• Title/Summary/Keyword: Tilt actuator

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Design of Moving Coil Type Optical Pickup Actuator for Flexible Disk System (유연디스크용 가동 코일형 광 픽업 엑추에이터 개발)

  • Kim, Yoon-Ki;Song, Myeong-Gyu;Lee, Dong-Ju;Yoo, Jeong-Hoon;Park, No-Cheol;Park, Young-Pil
    • Transactions of the Society of Information Storage Systems
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    • v.2 no.4
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    • pp.240-244
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    • 2006
  • As high-definition television(HDTV) broadcasting becoming more generalized, there have been many researches and developments about a large storage capacity and a fast data transfer rate in optical disk drives (ODD). Pickup actuators must have high flexible mode frequencies and large gain margins. Flexible modes are caused by the flexibility of moving parts in the actuator and a servo bandwidth is limited by them. As a result, the system becomes unstable for high-speed operations in high density reading and recording. In this paper, we suggest improved modeling method in considering of the bonding layer. And, the flexible mode frequency of actuator is improved by Design of Experiments of lens holder. The Magnet circuit is designed considering the relation with the moving part. Through improving the yoke design, the magnetic flux is changed and the DC tilt is reduced. Consequently, we designed an actuator which has a high flexible mode frequency and a large gain margins.

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Disturbance Observer and Time-Delay Controller Design for Individual Blade Pitch Control System Driven by Electro-Mechanical Actuator (전기-기계식 구동기 기반 개별 블레이드 피치 조종 시스템의 제어를 위한 외란 관측기와 시간 지연제어기 설계)

  • Jaewan Choi;Minyu Kim;Younghoon Choi
    • Journal of Aerospace System Engineering
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    • v.18 no.1
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    • pp.29-36
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    • 2024
  • Recently, the concept of Urban Air Mobility (UAM) has expanded to Advanced Air Mobility (AAM). A tilt rotor type of vertical take-off and landing aircraft has been actively studied and developed. A tilt-rotor aircraft can perform a transition flight between vertical and horizontal flights. A blade pitch angle control system can be used for flight stability during transition flight time. In addition, Individual Blade Control (IBC) can reduce noise and vibration generated in transition flight. This paper proposed Disturbance Observer Based Control (DOBC) and Time Delay Control (TDC) for individual blade control of an Electro-Mechanical Actuator (EMA) based blade pitch angle control system. To compare and analyze proposed controllers, numerical simulations were conducted with DOBC and TDC.

Design of flexure hinge to reduce lateral force of laser assisted thermo-compression bonding system (레이저 열-압착 본딩 시스템의 Lateral Force 감소를 위한 유연 힌지의 설계)

  • Lee, Dong-Won;Ha, Seok-Jae;Park, Jeong-Yeon;Yoon, Gil-Sang
    • Design & Manufacturing
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    • v.14 no.3
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    • pp.23-30
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    • 2020
  • Laser Assisted Thermo-Compression Bonding (LATCB) has been proposed to improve the "chip tilt due to the difference in solder bump height" that occurs during the conventional semiconductor chip bonding process. The bonding module of the LATCB system has used a piezoelectric actuator to control the inclination of the compression jig on a micro scale, and the piezoelectric actuator has been directly coupled to the compression jig to minimize the assembly tolerance of the compression jig. However, this structure generates a lateral force in the piezoelectric actuator when the compression jig is tilted, and the stacked piezoelectric element vulnerable to the lateral force has a risk of failure. In this paper, the optimal design of the flexure hinge was performed to minimize the lateral force generated in the piezoelectric actuator when the compression jig is tilted by using the displacement difference of the piezoelectric actuator in the bonding module for LATCB. The design variables of the flexure hinge were defined as the hinge height, the minimum diameter, and the notch radius. And the effect of the change of each variable on the stress generated in the flexible hinge and the lateral force acting on the piezoelectric actuator was analyzed. Also, optimization was carried out using commercial structural analysis software. As a result, when the displacement difference between the piezoelectric actuators is the maximum (90um), the maximum stress generated in the flexible hinge is 11.5% of the elastic limit of the hinge material, and the lateral force acting on the piezoelectric actuator is less than 1N.

Two-Axis Rotational Micro-Mirror for High-Capacity Optical Cross-Connect Switch (대용량 광 스위치를 위한 2축 자유도 마이크로 미러)

  • 김태식;이상신
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.40 no.8
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    • pp.543-548
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    • 2003
  • In this paper, we have proposed and fabricated a two-axis rotational micro-mirror with large tilt angle. Such a micro-mirror is a key element for N$\times$N high capacity optical cross-connect switches. The micro-mirror is required to have large tilt angle to increase the capacity of the cross-connect switches. For larger micro-mirror tilt angle between the grounded mirror plate and the bottom electrode is to be large enough to provide space for the tilting of the mirror. For our proposed structure, the gap was produced in such a way that the grounded mirror plate and the bottom electrode were made separately in different substrates by using the bulk micromachining technology, and combined later by employing self-align technique. As a result, a large tilt angle has been achieved without using additional actuators. The measured tilt angles were as large as $\pm$5.5$^{\circ}$ and $\pm$8.4$^{\circ}$ in the x and y direction respectively, and the pull-in voltages for the two directions were 380 V and 275 V respectively. Finally the fabricated mirror was successfully utilized to steer the optical beam. To our knowledge, our micro-mirror has the best performance among the micro-mirrors reported internationally so far.

