• Title/Summary/Keyword: surface structure control

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Covalent Functionalization of Carbon Nanotubes using Atom Transfer Radical Polymerization

  • Paik, Hyun-Jong
    • Proceedings of the Polymer Society of Korea Conference
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    • 2006.10a
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    • pp.196-197
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    • 2006
  • Among various polymerization methods to graft polymers on the surface of CNTs, Atom Transfer Radical Polymerization (ATRP) has several advantages, such as a wide range of polymerizable monomers and superb control in molecular structure and weights. Several research groups including us have showed that ATRP is an efficient and versatile method to modify the surface of CNTs. Here, two independent approaches for the covalent attachment of polymers based on ATRP graft-from and graft-onto methods will be discussed.

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Development of polishing tool system for robot (로보트용 금형 연마 공구 시스템의 개발)

  • 박종오;이대엽
    • 제어로봇시스템학회:학술대회논문집
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    • 1990.10a
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    • pp.190-193
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    • 1990
  • Die finishing (polishing and lapping) after NC machining is characterized as one bottleneck process for reducing lead time. For automation of this typical manual work, a flexible polishing tool system using industrial robot has been developed. This tool system has three principal functions in order to achieve reduction of waviness, 3 D.O.F. compliance and constant pressure structure. This polishing tool shows that adaptability to free form surface is increased and programmability to various areas of die surface is also acquired.

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A INTEGRAL VARIABLE STRUCTURE CONTROLLER FOR BLDDSM WITH PRESCRIBED OPTIMAL OUTPUT DYNAMICS (직접구동용 브러쉬없는 직류 전동기를 위한 적분 가변 구조 제어기)

  • Lee, Jung-Hoon;Chung, Se-Kyo;Moon, Gun-Woo;Kim, Il-Song;Youn, Myung-Joong
    • Proceedings of the KIEE Conference
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    • 1994.07a
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    • pp.472-474
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    • 1994
  • A new integral variable structure system without the reaching phase problems is presented for the prescribed control of the BLDDSM under load variation and parameter uncertainties. The control technique can yields the complete robustness of initially prescribed output dynamics in the sliding surface against the modeling errors. The comparative simulation and experiment studies of the BLDDSM position control are carried out in comparison with two previous algorithms.

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Design of an new variable structure model following control system for robot manipulators

  • Park, Kang-Bark;Lee, Ju-Jang
    • 제어로봇시스템학회:학술대회논문집
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    • 1994.10a
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    • pp.324-327
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    • 1994
  • In this paper, a new design method of variable structure model following control system(VSMFCS) for robot manipulators is proposed. The proposed controller overcomed reaching phase problem by using function augmenting scheme to the sliding surface. Therefore, it can be guaranteed that the overall system always has a robust property against parameter variations and external disturbances. Furthermore, the proposed controller does not use the model state, .chi.$_{m}$, different from other previous works. Regardless of not using the model state, the model following error dynamics, virtual dynamics, is shown to be globally exponentially stable. The efficiency of the proposed method has been demonstrated by an example.e.

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Variable Structure Controller Design For The Nonlinear System Using Sliding Sector (슬라이딩 섹터를 이용한 비선형 시스템의 가변 구조 제어기의 설계)

  • Seo, Ho-Joon;Park, Jang-Hyun;Park, Gwi-Tae
    • Proceedings of the KIEE Conference
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    • 2000.07d
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    • pp.2661-2663
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    • 2000
  • In general, to reduce chattering in sliding mode control, a boundary layer around the sliding surface is used, and a continuous control is applied within the boundary. In this paper we propose the design method of sliding mode controller with sliding sector. To do this, the variable structure controller is designed for the linear system with uncertainty using sliding sector. The control law designed in the paper transfers the system state from outside to the inside of the sliding sector and ensures that some norm of the system state keeps decreasing.

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Catalyst Enhanced by Controlling Structure and Shape of Nanocrystals, Support Materials, and Hybrid System in DMFCs (나노입자의 구조와 모양, 담지체 및 하이브리드 시스템 제어를 통한 직접메탄올 연료전지의 촉매 개발)

  • Lee, Young Wook;Shin, Tae Ho
    • Ceramist
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    • v.22 no.2
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    • pp.189-197
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    • 2019
  • Direct methanol fuel cells (DMFCs) have found a wide variety of commercial applications such as portable computer and mobile phone. In a fuel cell, the catalysts have an important role and durability and efficiency are determined by the ability of the catalyst. The activity of the catalyst is determined by the structure and shape control of the nanoparticles and the dispersion of the nanoparticles and application system. The surface energy of nanoparticles determines the activity by shape control and the nanostructure is determined by the ratio of bi- and tri-metals in the alloy and core-shell. The dispersion of nanoparticles depends on the type of support such as carbon, graphen and metal oxide. In addition, a hybrid system using both optical and electrochemical device has been developed recently.

