• 제목/요약/키워드: force balance test

검색결과 146건 처리시간 0.026초

Comparison of postural control between subgroups of persons with nonspecific chronic low back and healthy controls during the modified Star Excursion Balance Test

  • Shallan, Amjad;Lohman, Everett;Alshammari, Faris;Dudley, Robert;Gharisia, Omar;Al-Marzouki, Rana;Hsu, Helen;Daher, Noha
    • Physical Therapy Rehabilitation Science
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    • 제8권3호
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    • pp.125-133
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    • 2019
  • Objective: To compare the postural control between non-specific chronic low back pain (NSCLBP) subgroups and healthy people during dynamic balance performance using a modified Star Excursion Balance Test (mSEBT). Design: Cross-sectional study. Methods: Eighteen NSCLBP subjects (9 active extension pattern [AEP], 9 flexion pattern [FP]), and 10 healthy controls were enrolled in this study. All subjects performed mSEBT on their dominant leg on a force plate. Normalized reach distance and balance parameters, including the center of pressure (COP) displacement and velocity, were recorded. Results: There were significant differences in mean reach distances in both posterolateral and posteromedial (PM) reach directions between AEP and healthy subjects (p<0.001) and between FP and healthy subjects (p<0.001). However, there were no significant differences among the three groups in the anterior reach direction. Also, the results showed no significant differences in mean COP variables (velocity and displacement) between pooled NSCLBP and healthy subjects. However, the subjects were reclassified into AEP, FP and healthy groups and the results showed a significant difference in mean COP velocity in the PM direction between AEP and FP subjects (p=0.048), and between AEP and healthy subjects (p=0.024). Conclusions: The findings in this study highlight the heterogeneity of the individuals with NSCLBP and the importance of identifying the homogenous subgroups. Individuals with AEP and FP experience deficits in dynamic postural control compared to healthy controls. In addition, the findings of this study support the concept of the Multidimensional Classification System.

Field Adaptability Test for the Full Load Rejection of Nuclear Turbine Speed Controllers using Dynamic Simulator

  • Choi, In-Kyu;Kim, Jong-An;Woo, Joo-Hee
    • 조명전기설비학회논문지
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    • 제23권7호
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    • pp.67-74
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    • 2009
  • This paper describes the speed control functions of the typical steam turbine speed controllers and the test results of generator load rejection simulations. The goal of the test is to verify the speed controller's ability to limit the steam turbine's peak speed within a predetermined level in the event of generator load loss. During normal operations, the balance between the driving force of the steam turbine and the braking force of the generator load is maintained and the speed of the turbine-generator is constant. Upon the generator's load loss, in other word, the load rejection, the turbine speed would rapidly increase up to the peak speed at a fast acceleration rate. It is required that the speed controller has the ability to limit the peak speed below the overspeed trip point, which is typically 110[%] of rated speed. If an actual load rejection occurs, a substantial amount of stresses will be applied to the turbine as well as other equipments, In order to avoid this unwanted situation, not an actual test but the other method is necessary. We are currently developing the turbine control system for another nuclear power plant and have plan to do the simulation suggested in this paper.

회전 발사체용 마그너스 효과 특정기법의 개발 (Development of Magnus Effect Measurement Technique for Spinning Projectile)

  • 오세윤;김성철;이도관;최준호;안승기
    • 한국항공우주학회지
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    • 제35권1호
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    • pp.79-86
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    • 2007
  • 회전 발사체용 마그너스 효과 풍동실험 측정장치를 개발하였다. 국방과학연구소 풍동실험실에서는 고속풍동실험에 앞서 지상기능시험과 마그너스 저속풍동실험을 수행하였으며 마그너스 모형은 분당 약 6,000~10,000 회전하였으며, 속도 100 m/sec에서 측정한 마그너스 효과는 무차원 회전특성인자에 대해 선형적인 변화특성을 보였다. 동일형상 모형에 대해 미국 AEDC-4T 풍동에서 기 수행하였던 마그너스 측정결과와의 비교검토를 수행하였다.

