• Title/Summary/Keyword: Relative distance

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Effects of Source Correlation on Plates Driven by Multi-point Random Forces (불규칙 작용힘들간의 Correlation이 평판의 진동레벨에 미치는 영향)

  • Oh, S.G.;Park, J.D.;Kwak, C.S.
    • Journal of the Korean Society for Precision Engineering
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    • v.11 no.1
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    • pp.166-176
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    • 1994
  • The problem of reducing the vibration level of elastic plates driven by multiple random point forces is analyzed in this study. First, the analytical solution for the vibration level of finite thin plates with four simply supported edges under the action of multiple random point force is derived. By assuming the plates to be lightly damped, an approximate solution for the vibration level of the plate is obtained. A numerical study is carried out to determine an optimal spacing distance between the multiple point forces in order to produce a relative minimum in the plate's vibration level. The optimal spacing distance is shown to depend on the given excitation band. The effects of wave cancellation in the near field of the multiple point forces are discussed by using the equivalence of certain stationary random responses and deterministic pulse responese.

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Probabilistic analysis of structural pounding considering soil-structure interaction

  • Naeej, Mojtaba;Amiri, Javad Vaseghi
    • Earthquakes and Structures
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    • v.22 no.3
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    • pp.289-304
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    • 2022
  • During strong ground motions, adjacent structures with insufficient separation distances collide with each other causing considerable architectural and structural damage or collapse of the whole structure. Generally, existing design procedures for determining the separation distance between adjacent buildings subjected to structural pounding are based on approximations of the buildings' peak relative displacement. These procedures are based on unknown safety levels. This paper attempts to evaluate the influence of foundation flexibility on the structural seismic response by considering the variability in the system and uncertainties in the ground motion characteristics through comprehensive numerical simulations. Actually, the aim of this study is to evaluate the influence of foundation flexibility on probabilistic evaluation of structural pounding. A Hertz-damp pounding force model has been considered in order to effectively capture impact forces during collisions. In total, 5.25 million time-history analyses were performed over the adopted models using an ensemble of 25 ground motions as seismic input within OpenSees software. The results of the study indicate that the soil-structure interaction significantly influences the pounding-involved responses of adjacent structures during earthquakes and generally increases the pounding probability.

Dynamic Behavior Analyses of Bridges under Seismic Excitations in 2-Dimensional Directions (이차원 지진성분을 고려한 교량시스템의 지진거동분석)

  • 김상효
    • Proceedings of the Earthquake Engineering Society of Korea Conference
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    • 2000.10a
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    • pp.333-340
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    • 2000
  • Dynamic response behaviors of a bridge are examined under seismic excitations in the 2-dimensional directions are examined. A three-dimensional mechanical model is utilized and the corresponding equations of motions are derived to consider the two directional bridge motions due to the randomness residing in the excitation directions. The arbitrary 2-dimensional directions are simulated by applying two independent excitations in the two directions: main direction(longitudinal) ; the additive direction normal to the main (transverse). The rotational superstructure motions due to the spacial motions of the bridge are considered by admitting the deformation of the bearings at supports. The relative displacement to the ground motions and the relative distance between adjacent oscillators are found to be increased by a considerable amount in the case when considering arbitrary directional seismic excitations. It is also found that the piermotions show more complicated behaviors due to the arbitrary seismic directions.

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Relative relocation of Tadzhi kistan-Sin kiang events (타치키스탄 - 신강 지역 지진의 진앙에 대한 상대적 위치 결정)

  • 신진수;박창업
    • The Journal of Engineering Geology
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    • v.2 no.2
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    • pp.166-172
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    • 1992
  • Sixty Tadzhikistan-Sinkiang events occurred from the year 1966 to 1978 were relocated using relative location method with one reference event technique. Since the area covered by the events is about $300{\;}{\times}400{\;}km$, the region is subdivided into four. Each one has one reference event with accurate hypocenter location and travel time. The result shows average 0.3 change of distance.

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Statistical tests for biosimilarity based on relative distance between follow-on biologics for ordinal endpoints

  • Yoo, Myung Soo;Kim, Donguk
    • Communications for Statistical Applications and Methods
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    • v.27 no.1
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    • pp.1-14
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    • 2020
  • Investigations of biosimilarity between reference drugs and test drugs required statistical tests; in addition, statistical tests to evaluate biosimilarity have been recently proposed. Ordinal outcome data has been observed in research; however, appropriate statistical tests to deal with ordinal endpoints for biosimilar have not yet been proposed. This paper extends existing design for ordinal endpoints. Using measure of nominal-ordinal association and relative distances between drugs are defined so that testing procedures are developed. Through simulation studies, we investigate type I error rate and power to show the performance of our suggested method. Furthermore, a comparison between the statistical tests and other designs is proviede to show significance of ordinal endpoints.

