• 제목/요약/키워드: Linear transfer

검색결과 1,136건 처리시간 0.028초

Force control of a structurally flexible robotic manipulator

  • 최병오
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1992년도 춘계학술대회 논문집
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    • pp.369-373
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    • 1992
  • Force control of a planar two-link structurally flexible robotic manipulator is considered in this study. The dynamic model is obtained by using the extended Hamilton's principle and the Galerkin criterion. A method is pressented toobtain the linearized equations of motion in Cartesian space for use in designing the control system. The approachto solving the control problem is to use feedforward and feedback control torques. The feedforward torques maneuver the flexible manipulatro along a nominal trajectory and the feedback torques minimize any deviations from the nominal trajectory. The linear quadratic Gaussian/loop transfer recovery (LQG/LTR) design methodology is explotied to design a robust feedback control system that can handle modeling errors and sensor noise, and operates on Cartesian space trajectory errors. The Lqg/LTR compenstaor together with a feedforward ollp is used to control the flexible manipulator. Simulated results are presented for a numerical example.

견실한 다변수 제어에 의한 모형 헬리콥터의 자세제어기 설계및 실현 (Attitude controller design and implementation for a helicopter propeller setup using a robust multivariable control)

  • 이승국;이명의;권오규
    • 제어로봇시스템학회논문지
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    • 제4권1호
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    • pp.32-37
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    • 1998
  • This paper deals with the implementation of a robust multivariable controller using DSP board and the application to real systems. The LQG/LTR (Linear Quadratic Gaussian with Loop Transfer Recovery) controller proposed by Doyle et al.[1,2] is adopted to design the control system. A helicopter propeller setup is taken as the controlled system in the current paper, and the mathematical model is derived to design the multivariable controller. The performance of the controller is evaluated via simulations, and implementation and application to the MIMO system shows that the control performances are satisfactory and superior to those of the PID controller.

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말뚝-캡 강성을 고려한 군말뚝기초의 해석 (Analysis of Pile Groups Considering Pile-Cap Interaction)

  • 정상섬;원진오;허정원
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2001년도 봄 학술발표회 논문집
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    • pp.363-370
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    • 2001
  • A computationally efficient algorithm to analyze a group pile behavior is proposed by consideration of both soil-pile and pile-cap interactions. Using toad transfer method the nonlinear characteristics of the soil-pile interaction for a single pile is modeled by piecewise linear soil springs (p-y, t-z, and q-z curves). Beam-column method, one of the most practical approaches, is used for numerical modeling of the soil-pile system. In addition to the group effect resulting from the soil-pile-soil interaction, for a more realistic analysis it is essential to consider the effect of pile-cap interaction including geometric configuration of the piles in a group and conectivity conditions between piles and the cap. This paper mainly focuses on the pile-cap interaction and the development of a rational numerical procedure of its incorporation with the beam-column method.

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The Improved Design of Double Sided Coreless PMLSM with Consideration of Rising Winding Temperature

  • An, Ho-Jin;Cho, Gyu-Won;Jang, Ki-Bong;Kim, Gyu-Tak
    • Journal of Electrical Engineering and Technology
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    • 제8권1호
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    • pp.144-149
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    • 2013
  • This work deals with the optimal design of a coreless PMLSM (Permanent Magnet Linear Synchronous Motor) with consideration of rising winding temperature. The temperature distribution caused by copper loss in the coreless PMLSM was analyzed using a FEM (Finite Element Method). The thrust and current density where the winding temperature reaches the allowable temperature were calculated. The optimal model provides maximum thrust per unit weight.

주파수영역에서 축소모델을 이용한 PID 제어기 설계 (A Design of PID Controller Using Reduced Model in Frequency Domain)

  • 김종근;김주식;전병석
    • 조명전기설비학회논문지
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    • 제19권1호
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    • pp.80-86
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    • 2005
  • 본 논문에서는 시간지연을 갖는 고차모델의 축소모델로부터 요구된 주파수 설계사양을 만족하는 PID 제어기 설계방법을 제안한다. 제안된 방식은 주파수 경계조건으로부터 얻어진 2차원 입력행렬과 출력벡터를 재배열하여 구성된 선형연립방정식에 의해서 PID 제어기의 파라미터 벡터를 식별하는 방법이다. 그리고 네 개의 예제가 제안된 방식의 유용성을 나타내기 위해서 주어진다.