외바퀴 로봇 다이나믹 모델과 성능 개선 (Dynamic Modeling and Performance Improvement of a Unicycle Robot)

  • 김성하;이재오;황종명;안부환;이장명
    • 제어로봇시스템학회논문지
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    • 제16권11호
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    • pp.1074-1081
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    • 2010
  • Today, the research related to the robot is achieved in various part. With the high interest in means of transport, various researches about autonomous mobile robot and next generation transport is continuing. The unicycle robot among these needs much control technique like balance control model and driving model. For autonomous driving of this unicycle robot, from the basic balance control to direction switching control and velocity control are needed. But the environment elements like a gradient and frictional force or unbalanced elements from the structural feature. The unicycle needs the real time balance control so more complex, harder to control. And when functional addition is made, the problem that fall entire reaction velocity or accuracy would be happen. This paper introduces entire dynamics modeling of the unicycle robot and reduced model. And propose the new balance control algorithm using fuzzy controller. Also the evaluation about performance would be made through the test.

화포에 의해 손상된 날개의 공력특성에 관한 연구 (A Study on the Aerodynamic Characteristic of Gunfire Damaged Airfoil)

  • 이기영;정형석;김시태
    • 한국군사과학기술학회지
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    • 제11권2호
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    • pp.144-151
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    • 2008
  • An experimental study has been conducted to investigate the effects of circular damage hole on the characteristics of airfoil performance. The damage on a wing created from a hit by anti-air artillery was modeled as a circular hole. Force balance measurements and static pressure measurements on the wing surface were carried out for the cases of having damage holes of 10% chord size at quarter chord and/or half chord positions. All experiments were conducted at Reynolds number of $2.85\times10^5$ based on the chord length. The surface pressure data show big pressure alterations near the circular damage holes. This abnormal surface pressure distribution produces shear stress that could lead to the acceleration of the structural degradation of the wing around the circular damage hole. However, in spite of the existence of circular damage holes, the measured force data indicated the only a slight decrease in lift accompanied by increase in drag compared to the results of undamaged one. The influence of damage hole on the aerodynamic performance was increased as the location of damage moved to the leading edge. The effect on the control force was insignificant when the damaged size was not large.

TENS 적용과 균형운동이 여성노인의 균형능력에 미치는 효과 비교 (Comparison of the Effects on Balance Abilities in the Women Elderly with Application TENS versus Balance Training)

  • 이승원;이완희
    • 한국노년학
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    • 제30권3호
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    • pp.993-1003
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    • 2010
  • 본 연구는 여성노인을 대상으로 8주간의 경피신경자극(TENS)과 균형운동을 적용하여 균형 능력의 개선 여부를 알아보고자 하였다. 노인대학에 참여한 65세 이상의 여성노인 42명을 연구대상자로 선정하였다. 대상자는 무작위로 두 그룹으로 나누어 TENS군(21명, 84.53세)과 균형운동군(21명, 79.93세)으로 진행하였다. TENS의 적용과 균형운동은 8주 동안 주 3회에 걸쳐 연구자에 의해 실시하였다. 실험 전과 후에는 동적균형검사로 일어나 걸어가기 검사 (TUG)와 정적균형검사로 힘판을 이용하여 맨 바닥과 foam 위에서의 자세 동요 속도와 기능적 팔 뻗기 검사 (FRT)와 측방 기능적 팔 뻗기 검사 (LFRT)를 시행하여 다음과 같은 결과를 얻었다. TUG는 두 군 모두 유의하게 감소되었고(p<.05), 힘판을 이용한 자세동요 속도에서도 두 군 모두 모든 조건에서 유의하게 감소되었다(p<.05). FRT와 LFRT는 두 군 모두 유의하게 증가하였다(p<.05). TUG와 눈 감은 상태의 자세동요 속도는 두 군 간의 유의한 차이를 나타냈다(p<.05). 체성감각이 떨어져 있는 여성노인에게 적용한 TENS는 균형능력 증진에 효과적인 것으로 나타났다.

Numerical study on self-sustainable atmospheric boundary layer considering wind veering based on steady k-ε model

  • Feng, Chengdong;Gu, Ming
    • Wind and Structures
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    • 제30권1호
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    • pp.69-83
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    • 2020
  • Modelling incompressible, neutrally stratified, barotropic, horizontally homogeneous and steady-state atmospheric boundary layer (ABL) is an important aspect in computational wind engineering (CWE) applications. The ABL flow can be viewed as a balance of the horizontal pressure gradient force, the Coriolis force and the turbulent stress divergence. While much research has focused on the increase of the wind velocity with height, the Ekman layer effects, entailing veering - the change of the wind velocity direction with height, are far less concerned in wind engineering. In this paper, a modified k-ε model is introduced for the ABL simulation considering wind veering. The self-sustainable method is discussed in detail including the precursor simulation, main simulation and near-ground physical quantities adjustment. Comparisons are presented among the simulation results, field measurement values and the wind profiles used in the conventional wind tunnel test. The studies show that the modified k-ε model simulation results are consistent with field measurement values. The self-sustainable method is effective to maintain the ABL physical quantities in an empty domain. The wind profiles used in the conventional wind tunnel test have deficiencies in the prediction of upper-level winds. The studies in this paper support future practical super high-rise buildings design in CWE.

