• 제목/요약/키워드: Design Equations

검색결과 2,912건 처리시간 0.028초

최소 위상 오차를 갖는 곡선 배열안테나용 Rotman 렌즈의 설계 (Design of Rotman Lens for Curved Array Antenna with Minimal Phase Error)

  • 박주래;박동철
    • 한국전자파학회논문지
    • /
    • 제25권10호
    • /
    • pp.1077-1086
    • /
    • 2014
  • 컨포멀 배열에 적용할 수 있는 곡선 배열안테나용 Rotman 렌즈의 설계 방법을 제안한다. 본 논문에서는 곡선 배열안테나와 연동하여 Rotman 렌즈의 평행판 영역에 존재하는 배열 포트의 위치와, 배열 포트와 배열안테나 소자를 연결하는 전송선의 길이를 구하는 설계식을 유도하고, 이 설계식을 바탕으로 빔 곡선 최적화 절차와 재초점 절차를 통하여 위상 오차를 최소화하고 있다. 제안된 설계식과 설계 절차에 의해 설계된 Rotman 렌즈는 정확히 3초점을 보유한 채 직선 배열안테나뿐만 아니라, 원곡선, 포물선, V자형 곡선 등의 오목하거나 볼록한 배열안테나를 급전할 수 있으며, 최소의 위상 오차를 나타내고 있다.

우주로봇의 이산시간 출력 귀환 LQ 제어 (Output Feedback LQ control of a Space Robot in Discrete-Time)

  • 임승철
    • 소음진동
    • /
    • 제6권5호
    • /
    • pp.567-574
    • /
    • 1996
  • This paper concerns an articulated space robot with flexible links. The equations of its motion are derived by means of the Lagrangian mechanics. Assuming that magnitude of elastic motions are relatively small, the perturbation approach is taken to separate the original equations of motion into linear and nonlinear equations. Th effect the desired payload motion, open loop control inputs are first determined based on the nonlinear equations. One the other hand, in order to reduce the positional errors during the maneuver, vibration suppression is actively done with a feedforward control for disturbance cancellation to some extent. Additionally, for performance robustness against residual disturbance, an LQ control modified to have a prescribed degree of stability is applied based on the linear equations. Measurement equations are formulated to be used for the maximum likelihood estimator to reconstruct states from the original robot equations of motion. Finally, numerical simulations show effectiveness of the proposed control design scheme.

  • PDF

Walking Pattern Generation employing DAE Integration Method

  • Kang Yun-Seok;Park Jung-Hun;Yim Hong Jae
    • Journal of Mechanical Science and Technology
    • /
    • 제19권spc1호
    • /
    • pp.364-370
    • /
    • 2005
  • A stable walking pattern generation method for a biped robot is presented in this paper. In general, the ZMP (zero moment point) equations, which are expressed as differential equations, are solved to obtain a stable walking pattern. However, the number of differential equations is less than that of unknown coordinates in the ZMP equations. It is impossible to integrate the ZMP equations directly since one or more constraint equations are involved in the ZMP equations. To overcome this difficulty, DAE (differential and algebraic equation) solution method is employed. The proposed method has enough flexibility for various kinematic structures. Walking simulation for a virtual biped robot is performed to demonstrate the effectiveness and validity of the proposed method. The method can be applied to the biped robot for stable walking pattern generation.

Design Equations for the H-plane Power Divider with a Circular Post in a Rectangular Waveguide

  • Han Sang-Sin;Lee Sun-Young;Ko Han-Woong;Park Dong-Hee;Ahn Bierng-Chearl
    • Journal of electromagnetic engineering and science
    • /
    • 제4권4호
    • /
    • pp.150-155
    • /
    • 2004
  • Universal design equations are presented for the H-plane T-junction power divider with a circular conducting post in a rectangular waveguide. For a given operating frequency and power split ratio, the post offset from the T-junction center line, the distance between the post and the waveguide wall, and the post diameter can be adjusted to obtain a minimum reflection at the input waveguide. Optimum values of the post offset are given in terms of the normalized frequency and the power split ratio. Corresponding values of the post diameter and the distance of the post from the waveguide wall are given in terms of the normalized frequency and the post offset.

축류송풍기의 저소음 설계에서 수치최적화기법들의 평가 (Assessment of Numerical Optimization Algorithms in Design of Low-Noise Axial-Flow Fan)

  • 최재호;김광용
    • 대한기계학회논문집B
    • /
    • 제24권10호
    • /
    • pp.1335-1342
    • /
    • 2000
  • Three-dimensional flow analysis and numerical optimization methods are presented for the design of an axial-flow fan. Steady, incompressible, three-dimensional Reynolds-averaged Navier-Stokes equations are used as governing equations, and standard k- ${\varepsilon}$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Steepest descent method, conjugate gradient method and BFGS method are compared to determine the searching directions. Golden section method and quadratic fit-sectioning method are tested for one dimensional search. Objective function is defined as a ratio of generation rate of the turbulent kinetic energy to pressure head. Two variables concerning sweep angle distribution are selected as the design variables. Performance of the final fan designed by the optimization was tested experimentally.

