• Title/Summary/Keyword: System of Linear Equations

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V-벨트 무단변속기(無斷變速機)를 이용(利用)한 자탈형(自脫型) 콤바인의 주행속도(走行速度) 제어(制御)(I) (A Forward Speed Control of Head-feed Combine Using Continuously Variable V-belt Transmission -Combine Load Characteristics-)

  • 최규홍;유관희;조영길;박판규
    • Journal of Biosystems Engineering
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    • 제16권2호
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    • pp.124-132
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    • 1991
  • This study was carried out to obtain the information needed in the development of forward speed control system and the improvement of combine performance. The effects of variety, grain moisture content and forward speed on the combine load characteristics were investigated through experiments. The results of this study are summarized as follows. 1. A data acquisition system was developed to measure the engine speed and the torques and speeds of the threshing cylinder, dean-grain auger and tailings-return auger. The system consisted of transducers, signal conditioner, interface board and microcomputer. The system accuracy is better than ${\pm}2.3%$ full scale. 2. Linear regression equations were obtained for the torque, speed and power requirement of threshing cylinder for different paddy varieties, grain moisture contents and feed rates. 3. The maximum value of relative frequency for threshing cylinder torque decreased as the increase in feed rate and moisture content. The range of torque fluctuation was 1.2~3.7 and 1.2~1.9 times the average and maximum torque, respectively. The maximum value of power spectrum density (PSD) appeared to be about 11 Hz regardless of paddy variety, grain moisture content and feed rate. 4. The speed of tailings return thrower decreased rapidly at below 900rpm, and it fell to near zero about 3 seconds after that time. When the travelling of combine harvester was stopped immediately after sensing the overload, it took about 7 seconds for a full recovery of the no-load speed of tailings return thrower.

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A geometrically nonlinear thick plate bending element based on mixed formulation and discrete collocation constraints

  • Abdalla, J.A.;Ibrahim, A.K.
    • Structural Engineering and Mechanics
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    • 제26권6호
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    • pp.725-739
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    • 2007
  • In recent years there are many plate bending elements that emerged for solving both thin and thick plates. The main features of these elements are that they are based on mix formulation interpolation with discrete collocation constraints. These elements passed the patch test for mix formulation and performed well for linear analysis of thin and thick plates. In this paper a member of this family of elements, namely, the Discrete Reissner-Mindlin (DRM) is further extended and developed to analyze both thin and thick plates with geometric nonlinearity. The Von K$\acute{a}$rm$\acute{a}$n's large displacement plate theory based on Lagrangian coordinate system is used. The Hu-Washizu variational principle is employed to formulate the stiffness matrix of the geometrically Nonlinear Discrete Reissner-Mindlin (NDRM). An iterative-incremental procedure is implemented to solve the nonlinear equations. The element is then tested for plates with simply supported and clamped edges under uniformly distributed transverse loads. The results obtained using the geometrically NDRM element is then compared with the results of available analytical solutions. It has been observed that the NDRM results agreed well with the analytical solutions results. Therefore, it is concluded that the NDRM element is both reliable and efficient in analyzing thin and thick plates with geometric non-linearity.

병렬 처리를 이용한 부분 시스템 기반 유연다물체 동역학의 효율적인 해석 연구 (Study on Parallel Processing for Efficient Flexible Multibody Analysis based on Subsystem Synthesis Method)

  • 한종부;송하준;김성수
    • 대한기계학회논문집A
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    • 제41권6호
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    • pp.507-515
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    • 2017
  • 많은 절점 자유도로 표현이 되는 유연다물체 시스템의 효율적인 해석을 위해서는 병렬처리 기법이 적용될 수 있다. 이 분야에서의 병렬처리기법은 주로 선형대수방정식의 효율적인 해법에 초점이 맞추어 연구가 진행되었다. 본 논문에서는 기존의 방법과는 달리 병렬처리에 적합한 유연다물체 동역학 공식을 부분 시스템 합성방법을 이용하여 개발하고, OpenMP를 사용한 효율적인 병렬처리 방식을 제안하였다. 서로 다른 두 가지 병렬처리 방식을 3개의 동일한 유연체 회전 날개 시스템 시뮬레이션 통하여 비교하였다. 또한 실제의 CPU시간을 비교하여 제안한 병렬처리 방법의 효율성을 고찰하였다.

