in present system, DOB control scheme is applied and shows the effect of disturbance attenuation well.

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Dual Stage Actuator System for High Density Magnetic Disk Drives Using a Rotary-type Electrostatic Microatuator (회전구동 정전형 마이크로 액추에이터를 이용한 고트랙밀도 HDD용 이단 구동 시스템)

  • Jung Sunghwan;Choi Jae-Joon;Park Jihwang;Lee Chang-Ho;Kim Cheol-Soon;Min Dong-Ki;Kim Young-Hoon;Lee Seung-Hi;Jeon Jong Up
    • Journal of the Korean Society for Precision Engineering
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    • v.22 no.10 s.175
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    • pp.174-185
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    • 2005
  • This paper presents the design, fabrication, and testing results of a dual stage actuator system for a fine positioning of magnetic heads in magnetic disk drives. A novel rotary microactuator which is electrostatically driven and utilized as a secondary actuator was designed. The stator and rotor electrodes in the microactuator was revised to have the optimal shapes and hence produces much higher rotational torque compared with the conventional comb-shape electrodes. The microactuators were successfully fabricated using SoG(silicon on glass) processing technology, which is known as being cost-effective. The fabricated microactuator has the structural thickness of $45{\mu}m$ with the gap width of approximately $3{\mu}m$. The dynamic characteristic of microactuator/slider assembly was investigated, and its natural frequency and DC gain were measured to be 3.4kHz and 32nm/V, respectively. The microactuator/slider assembly was integrated into a HDD model V10 of Samsung Electronics Co. and a dual servo algorithm was tested to explore the tracking performance of dual stage actuator system where the LDV signals instead of magnetic head signals were used. Experimental results indicate that this system achieves the tracking accuracy of 30nm. This value corresponds to a track density of 85,000 track per inch(TPI), which is about 3 times greater than that of current hard disk drives.

The Influence of elastic stiffness for a Starting State of Linear Actuator (선형액추에이터의 초기구동에 미치는 탄성계수의 영향)

  • Woo, Byung-Chul;Kang, Do-Hyun;Hong, Do-Kwan
    • Proceedings of the KIEE Conference
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    • 2004.10a
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    • pp.77-79
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    • 2004
  • A typical conventional systems of a linear motion use rack and pinions or ball screws to convert rotary motions from DC servo motors. A linear motor has been used a several field for a MEMS technology and a aircraft carrier. We was studied a transient response of a linear actuator with a damping ratio, spring constant and a pressed power.

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Transient Response of a linear actuator with a damping ratio (공진형 선형 액추에이터의 감쇄지수 변화에 따른 과도 응답특성)

  • Woo Byung Chul;Kang Do Hyun
    • Proceedings of the KIEE Conference
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    • summer
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    • pp.1037-1039
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    • 2004
  • A typical conventional systems of a linear motion use rack and pinions or ball screws to convert rotary motions from DC servo motors. A linear motor has been used a several field for a MEMS technology and a aircraft carrier. We was studied a transient response of a linear actuator with a damping ratio, spring constant and a pressed power.

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Dynamic Characterizations of a Piezoelectric Microactuator in Hard Disk Drive (HDD용 압전형 마이크로엑츄에이터의 동특성 규명)

  • Kim, Cheol-Soon;Kim, Kyu-Yong
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2000.11a
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    • pp.232-236
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    • 2000
  • To provide model parameters for servo control system design, dynamic characteristics of a piezoelectric microactuator for hard disk drive(HDD) were investigated. At first frequency response characteristics was measured and a second order model was proposed. Here the amplitude dependent dynamic characteristics such as low frequency gain and damping ratio were studied. In addition, the load current and equivalent impedance of the piezoelectric actuator were measured by varying excitation voltage and frequency. At last, the super-harmonic resonance of the piezoelectric actuator was discussed.

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A Study on the Air Vent Valve of the Hydraulic Servo Actuator for Steam Control of Power Plants (발전소의 스팀제어용 유압서보 액추에이터의 공기배출 밸브에 관한 연구)

  • Lee, Yong Bum;Lee, Jong Jik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.6
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    • pp.397-402
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    • 2016
  • To produce adequate electricity in nuclear and thermal power plants, an optimal amount of steam should be supplied to a generator connected to high- and low-pressure steam turbines. A turbine output control device, which is a special steam valve employed to supply or interrupt the steam to the turbine, is operated using a hydraulic servo actuator. In power plants, the performance of servo actuators is degraded by the air generated from the hydraulic system, or causes frequent failures owing to an increase in the wear of the seal. This is due to the seal being burnt as generated heat using the produced compressed air. Some power plants have exhausted air using a fixed orifice, and thus they encounter power loss due to mass flow exhaust. Failures are generated in hydraulic pumps, electric motors, and valves, which are frequently operated. In this study, we perform modeling and analysis of the load-sensing air-exhaust valves, which can be passed through very fine flow under normal use conditions, and exhaust mass flow air at the beginning stage as with existing fixed orifices. Then, we propose a method to prevent failures due to the compressed air, and to ensure the control accuracy of hydraulic servo actuators.

Dynamic Characteristic Analysis of Aerodynamic Load Simulator English (항공기 조종면 부하재현장치의 운동 특성 해석)

  • Nam, Yun-Su
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.25 no.3
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    • pp.478-485
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    • 2001
  • A dynamic load simulator(DLS) which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of aircraft actuation system. By setting up load actuator as counter acting with the control surface driving actuator and designing an appropriate force control system for load actuator, DLS can be mechanized. Obtaining an accurate mathematical model for the DLS is the first step to successfully design an aerodynamic load replicati on system. Two theoretical models are presented and tested for their validities with the experimental results, which turns out to be not successful. An alternative way of using system identification approaches in investigated to develop a good nominal model for DLS dynamics, and suitable uncertainty bounds for this nominal model are proposed with the consideration of experimental results.