• 제목/요약/키워드: Miniature actuator

검색결과 26건 처리시간 0.019초

FUZZY POSITION/FORCE CONTROL OF MINIATURE GRIPPER DRVEN BY PIEZOELECTRIC BIMORPH ACTUATOR

  • Kim, Young-Chul;Chonan, Seiji;Jiang, Zhongwei
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 Proceedings of the Korea Automatic Control Conference, 11th (KACC); Pohang, Korea; 24-26 Oct. 1996
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    • pp.24.2-27
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    • 1996
  • This paper is a study on the fuzzy force control of a miniature gripper driven by piezoelectric bimorph actuator. The system is composed of two flexible cantilevers, a stepping motor, a laser displacement transducer and two semiconductor force sensors attached to the beams. Obtained results show that the present artificial finger system works well as a miniature gripper, which produces approximately 0.06N force in the maximum. Further, the fuzzy position/force control algorithm is applied to the soft-handing gripper for stable grasping of a object. It revealed that the fuzzy rule-based controller be efficient controller for the stable drive of the flexible miniature gripper. It also showed that two semiconductor strain gauges located in the flexible beam play an important roles for force control, position control and vibration suppression control.

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바이몰프형 PZT를 이용한 소형만능재료시험기용 정밀 구동 액추에이터의 개발 (Development of a New Precision Actuator by Bi-morph Type PZT to Realize Nano/Micro Mechanical Testing in MUTM)

  • 권현규;최성대;정선환
    • 한국기계가공학회지
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    • 제5권1호
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    • pp.45-50
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    • 2006
  • This paper shows a new precision actuator of MUTM(miniature universal testing machine) for the testing of compression and tensile load on the MEMS materials and structures. The MUTM consists of a sample holder, an ultraprecision precision actuator(tranlation stage) and load sensor. The precision actuator has been developed for generating displacements with nanometer accuracy and a dynamic range of 1mm simultaneously. In this paper, it can be made by using the displacement property of bi-morph type PZT, which is able to extend the long range(stroke) according to cantilever size. However, it is not enough to be generated for compression and tensile load in miniature universal testing machine. Therefore, three dozen bi-morph type PZTs are used for generating the load. The load and displacement of the precision actuator are 35g and 0.4mm respectively.

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자가 변위 측정이 가능한 전기-유압식 소프트 지핑 구동기의 개발 (Development of an Electro-hydraulic Soft Zipping Actuator with Self-sensing Mechanism)

  • 이동영;곽보건;배준범
    • 로봇학회논문지
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    • 제16권2호
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    • pp.79-85
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    • 2021
  • Soft fluidic actuators (SFAs) are widely utilized in various areas such as wearable systems due to the inherent compliance which allows safe and flexible interaction. However, SFA-driven systems generally require a large pump, multiple valves and tubes, which hinders to develop a miniaturized system with small range of motion. Thus, a highly integrated soft actuator needs to be developed for implementing a compact SFA-driven system. In this study, we propose an electro-hydraulic soft zipping actuator that can be used as a miniature pump. This actuator exerts tactile force as a dielectric liquid contained inside the actuator pressurized its deformable part. In addition, the proposed actuator can estimate the internal dielectric liquid thickness by using its self-sensing function. Besides, the electrical characteristics and driving performance of the proposed system were verified through experiments.

초소형 스마트탄 최근기술 동향분석 (Recent Status on Miniature Smart-bullet Techniques)

  • 이성헌;조한진;조영기;방효충
    • 한국항공우주학회지
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    • 제43권3호
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    • pp.272-281
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    • 2015
  • 초소형 스마트탄은 탄도를 수정하여 손쉽게 목표물을 타격할 수 있도록 고안된 개인 휴대용 유도미사일이다. 초소형 스마트탄은 유도미사일에 준하는 기능을 수행하는데 반하여 그 크기가 일반 병사들이 쉽게 휴대할 수 있도록 축소됨으로써 아군의 전력과 생존율을 크게 높일 수 있을 것으로 기대된다. 본 논문에서는 초소형 스마트탄의 탄도수정을 위해 사용된 구동장치를 중심으로 해외에서 선행된 기술개발 사례와 특허들을 수집해 보았다. 이를 바탕으로 초소형 스마트탄의 개발을 위한 소요기술들을 분석해 보고, 추후 개념설계를 위한 초석을 마련하였다.