한국무용 숙련자와 미숙련자에 따른 폐기능, 부드러움, 그리고 지면반력의 차이 분석 (The Analysis of Differences in Pulmonary Functions, Jerk Cost, and Ground Reaction Force Depending on Professional and Amateur Dancers in Korea Dance)

  • 박양선;김미예;이성노
    • 한국운동역학회지
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    • 제24권4호
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    • pp.349-357
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    • 2014
  • The purpose of this study was to examine the differences in the performance of dancing motions depending on the level of skill by investigating pulmonary functions, ground reaction force, and jerk cost. The subjects of this study were 12 professional dancers (career: 16 yrs) and 12 amateur dancers (career: 9 yrs) who had similar physical conditions. We selected four motion phases which included the diagonal line motion, the deep flexion motion, the breath motion, and the turn motion with one leg after a small step walking motion, with Goodguri Jangdan. In the experiment, 6 infrared cameras were installed in order to analyze the value of the jerk costs and the force plate form. Finally, we measured the pulmonary functions of the subjects. For data analysis, independent t-tests according to each event, were carried out in the data processing. According to the results of FVC % Predicted, the professional dancers showed greater lung capacities than the amateur dancers, indicating that the level of dancing skill influences lung capacity. Based on the result of the balance test, the professional dancers used more vertical power than did the amateur dancers when performing maximal flexion motion. The professional dancers used a propulsive force of pushing their body forward by keeping the center of body higher while the amateur dancers used a braking power by keeping their bodies backward. When performing medial-lateral movements, the amateur dancers were less stable than the professional dancers. There were no differences in values of jerk costs between the amateur dancers and the professional dancers.

미사일 모델의 피치 동안정미계수 측정을 위한 강제진동기법의 적용 (Application of Forced Oscillation Technique for Pitch Dynamic Stability Derivatives of a Missile Model)

  • 김승필;조환기;백승욱
    • 한국군사과학기술학회지
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    • 제3권2호
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    • pp.81-87
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    • 2000
  • This paper presents an application of forced oscillation technique to measure pitch dynamic stability derivatives of a missile model in the low speed wind tunnel. The missile model is oscillated by D.C. electric servomotor with constant amplitudes and frequencies. Phase shift is determined as the difference of peak values between input and output signals from the dynamic stability balance installed at the center of gravity of the model. Stability derivatives were calculated by using phase shifts, amplitudes, forcing moments and input frequencies. Test results show the proper usage of the force oscillation technique with good damping effects.

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Mean wind loads on T-shaped angle transmission towers

  • Guohui Shen;Kanghui Han;Baoheng Li;Jianfeng Yao
    • Wind and Structures
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    • 제38권5호
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    • pp.367-379
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    • 2024
  • Compared with traditional transmission towers, T-shaped angle towers have long cross-arms and are specially used for ultrahigh-voltage direct-current (UHVDC) transmission. Nevertheless, the wind loads of T-shaped towers have not received much attention in previous studies. Consequently, a series of wind tunnel tests on the T-shaped towers featuring cross-arms of varying lengths were conducted using the high-frequency force balance (HFFB) technique. The test results reveal that the T-shaped tower's drag coefficients nearly remain constant at different testing velocities, demonstrating that Reynolds number effects are negligible in the test range of 1.26 × 104-2.30 × 104. The maximum values of the longitudinal base shear and torsion of the T-shaped tower are reached at 15° and 25° of wind incidence, respectively. In the yaw angle, the crosswind coefficients of the tower body are quite small, whereas those of the cross-arms are significant, and as a result, the assumption in some load codes (such as ASCE 74-2020, IEC 60826-2017 and EN 50341-1:2012) that the resultant force direction is the same as the wind direction may be inappropriate for the cross-arm situation. The fitting formulas for the wind load-distribution factors of the tower body and cross-arms are developed, respectively, which would greatly facilitate the determination of the wind loads on T-shaped angle towers.