An Optimal Design of a two stage relief valve by Genetic Algorithm

  • Kim, seungwoo;doowan Im;Kyungkwan Ahn;Soonyong Yang;Lee, Byungryong
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2002년도 ICCAS
    • /
    • pp.66.2-66
    • /
    • 2002
  • In this study, a novel systematic design procedure by Genetic Algorithm of a two stage relief valve is proposed. First of all, a mathematical model describing the dynamics of a balanced piston type relief valve has been derived. Governing equations such as dynamic equations for the main spool and the pilot spool and flow equations for each orifice are established. The mathematical model is verified by comparing the results of simulation with that of experiments. Furthermore, influences of the parameters on the dynamic characteristics of a relief valve have been investigated by simulation of the proposed model. Major design parameters on the valve response are determin...

  • PDF

Single and High-Lift Airfoil Design Optimization Using Aerodynamic Sensitivity Analysis

  • Kim, Chang Sung;Lee, Byoungjoon;Kim, Chongam;Rho, Oh-Hyun
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제2권1호
    • /
    • pp.20-27
    • /
    • 2001
  • Aerodynamic sensitivity analysis is performed for the Navier-Stokes equations coupled with two-equation turbulence models using a discrete adjoint method and a direct differentiation method respectively. Like the mean flow equations, the turbulence model equations are also hand-differentiated to accurately calculate the sensitivity derivatives of flow quantities with respect to design variables in turbulent viscous flows. The sensitivity codes are then compared with the flow solver in terms of solution accuracy, computing time and computer memory requirements. The sensitivity derivatives obtained from the sensitivity codes with different turbulence models are compared with each other. The capability of the present sensitivity codes to treat complex geometry is successfully demonstrated by analyzing the flows over multi-element airfoils on Chimera overlaid grid systems.

  • PDF

토션빔 후륜 현가장치의 기구학적 특성 해석 (Kinematic Analysis of Torsion Beam Rear Suspension)

  • 강주석
    • 한국자동차공학회논문집
    • /
    • 제12권5호
    • /
    • pp.146-153
    • /
    • 2004
  • Torsion beam rear suspension has been widely adopted to the rear suspension of vehicle by reason of simple structure and cost competitiveness. Since the kinematic characteristics of torsion beam rear suspension are determined by elastic behavior of torsion beam, quasi-static analysis based on finite element modeling of torsion beam has been conducted to obtain the kinematic parameters of torsion beam rear suspension. In this paper, simple kinematic equations with rear geometric parameters are derived to predict the kinematic behavior of torsion beam rear suspension. The suspension design parameters such as roll center height, roll stiffness, roll steer and roll camber can be easily obtained with the kinematic equations. The suggested kinematic equations are validated from comparison with the test results and solution offered by ADAMS. The suspension design parameters varied with the position of torsion beam are discussed.

축류송풍기 설계를 위한 최적설계기법의 평가 (Assessment of Optimization Methods for Design of Axial-Flow Fan)

  • 최재호;김광용
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.221-226
    • /
    • 1999
  • Three-dimensional flow analysis and numerical optimization methods are presented for the design of an axial-flow fan. Steady, Incompressible, three-dimensional Reynolds-averaged Wavier-Stokes equations are used as governing equations, and standard k-$\epsilon$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Steepest descent method, conjugate gradient method and BFGS method are compared to determine the searching directions. Golden section method and quadratic fit-sectioning method are tested for one dimensional search. Objective function is defined as a ratio of generation rate of the turbulent kinetic energy to pressure head. Sweep angle distributions are used as design variables.

  • PDF

Formulae for the frequency equations of beam-column system carrying a fluid storage tank

  • El-Sayed, Tamer. A.;Farghaly, Said. H.
    • Structural Engineering and Mechanics
    • /
    • 제73권1호
    • /
    • pp.83-95
    • /
    • 2020
  • In this work, a mathematical model of beam-column system carrying a double eccentric end mass system is investigated, and solved analytically based on the exact solution analysis. The model considers the case in which the double eccentric end mass is a rigid storage tank containing fluid. Both Timoshenko and Bernoulli-Euler beam bending theories are considered. Equation of motion, general solution and boundary conditions for the present system model are developed and presented in dimensional and non-dimensional format. Several important non-dimensional design parameters are introduced. Symbolic and/or explicit formulae of the frequency and mode shape equations are formulated. To the authors knowledge, the present reduced closed form symbolic and explicit frequency equations have not appeared in literature. For different applications, the results are validated using commercial finite element package, namely ANSYS. The beam-column system investigated in this paper is significant for many engineering applications, especially, in mechanical and structural systems.