Sliding Mode Controller Applied to Coupled Inductor Dual Boost Inverters

  • Fang, Yu;Cao, Songyin;Wheeler, Pat
    • Journal of Power Electronics
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    • v.19 no.6
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    • pp.1403-1412
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    • 2019
  • A coupled inductor-dual boost-inverter (CIDBI) with a differential structure has been presented for application to a micro-inverter photovoltaic module system due to its turn ratio of a high-voltage level. However, it is difficult to design a CIDBI converter with a conventional PI regulator to be stable and achieve good dynamic performance, given the fact that it is a high order system. In view of this situation, a sliding mode control (SMC) strategy is introduced in this paper, and two different sliding mode controllers (SMCs) are proposed and adopted in the left and right side of two Boost sub-circuits to implement the corresponding regulation of the voltage and current. The schemes of the SMCs have been elaborated in this paper including the establishment of a system variable structure model, selection of the sliding surface, determination of the control law, and presentation of the reaching conditions and sliding domain. Finally, the mathematic analysis and the proposed SMC are verified by experimental results.

Wakes of two inline cylinders at a low Reynolds number

  • Zafar, Farhan;Alam, Md. Mahbub;Muhammad, Zaka;Islam, Md.
    • Wind and Structures
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    • v.29 no.1
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    • pp.55-64
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    • 2019
  • The effect of vortex impingement on the fluid dynamics around a cylinder submerged in the wake of another of different diameters is numerically investigated at a Reynolds number Re = 200. While the diameter (D) of the downstream cylinder is fixed, impinging vortices are produced from the upstream cylinder diameter (d) varied as d/D = 0.24, 0.4, 0.6, 0.8 and 1.0, with a spacing ratio L=5.5d, where L is the distance between the center of the upstream cylinder to the front stagnation point of the downstream cylinder. Two-dimensional simulations are carried out using the finite volume method. Fluid forces acting on the two cylinders are correlated with impinging vortices, vortex shedding, and wake structure. Different facets of wake formation, wake structure, and flow separation and their connections to fluid forces are discussed.

대칭형 유압 실린더를 이용한 부하재현에 관한 연구

  • 김학성;이교일
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1991.04a
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    • pp.214-224
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    • 1991
  • The porpose in this study is to simulate te force required in the measurement of the performance of the equipments or testipieces. For the simulation of the required force, the difference in eachchamber pressure in the hydraulic cylinder was controlled with Variable Structure Control (VSC) theory. Also, nonlinear Variable Structure Observer (VSO) was designed to estimate the derivative of the load pressure which is necessary to determine the sliding surface in VSC theory. In this paper, the digital computer simulation and experiments were executed.

Structural Optimization of 3D Printed Composite Flight Control Surface according to Diverse Topology Shapes (다양한 위상 형상에 따른 3D 프린트 복합재료 조종면의 구조 최적화)

  • Myeong-Kyu Kim;Nam Seo Goo;Hyoung-Seock Seo
    • Composites Research
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    • v.36 no.3
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    • pp.211-216
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    • 2023
  • When designing ships and aircraft structures, it is important to design them to satisfy weight reduction and strength. Currently, studies related to topology optimization using 3D printed composite materials are being actively conducted to satisfy the weight reduction and strength of the structure. In this study, structural analysis was performed to analyze the applicability of 3D printed composite materials to the flight control surface, one of the parts of an aircraft or unmanned aerial vehicle. The optimal topology shape of the flight control surface for the bending load was analyzed by considering three types (hexagonal, rectangular, triangular) of the topology shape of the flight control surface. In addition, the bending strength of the flight control surface was analyzed when four types of reinforcing materials (carbon fiber, glass fiber, high-strength high-temperature glass fiber, and kevlar) of the 3D printed composite material were applied. As a result of comparing the three-point bending test results with the finite element method results, it was confirmed that the flight control surface with hexagonal topology shape made of carbon fiber and Kevlar had excellent performance. And it is judged that the 3D printed composite can be sufficiently applied to the flight control surface.