• Title/Summary/Keyword: Motion equations

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Measuring Tensions of Character Motions based on LMA (LMA를 기반으로 한 캐릭터 동작의 긴장도 측정)

  • Kwak, Chang-Sub;Kwon, Ji-Yong;Lee, In-Kwon
    • Journal of KIISE:Computing Practices and Letters
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    • v.14 no.5
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    • pp.532-536
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    • 2008
  • In this paper, we propose the method to measure tensions of character motions, using LMA (Laban Movement Analysis). Using tension values, we tan take advantage of them as a standard for synchronization of motion and BGM(Back Ground Music). In LMA, a motion is divided into 4 space-time factors which are called Efforts, and each Effort has two bases opposed to each other. We can analyze the motion by justifying which basis is stronger than the other in each Effort of motion. To measure quantitatively tension values, we propose some equations based on kinematics and dynamics. Then we can measure the tension value by the weighted sum of values calculated from those equations. Each weight can be determined by the optimization process which tries to minimize the difference between the calculated tension value and human's decision. The experimental result shows that the in creasing order of the motion tension value is similar to that of the tension score given by human.

Rollover Propensity Analysis of A Jeep Vehicle (지프차량의 전복성향 해석)

  • 백운경
    • Journal of the Korean Society of Safety
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    • v.14 no.4
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    • pp.85-92
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    • 1999
  • Vehicle rollover is an important issue for the traffic safety. Rollover can occur from the driver's action, the vehicle characteristics, or the road condition. This study is about the rollover propensity analysis of a jeep vehicle using the steering and braking maneuver, which is the combined result by the driver and the vehicle. Simple equations of roll motion is used to analyze the roll motion and a special purpose vehicle dynamics program is used to simulate the rollover of the jeep vehicle. From the simulation, an incipient rollover motion of the vehicle was found. However, the more complete rollover propensity analysis would require further investigation using roll dynamic sensitivity study.

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The Measurement of Detachment of Vane Tip in a Positive Displacement Small Vane Pump (압력 평형형 소형 베인펌프에서의 베인 이간 현상 측정)

  • 안형준;양광식;한동철;박민호
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1998.10a
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    • pp.365-370
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    • 1998
  • This paper reports on the measurement of the vane motion in a positive displacement small vane pump. The capacitive method using ceramic vane is proposed to measure the vane motion. This method enables us to measure only radial motion of the vane regardless of the motions of other directions. With simple experiments and solutions of simultaneous equations, the indirect compensation of measured signal was performed.

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Collective Motion of Interacting Simple Robot System

  • Masaki, Sano;Jung, Si
    • 제어로봇시스템학회:학술대회논문집
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    • 2001.10a
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    • pp.24.4-24
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    • 2001
  • Many livings form groups which we consider as collective systems. The collective motion of the group shows various dynamics and patterns, and many model equations are proposed to explain such phenomenon. In our previous work, We proposed simple deterministic model which shows various types of group behaviors. In this paper, we modify it in order to apply to a real robotic system. Here we assume that the space resolution of each robot´s sensors is low and that the sensors detect the nearest robots. It was confirmed the robots with modified model also shows various types of motion.

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Analysis of the Snake Motion of a Machine Tool Cross Head Assembly Travelling on Parallel Linear Motion Guides Using a Planar 2-D.O.F. Model (평면 2자유도 모델을 이용한 LMG 상에서 이동되는 Cross Head의 사행동 해석)

  • 최영휴;김성훈;정택수;장은성
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2001.10a
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    • pp.111-116
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    • 2001
  • In this paper, a simple 2 D.O.F. planar motion model is proposed in order to analyze the snake motion of a machining center cross head assembly, that is travelling on linear guide rails. In the proposed mathematical model, the friction between head and guide ways is neglected, and also the support structures including guide rails, rear- and side-panels of the machining center are assumed to be rigid. The equations of motion of the proposed model are derived and successfully solved to determine vibration responses of the head assembly due to some applied traction forces.