Dynamic response for electromechanical integrated toroidal drive to electric excitation

  • Xu, Lizhong;Hao, Xiuhong
    • Structural Engineering and Mechanics
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    • 제26권6호
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    • pp.635-650
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    • 2007
  • In this paper, the equivalent exciting force caused by electric excitation is derived. By dividing load and displacement vectors into mean values and time-varying ones, the dynamic equations of the system are transformed into linear ones for time-varying portion of the displacements. The analytical equations of the forced time responses of the drive system to electric excitations are obtained. Using the Laplace transformation, the transfer function of the drive system is obtained. These equations are used to analyze the time and frequency responses of the drive system to the electric excitation. It is known that electric excitation can cause forced responses of the drive system, the total dynamic responses are decided by three phase exciting voltages, exciting frequency and natural frequencies of the drive system, and the drive parameters have obvious influence on the time and frequency responses.

터빈 블레이드 캐버티 내 막냉각 특성에 관한 수치해석적 연구 (Numerical Study of Film Cooling Characteristics in Turbine Blade Cavity)

  • 김경석;조형희;강신형
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.648-651
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    • 2008
  • Numerical calculations are performed to simulate the film cooling effect of turbine blade tip with squealer rim. Because of high temperature of inside rim, squealer rim is damaged easily. Therefore many various cooling systems were used. The calculations are based on 100,000 Reynolds number in linear cascade model. A blade has 2% tip clearance and 8.4% rim height. The axial chord length and turning angle is 237mm, 126$^{\circ}$. Numerical calculations are performed without and with film cooling. In a film cooling in the cavity, hot spots of cavity were cooled effectively. However hot spots of suction side rim still remains. The CFD results show that the circulation flow in cavity of squealer tip affects the temperature rise of squealer rim. To maintain the blade integrity and avoid the excessive hot spot of blade, rearrangement of cooling hole is needed.

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유한체적법을 통한 구면 좌표계에서의 볼츠만 수송방정식의 해석 (Analysis of Boltzmann transport equation with Finite Volume Method at Spherical coordinate)

  • 오혁근;진재식;이준식
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.1800-1805
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    • 2008
  • A "finite volume method" is proposed to predict heat transport in a spherical enclosure at micro/nanoscale with the Boltzmann transport equation (BTE). The gray version of the BTE with the relaxation time approximation has been applied. Pointing out similarity between radiative transfer equation (RTE) and BTE, the mapping process in RTE is adopted to treat the angular derivative term and linear algebraic discretization equation is derived by using the established method which is used in 2-D BTE in cartesian coordinates. The simulation results are compared to exact solution to RTE for various acoustic thicknesses and ratio of radii. The comparison shows that this method is logical and accurate, and it is possible to easily adopt various models in spherical BTE.

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On Effects of Large-Deflected Beam Analysis by Iterative Transfer Matrix Approach

  • 신중호
    • 한국기계연구소 소보
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    • 통권18호
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    • pp.131-136
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    • 1988
  • A small-deflected beam can be easily solved by assuming a linear system. But a large-deflected beam can not be solved by superposition of the displacements, because the system is nonlinear. The solutions for the large-deflection problems can not be obtained directly from elementary beam theory for linearized systems since the basic assumptions are no longer valid. Specifically, elementary theory neglects the square of the first derivative in the beam curvature formula and provides no correction for the shortening of the moment-arm cause by transverse deflection. These two effects must be considered to analyze the large deflection. Through the correction of deflected geometry and internal axial force, the proposed new approach is developed from the linearized beam theory. The solutions from the proposed approach are compared with exact solutions.

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분무성형 공정에서 분무액적의 열이력 해석 및 고상분율 예측 (Thermal History Analysis and Solid Fraction Prediction of Gas-Atomized Alloy Droplets during Spray Forming)

  • 이언식
    • 한국분말재료학회지
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    • 제1권1호
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    • pp.85-94
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    • 1994
  • In order to predict droplet velocity and temperature profiles and fractional solidification with flight distance during spray forming, the Newtonian heat transfer formulation has been coupled with the classical heterogeneous nucleation and the specific solidification process. It has been demonstrated that the thermal profile of the droplet in flight is significantly affected by process parameters such as droplet size, initial gas velocity, undercooling. As the droplet size and/or the initial gas velocity increase, the onset and completion of solidification are shifted to greater flight distances and the solidification process also extends over a wider range of flight distances. The amounts of solid fractions formed during recoalescence, segregated solidification and eutectic solidification are insensitive to droplet size and initial gas velocity whereas those are strongly affected by the degree of undercooling. There are good linear relations between the undercooling and the corresponding solid fractions generated during recoalesced, segregated and eutectic stages.

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