PID 제어기에 의한 소형 로봇용 그리퍼의 힘 제어 (PID Force Control of a miniature robot Gripper)

  • 홍동표
    • 한국생산제조학회지
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    • 제8권2호
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    • pp.44-49
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    • 1999
  • This paper is concerned with the theoretical and experimental study on the force conrtrol of a miniature robotic gripper. The gripper is an uniform flexible cantilever equipped with a distributed set of compact force sensor. As an actuator piezoelectric acturator, piezoelectric acturator is fixed with cupper plate at which the beam is clamped. The mathematical model of the assembled electro-mechaincal system is developed. The force sensor is described by a set of concentrated mass-spring system. The formulated equations of motion are applied to he study of a control problem where the gripper is commanded to grip an object The usefulness of the PID control technique is verified by experiment.

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피에조를 이용한 초소형 단일 솔더볼 연결부의 전단 시험장치 개발 (Development of a Shear Testing Machine for a Miniature Single Solder Ball Joint using Piezoelectric Loading Device)

  • 권용상;고국종;김호경
    • Tribology and Lubricants
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    • 제26권1호
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    • pp.44-51
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    • 2010
  • A miniature shear testing machine was designed and developed, adopting a piezoelectric actuator with mechanical advantage using 4 levers in order to investigate shear behavior of a small solder ball. The final output displacement was initially expected to be 2.88 mm without load resistance, considering the lever ratio of 24 and the piezo displacement of 0.12 mm with an exciting voltage of 10 V. However, the final plunger displacement ${\Delta}{\upsilon}$ can be expected as ${\Delta}{\upsilon}=2.88-3.04{\times}10^{-4}F$ as a function of piezoelectric force F due to the stiffness of various levers and connectors and piezo actuator. The shear behavior of lead-free solder ball in diameter of $760{\mu}m$ was successfully investigated in a speed range of 2 mm/s~0.0035 mm/s using this designed device.

근감과 진동촉감 피드백을 제공하는 햅틱 인터페이스용 새로운 소형 액추에이터의 개발 (Development of a New Miniature Actuator providing both Kinesthetic and Vibrotactile Feedback for Haptic Interface)

  • 표동범;류세민;한병길;권동수
    • 로봇학회논문지
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    • 제8권3호
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    • pp.143-149
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    • 2013
  • This paper presents a new miniature haptic display to convey ample haptic information to a user of a handheld interface. There are buttons on interfaces or general electronic devices, but existing buttons provide haptic feedback of only one passive pattern to a user. Because humans perceive tactile and kinesthetic information simultaneously when they handle objects the proposed actuator provides both sensations at once. It is able to generate various levels of kinesthetic sensations when pressing a button under diverse situations. Also, vibrotactile feedback can be delivered for exciting haptic effects with numerous patterns. Its performance was evaluated in accordance with the resistive force by changing the intensity of the input current. Experiments show that the proposed actuator has the ability to provide numerous haptic sensations for more realistic and complex haptic experiences.

탐침형 정보저장장치용 이차원 구동기의 내진 구조 (Design of X-Y Actuator with High Vibration Resistance lot Probe-based Data Storages)

  • 이경일;김성현;조진우;최영진;신진국
    • 정보저장시스템학회:학술대회논문집
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    • 정보저장시스템학회 2005년도 추계학술대회 논문집
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    • pp.195-196
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    • 2005
  • We report the new design of a miniature electromagnetic actuator for probe-based data storage with anti-vibration mechanism. The actuator consists of a media substrate, silicon frame, 2 pairs of magnets, a spacer, and a printed circuit board (PCB). The total area of the device is $11.2{\times}11.2 mm^2$ while the data recording area is $7.4{\times}7.4 mm^2$. A net momentum fee structure was included for high vibration resistance. The simulation shows that the lateral vibration can be reduced to below 100 nm for 1 G acceleration if the counter mass is adjusted with $1\%$ difference. The peak power for ${\pm}50 {\mu}m$ displacement is below 50 mW for a actuator with a resonance at 200 Hz.

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초소형 유도탄 구동날개 시스템의 플러터 예측에 관한 연구 (Study on the Flutter Prediction of the Miniature Guided-bullet Control Surface System)

  • 이성헌;조영기;조한진;방효충
    • 한국군사과학기술학회지
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    • 제20권1호
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    • pp.148-157
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    • 2017
  • Miniature guided-bullet is an advanced military technology of developing guided missile which is designed to hit a target precisely while having easily carriable miniature size. A key issue of developing such system involves size reduction of the original guided missile system, and this in turn arouses stiffness issue regarding small and thin sized control surface. In this study, procedures on how to calculate the critical flutter speed of special type of control surface with the change of its dimension or material property is arranged. During this procedure, design parameters related to critical flutter speed are abridged to help preliminary design of similar structure even faster than time-consuming, and cumbersome computer analysis.