Novel mechanism of Compact size Holographic Data Storage (소형 홀로그래픽 고밀도 저장장치에서의 메카니즘 구성)

  • Ha, Sang-Woo;Park, Hong-Soo;Song, In-Sang;Seo, Jeong-Kyo;Choi, In-Ho;Min, Byung-Hoon
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2007.11a
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    • pp.1333-1334
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    • 2007
  • Page-oriented angle multiplexing Holographic data storage system is the one of promising techniques for high capacity and data transfer rate, but its size and narrow tilt margin is pointed as a demerit. To overcome this weak point, in this paper, 2-axis deck mechanism for compensation of disc is employed to Compact size Holographic Data Storage (CHDS) which consists of minimized optical components and small 2-axis actuator moving linear & angle direction. Compensation of radial/tangential disc tilt with 2-axis deck mechanism is demonstrated.

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GMT FSM Prototype의 개발 현황

  • Kim, Yeong-Su;Go, Ju-Heon;Han, In-U;Yang, Ho-Sun;Kim, Ho-Sang;Lee, Gyeong-Don;An, Hyo-Seong;Cho, Myung;Cheon, Mu-Yeong;Park, Byeong-Gon;Gyeong, Jae-Man;Yun, Yang-No
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.124.2-124.2
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    • 2011
  • 한국천문연구원은 GMT (Giant Magellan Telescope)의 부경 중의 하나인 FSM (Fast Steering Mirror)의 시험모델을 개발 중이다. 구경 1.06m의 비축 비구면 반사경을 경량화 가공을 하는 중이며, tip-tilt 제어를 위한 test-bed를 제작하고 시험하는 중이다. 이를 위하여 actuator control model과 진공 운영모델을 마련하고 있다. 또한 tip-tilt의 최종 성능시험을 위한 장치를 개발하기 위한 계획을 세우고 있다. 이 발표에서는 FSM 시험모델의 개발 현황에 대해 논한다.

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A Design of Pan-tilt Leaf Spring Structure for Artificial Eyeball (인공안구를 위한 팬틸트 구동용 판스프링 설계)

  • Kim Jung-Han;Kim Young-Suk
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.14 no.4
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    • pp.22-31
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    • 2005
  • The purpose of this study is to design a flexural structure that has a function of pan and tilt for an artificial eyeball. The artificial eyeball system has a function of image stabilization, which compensate panning and tilting vibration of the body on which the artificial eyeball is attached. The target closed loop control bandwidth is 50Hz, so the mechanical resonance frequency is required to be more than the control bandwidth, which is a tough design problem because of a big mass of camera and actuator. In this study, the design process including the selection of the principal parameters by numerical analysis with ANSYS will be described, as well as the design results and frequency response.

Development of Panel-Based Rapid Aerodynamic Analysis Method Considering Propeller Effect (프로펠러 효과를 반영 가능한 패널 기반 신속 공력 해석 기법 개발)

  • Tai, Myungsik;Lee, Yebin;Oh, Sejong;Shin, Jeongwoo;Lim, Joosup;Park, Donghun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.2
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    • pp.107-120
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    • 2021
  • Electric-powered distributed propulsion aircraft possess a complex wake flow and mutual interference with the airframe, due to the use of many propellers. Accordingly, in the early design stage, rapid aerodynamic and load analysis considering the effect of propellers for various configurations and flight conditions are required. In this study, an efficient panel-based aerodynamic analysis method that can take into account the propeller effects is developed and validated. The induced velocity field in the region of propeller wake is calculated based on Actuator Disk Theory (ADT) and is considered as the boundary condition at the vehicle's surface in the three-dimensional steady source-doublet panel method. Analyses are carried out by selecting an isolated propeller of the Korea Aerospace Research Institute (KARI)'s Quad Tilt Propeller (QTP) aircraft and the propeller-wing configuration of the former experimental study as benchmark problems. Through comparisons with the results of computational fluid dynamics (CFD) based on actuator methods, the wake velocity of propeller and the changes in the aerodynamic load distribution of the wing due to the propeller operation are validated. The method is applied to the analysis of the Optional Piloted Personal Aerial Vehicle (OPPAV) and QTP, and the practicality and validity of the method are confirmed through comparison and analysis of the computational time and results with CFD.

Face Recognition using AdaBoost Algorithm and Development of Surveillance Robot for a Ship (AdaBoost 알고리즘을 이용한 얼굴인식 및 선박용 감시로봇 개발)

  • Go, Seok-Jo;Park, Jang-Sik;Jang, Yong-Seo;Choi, Moon-Ho
    • The Journal of Korea Robotics Society
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    • v.3 no.3
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    • pp.219-225
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    • 2008
  • This study developed a surveillance robot for a ship. The developed robot consists of ultrasonic sensors, an actuator, a lighting fixture and a camera. The ultrasonic sensors are used to avoid collision with obstacles in the environment. The actuator is a servo motor system. The developed robot has four drive wheels for driving. The lighting fixture is used to guide the robot in a dark environment. To transmit an image, a camera with a pan moving and a tilt moving is equipped on the upper part of the robot. AdaBoost algorithm trained with 15 features, is used for face recognition. In order to evaluate the face recognition of the developed robot, experiments were performed.

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Development of an Unmanned Test System Based on Forklift for Mast Operation Durability (지게차 마스트 작동내구를 위한 실차 기반 무인시험장치 개발)

  • Cho, Jae-Hong;Na, Seon-Jun;Kim, Min-Seok;Park, Myeong-Kwan
    • Journal of Drive and Control
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    • v.19 no.4
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    • pp.70-76
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    • 2022
  • In this paper, we develops an unmanned test system for the purpose of realizing an actual forklift-based test-bed for the operation durability of the forklift mast. First, two robot actuators were applied to the lever to replace lever manipulation of the operator. For detecting the height of the fork and the tilt angle of the mast, the laser displacement sensor and the inclinometer were installed to the forklift. Next, the embedded control system was used to control the robot actuator with reference to test mode. Experimental evaluation verified that developed test system was effective and practical for the viewpoint of the repeatability of the test mode.