조타에 의한 선박의 횡요 감소시스템의 개발 (Development of the Rudder Roll Control System of a Vessel in Irregular Waves)

  • 이승건;이경우;황성준;강동훈
    • 한국항해항만학회지
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    • 제29권10호
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    • pp.839-845
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    • 2005
  • 조타에 의해 불규칙파 중 선박의 선수동요 및 횡요를 제어하는 횡요 감소시스템에 관한 연구를 수행하였다. 횡요를 포함한 선박 운동 시뮬레이션을 위해 4-자유도 조종 운동방정식을 사용하였고, 선체에 가해지는 외력으로서 파강제력이 고려되었다. 파강제력은 3차원 특이점 분포법에서 얻어진 주파수 전달함수로부터 시간영역해석법을 적용하였다. 선수동요와 횡요를 제어하는 PD 제어기를 각각 구성하고, 이를 선형 결합하여 횡요 감소 조타 제어기를 구성하였다. 조타 속도 및 타의 종류를 변화시켜 선수동요 및 횡요의 제어효율을 검토하였다.

비구면 연삭 및 연마를 위한 공구 경로 제어에 관한 연구 (A Study on the Control Method for the Tool Path of Aspherical Surface Grinding and Polishing)

  • 김형태;양해정;김성철
    • 한국정밀공학회지
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    • 제23권1호
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    • pp.113-120
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    • 2006
  • This paper proposed the control algorithm fur aspheric surface grinding and was verified by the experiment. The functions of the algorithm were simultaneous control of the position and interpolation of the aspheric curve. The non-linear formula of the tool position was derived from the aspheric equations and the shape of the tool. The function was partitioned by an certain interval and the control parameters were calculated at each control section. The movement in a session was interpolated with acceleration and velocity. The position error was feed-backed by rotary encorder. The concept of feedback algorithm was correcting position error by increasing or decreasing the speed. In the experiment, two-axis machine was controlled to track the aspheric surface by the proposed algorithm. The effect of the control and process parameters was monitored. The result showed that the maximum tracking error was under sub-micro level for the concave and convex surfaces.

고속 흐름에서의 충격파와 난류경계층의 상호작용에 관한 수치적 연구 (A Numerical Study on Shock Wave Turbulent Boundary Layer Interactions in High-Speed Flows)

  • 문수연;손창현;이충원
    • 대한기계학회논문집B
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    • 제25권3호
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    • pp.322-329
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    • 2001
  • A study of the shock wave turbulent boundary layer interaction is presented. The focus of the study is the interactions of the shock waves with the turbulent boundary layer on the falt plate. Three examples are investigated. The computations are performed, using mixed explicit-implicit generalized Galerkin finite element method. The linear equations at each time step are solved by a preconditioned GMRES algorithm. Numerical results indicate that the implicit scheme converges to the asymptotic steady state much faster than the explicit counterpart. The computed surface pressures and skin friction coefficients display good agreement with experimental data. The flowfield manifests a complex shock wave system and a pair of counter-rotating vortices.

조타에 의한 선박의 횡요 감소시스템의 개발에 관한 연구 (A Study on Developing the Rudder Roll Control System of a Vessel in Irregular Waves)

  • 이승건;황성준;강동훈
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2005년도 추계학술대회 논문집
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    • pp.55-61
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    • 2005
  • 조타에 의해 불규칙파$\cdot$중 선박의 선수동요 및 횡요를 제어하는 횡요 감소시스템에 관한 연구를 수행하였다. 횡요를 포함한 선박 운동 시뮬레이션을 위해 4-자유도 조종 운동방정식을 사용하였고, 선체에 가해지는 외력으로서 파강제력이 고려되었다. 파강제력은 3차원 특이점 분포법에서 얻어진 주파수 전달함수로부터 시간영역해석법을 적용하였다. 선수동요와 횡요를 제어하는 PD 제어기를 각각 구성하고, 이를 선형 결합하여 횡요 감소 조타 제어기를 구성하였다. 조타 속도 및 타의 종류를 변화시켜 선수동요 및 횡요의 제어효율을 검토하였다.