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Numerical Flow Visualization of Cyclic Motion of a Fling-Clapping Wing (프링-크래핑 날개의 주기적 운동에 관한 수치적 흐름 가시화)

  • Chang, Jo-Won;Sohn, Myong-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.12
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    • pp.1511-1520
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    • 2004
  • A flow visualization of the two-dimensional rigid fling-clap motions of the flat-plate wing are performed to gain knowledge of butterfly mechanisms that might be employed by butterflies during flight. In this numerical visualization, the time-dependent Navier-Stokes equations are solved for cyclic fling and clap types of wing motion. The separation vortex pair that is developed in the fling phase of the cyclic fling and clap motion is observed to be stronger than those of the fling followed by clap and pause motion(1st cycle motion). This stronger separation vortex pair in the fling phase is attributable to the separation vortex pair of the outside space developed in the clap phase as it moves into the opening in the following fling phase. Accordingly, higher lift and power expenditure coefficients in the fling after clap phase is caused by the stronger separation vortex pair.

A Study of Motion for Four-Axis Stabilized Platform Including Effects of Gimbal Bearing Friction (김벌 베어링 마찰의 영향을 고려한 4축 안정화 플랫폼의 운동에 관한 연구)

  • Shin, Y.J.;Cho, K.R.;Lee, J.K.;Cho, S.;Choi, S.
    • Journal of the Korean Society for Precision Engineering
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    • v.12 no.6
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    • pp.52-63
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    • 1995
  • This paper presents a detailed derivation of the equations of motion for the stable member of a four-axis platform. Gimbal bearing friction is considered for motion analysis. First, dynamic characteristics of platform, gimbal and gyro with Coulomb friction are studied due to vehicle's angular motion. Second, Vehicle's motion is assumed the sinusoidal function and dynamic characteristics of platform, gimbal and gyro are studied. Conclusively, considering effects of Coulomb friction, they could not follow the vehicle's angular motion and have constant errors. In case of sinusoidal motion, relative angles for each gimbal are amplified, but they are sinusoidal function with almost the same phases.

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On the Dynamics of Multi-Dimensional Lotka-Volterra Equations

  • Abe, Jun;Matsuoka, Taiju;Kunimatsu, Noboru
    • 제어로봇시스템학회:학술대회논문집
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    • 2004.08a
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    • pp.1623-1628
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    • 2004
  • In the 3-dimensional cyclic Lotka-Volterra equations, we show the solution on the invariant hyperplane. In addition, we show the existence of the invariant hyperplane by the center manifold theorem under the some conditions. With this result, we can lead the hyperplane of the n-dimensional cyclic Lotka-Volterra equaions. In other section, we study the 3- or 4-dimensional Hamiltonian Lotka-Volterra equations which satisfy the Jacobi identity. We analyze the solution of the Hamiltonian Lotka- Volterra equations with the functions called the split Liapunov functions by [4], [5] since they provide the Liapunov functions for each region separated by the invariant hyperplane. In the cyclic Lotka-Volterra equations, the role of the Liapunov functions is the same in the odd and even dimension. However, in the Hamiltonian Lotka-Volterra equations, we can show the difference of the role of the Liapunov function between the odd and the even dimension by the numerical calculation. In this paper, we regard the invariant hyperplane as the important item to analyze the motion of Lotka-Volterra equations and occur the chaotic orbit. Furtheremore, an example of the asymptoticaly stable and stable solution of the 3-dimensional cyclic Lotka-Volterra equations, 3- and 4-dimensional Hamiltonian equations are shown.

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Simulation of Motion Accuracy Considering Loads in Linear Motion Units (부하를 고려한 직선운동유니트의 정밀도 시뮬레이션 기술)

  • Khim, Gyungho;Park, Chun Hong;Oh, Jeong Seok
    • Journal of the Korean Society for Precision Engineering
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    • v.32 no.5
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    • pp.405-413
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    • 2015
  • This paper presents the motion accuracy simulation considering loads such as workpiece weight, cutting force, cogging force of a linear motor, and force caused by misalignment and runout error of a ballscrew in linear motion units. The transfer function method is basically utilized to estimate 5-DOF motion errors, together with the equilibrium equations of force and moment on the table. The transfer function method is modified in order to consider clearance changed according to the loads in the double sided hydrostatic/aerostatic bearings. Then, the analytic model for predicting the 5-DOF motion errors is proposed with the modified transfer function method. Motion errors were simulated under different loading conditions in the linear motion units using hydrostatic, aerostatic, and linear motion bearings, respectively. And the proposed analytic model was verified by comparing the estimated and measured motion errors.