Optimal Control for Proximity Operations and Docking

  • Lee, Dae-Ro;Pernicka, Henry
    • International Journal of Aeronautical and Space Sciences
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    • v.11 no.3
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    • pp.206-220
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    • 2010
  • This paper proposes optimal control techniques for determining translational and rotational maneuvers that facilitate proximity operations and docking. Two candidate controllers that provide translational motion are compared. A state-dependent Riccati equation controller is formulated from nonlinear relative motion dynamics, and a linear quadratic tracking controller is formulated from linearized relative motion. A linear quadratic Gaussian controller using star trackers to provide quaternion measurements is designed for precision attitude maneuvering. The attitude maneuvers are evaluated for different final axis alignment geometries that depend on the approach distance. A six degrees-of-freedom simulation demonstrates that the controllers successfully perform proximity operations that meet the conditions for docking.

Numerical Analysis on the Development of an Undularbore (Undular Bore의 발생과정에 관한 수치 해석)

  • Bea, Heon-Meen;Kim, In-Chull
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.22 no.2
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    • pp.31-35
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    • 1986
  • A bore is a transition between different uniform flows of water. If a long wave of elevation travels in shallow water it steepens and forms a bore. The bore is undular if the change in surface elevation of the wave is less than 0.28 of the original depth of water. This paper describes the growth of an undular bore from a long wave which forms a gentle transition between a uniform flow and still water. A physical account of its development is followed by the results of numerical calculations. Finite-difference approximations are used in the partial differential equations of motion. For undular bores, numerical calculations show that (i) the relationship between relative elevation and relative velocity given by long wave theory is approached for an undular bore, (ii) the amplitude of first crest of an undular bore approaches a finite limit approximately at an exponential rate, and (iii) the distance between the first two crests increases without bound, approximately logarithmically.

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Characterization of Plasma Sprayed $Cr_2O_3$ Coatings ($Cr_2O_3$계 용사분말의 제조조건 및 용사거리에 따른 플라즈마 용사 코팅층의 특성)

  • 김의준
    • Journal of Powder Materials
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    • v.6 no.3
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    • pp.224-230
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    • 1999
  • Oxide powders of $Cr_2O_3 \;and\;Cr_2O_3+3{\%}TiO_2$ were prepared by spray drying, plasma densification and fused+crushed processes. The oxide coating layers were made by plasma spray and characterized by microstructure, hardness, adhesion strength and relative density. The optimum spray distance for the high quality coatings by spraying dried powders was found to be 9cm. A small amount addition of $TiO_2\;in\;Cr_2O_3$ powder significantly improved coating characteristics by lowering the melting point of powders. The hardness and relative density of coating layers of the plasma densified powders were comparable to fused and crushed powders, however, the adhesion strength was much higher in the former case.

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Controller Design using Sliding Mode Techniques for Satellite Formation Flying

  • Lim, Hyung-Chul;Bang, Hyo-Choong;Park, Kwan-Dong;Park, Pil-Ho;Jo, Jeong-Ho
    • Bulletin of the Korean Space Science Society
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    • 2003.10a
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    • pp.41-41
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    • 2003
  • Satellite formation flying is currently an active area of research in the aerospace engineering. There are many categories for this research such as the determination of initial conditions, formation keeping, configuration and reconfiguration. In this study, a tracking controller using sliding mode techniques is designed to control a satellite for the satellite formation flying. In general, Hill's equations are used to describe the relative motion of the follower satellite with respect to the leader satellite. But, the modified Hill's equations considering J2 perturbation were used for the design of sliding mode controller. Sliding mode control law causes the chattering phenomenon because it is a discontinuous control. Dead-zone was used to avoid the chattering. The Extended Kalman filter was applied to estimate the state vector based on the measurements of relative distance and velocity between two satellites.

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Control Design for Fuel-Optimal Formation Keeping

  • Lee, Woo-Kyoung;Yoo, Sung-Moon;Park, Sang-Young;Park, Kyu-Hong
    • Bulletin of the Korean Space Science Society
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    • 2003.10a
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    • pp.42-42
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    • 2003
  • Satellite formation flying is the placing of multiple satellites into nearby orbits to form 'clusters' of satellites. These clusters of satellites usually work together to accomplish a mission. There are many benefits to using multiple satellite as opposed to one large satellites such as increasing productivity. reducing mission and launch cost. Hill's equations are useful to describe the relative motion of two satellites in formation flying, however. the disturbance forces acting on satellites is not considered in that equations. In this paper, a method for maintaining the relative distance between satellites is presented, which used mean orbital elements considering J2 perturbation. Control design process is also presented for minimizing total fuel consumption.

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