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덕티드 팬 무인기의 동익과 정익 공력상호작용에 대한 실험적 연구 (Experimental Study on the Aerodynamic Interaction of the Rotor and Stator for the Ducted fan UAV)

  • 류민형;조이상;조진수
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.387-391
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    • 2009
  • 소형 무인항공기 추진용 덕티드 팬의 실험적 연구가 수행되었다. 이 논문에서는 덕티드 팬의 입구, 로터 뒤, 스테이터 뒤에서 허브에서 팁 방향으로 $45^{\circ}$ 경사 열선으로 측정하여 비정상 3차원 유동 특성을 연구하였다. 경사열선 요각을 고정시켜 데이터를 획득하였다. 이 데이터는 위상평균기법을 이용하여 평균되었다. 이 데이터는 Newton-Rhapson 수치해법을 통하여 3개의 비선형 연립방정식을 풀었다. 축 방향, 반경 방향 그리고 원주 방향 속도의 윤곽을 통해 팁 후류, 이차유동 그리고 팁 누설유동과 같은 유동 특성을 확인 하였다.

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Numerical simulation of single-phase two-components flow in naturally fractured oil reservoirs

  • Debossam, Joao Gabriel Souza;dos Santos Heringer, Juan Diego;de Souza, Grazione;Souto, Helio Pedro Amaral
    • Coupled systems mechanics
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    • 제8권2호
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    • pp.129-146
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    • 2019
  • The main goal of this work is to develop a numerical simulator to study an isothermal single-phase two-component flow in a naturally fractured oil reservoir, taking into account advection and diffusion effects. We use the Peng-Robinson equation of state with a volume translation to evaluate the properties of the components, and the discretization of the governing partial differential equations is carried out using the Finite Difference Method, along with implicit and first-order upwind schemes. This process leads to a coupled non-linear algebraic system for the unknowns pressure and molar fractions. After a linearization and the use of an operator splitting, the Conjugate Gradient and Bi-conjugated Gradient Stabilized methods are then used to solve two algebraic subsystems, one for the pressure and another for the molar fraction. We studied the effects of fractures in both the flow field and mass transport, as well as in computing time, and the results show that the fractures affect, as expected, the flow creating a thin preferential path for the mass transport.

네 대의 주 추진기를 이용한 무인잠수정의 속도, 심도 및 방위각 제어 - 시뮬레이션 및 실험 (Speed, Depth and Steering Control of Underwater Vehicles with Four Stem Thrusters - Simulation and Experimental Results)

  • 전봉환;이판묵;이계홍;홍석원;이지홍
    • 한국해양공학회지
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    • 제19권2호
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    • pp.67-73
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    • 2005
  • This paper describes depth, heading and speed control of an underwater vehicle that has four stern thrusters of which forces are coupled in the diving and, steering motion, as well as the speed of the vehicle. The optimal linear quadratic controller is designed based on a linearized- state space model, developed by combining the dynamic equations of speed, steering and diving motion. The designed controller gives provides an optimal thrust distribution, minimizing the given performance index to control speed, depth and heading simultaneously. To validate the performance of the controller, a simulation and tank-test are carried out with DUSAUV (Dual Use Semi-Autonomous Underwater Vehicle), developed by KORDI as a test-bed for testing new underwater technologies. Optimal gains of the controller are tuned, using a computer simulation environment with a nonlinear 6-DOF numerical DUSAUV model, developed by PMM (Planner Motion Mechanism) test. To verify the performance of the presented controller in experiment, a tank-test with DUSAUV is carried out in the ocean engineering basin in KORDI. The experimental results are also compared with the simulation results to investigate the accordance of the numerical and the real mode.