• Title/Summary/Keyword: 자세변화

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Effect of Muscle Activation Change of Lower Limb According to Whole Body Vibration During Different Squat Exercises (다양한 스쿼트 자세 수행 시 전신진동자극이 하지 근 활성도에 미치는 영향)

  • Seo, S.B.;Kang, S.R.;Yu, C.H.;Min, J.Y.;Kwon, T.K.
    • Journal of rehabilitation welfare engineering & assistive technology
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    • v.8 no.1
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    • pp.33-40
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    • 2014
  • The objective of this study was to assess leg muscle activities during whole body vibration (WBV) training with various squat position exercises. Subjects performed four different squat exercises on a vibration platform (VM-10, Sonicworld Co.) Ten healthy women volunteers (age $21{\pm}1.3years$, height $160{\pm}2.1cm$, weight $52{\pm}4.6kg$) were selected. EMG signals four leg muscles were taken and analyzed. The exercises were performed both with 10 seconds WBV and without 10 seconds WBV. Muscle activities during WBV were compared with non-vibration stimulus. In the result, EMG signals caused by WBV were significantly higher (P<0.05) compared with non-vibration stimulus in all leg muscles and squat exercises. The increase in muscle activity caused by Whole body vibration was significantly higher (P<0.05) in LS and OS compared with HU&HS.

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The 3-Axis Attitude Stabilization System Design of Picosat Hausat-1 (극소형 위성 HAUSAT-1의 3축 자세 안정화 시스템 설계)

  • Seo,Seung-Won;Jeong,Nam-Suk;Jang,Yeong-Geun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.7
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    • pp.100-111
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    • 2003
  • The HAUSAT-1(Hankuk Aviation University SATellite-1) will orbit at the altitude of 650km-800 km with 65 or 98 degree inclination angle. The effects of magnetic field and Earth gravity are more predominant than other space disturbances because the HAUSAT-1 will be positioned in LEO(Low Earth Orbit). The HAUSAT-1 design implements a magnetic control system and gravity-stable system which implement the solar panel deployment system. The simulation using MATLAB was performed to make sure the attitude stability of HAUSAT-1, which is based on the 8th order magnetic field model and non-linear equations of disturbances and the HAUSAT-1 attitude. The stability is investigated for two different HAUSAT-1 configurations and attitude which are affected by disturbances through simulation. The results for gravity-gradient stable and non gravity-gradient stable system are compared. Methodology of attitude stabilization was explored to develop an effective attitude control system for the HAUSAT-1 using magnetic torquers.

Analysis of Fault Attitudes by Using Trajectories of the Maximum Longitudinal Displacement on Tunnel Face (터널 굴진면 최대 수평변위의 변화 양상에 따른 단층 자세 분석)

  • Yun, Hyun-Seok;Seo, Yong-Seok
    • The Journal of Engineering Geology
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    • v.26 no.3
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    • pp.393-401
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    • 2016
  • In the present study, fault attitudes and the locations of appearance of faults in tunnel faces were predicted by analyzing the trajectory of the maximum longitudinal displacement immediately before the appearance of faults through three-dimensional finite element analysis. A total of 28 fault attitude models were used in the analysis. Those faults that have drives with dip appear first in the upper part of tunnel faces as tunnel excavation progresses and their maximum longitudinal displacement shows a tendency to move from the middle part to the upper part of tunnel faces. Those faults that have drives against dip appear first in the lower part of tunnel faces as tunnel excavation progresses and their maximum longitudinal displacement shows a tendency to move from the middle part or middle upper part to the lower part of tunnel faces. In addition, when the dip of faults is larger the maximum longitudinal displacement moves from the left upper part toward the wall part in the case of drive with dip models and from the left lower part toward the wall part in the case of drives against dip models. Therefore, it was indicated that the attitudes of faults distributed ahead of tunnel faces and the locations where faults appear in tunnel faces can be predicted by analyzing the longitudinal displacement trajectory of tunnel faces following excavation.

The Effect of Cervical and Thoracic Joint Mobilization on the Cervical Pain, Cervical Range of Motion and Balance in Adults with Forward Neck Posture (목뼈 및 등뼈 관절가동술이 전방머리자세 성인의 목통증, 목 관절가동범위 및 균형에 미치는 영향)

  • Lee, Sang-Bin
    • Journal of Industrial Convergence
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    • v.18 no.2
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    • pp.27-35
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    • 2020
  • The purpose of this study was to investigate the effect of cervical and thoracic joint mobilization on cervical pain, cervical range of motion(ROM) and balance in adults with forward neck posture. A total 26 subjects were divided into a cervical joint mobilization group(CMG, n=13) and a thoracic joint mobilization group(TMG, n=13). performed joint mobilization three times per week for four weeks. As for changes in pain and ROM, statistically significant decrease were founded within group comparison(p<.05). In changes of static balance within group comparison, the CMG showed statically significant improvement in right foot on eyes closed(p<.05), while there were no significant changes in the TMG(p<.05). There were no significant differences were observed between group comparison(p<.05). In changes of dynamic balance within group comparison, the CMG and TMG were showed statistically significant improvement(p<.05). In conclusion, the joint mobilization on cervical and thoracic were effective on improving cervical pain, cervical range of motion and balance in adults with forward neck posture.

Consideration of Shoulder Joint's Image with the Changed Tube Angle of the Shoulder Oblique Projection in Supine Position (Supine 자세에서 Shoulder oblique촬영시 Tube angle 변화에 따른 Shoulder joint에 대한 고찰)

  • Seo, Jae-Hyun;Choi, Nam-Gil
    • Journal of radiological science and technology
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    • v.31 no.2
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    • pp.109-114
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    • 2008
  • There is a standard shoulder oblique method (Grashey method) available to view the shoulder joint. This method projects AP view of the shoulder joint so that the Humerus head's subuxation or joint degeneration can be easily visualized. However, in this view, the patients, with supine or sitting or erect position, have to keep their body obliquely. Whereas, the patients who are not well or operated, usually feel very uncomfortable to keep their body in this position and hence, we need other persons' help and much efforts will be needed to get the good quality shoulder joint view. Therefore, we thought of examining a method which shows the joint well by angling the tube to Medio-Lateral direction and without keeping the patients' one side upward in supine position. For this study, total 15 subjects with no history of neurological or psychiatric illness, were recruited for examinations. They consisted of 9 males and 6 females. Statistic group analysis was performed with ANOVA test. Scores of the evaluation of the experts were $1.10{\pm}0.54$ at $25^{\circ}$, $2.50{\pm}0.50$ at 30^{\circ}$, $2.85{\pm}0.36$ at $35^{\circ}$ and $2.33{\pm}0.47$ at $40^{\circ}$, respectively, and they were significant(p<0.05, Table 1). Joint space of the Humerus head and Scapula were well distinguished at $35^{\circ}$, $30^{\circ}$ and $40^{\circ}$ with the almost same score. However, the degree of distortion at $40^{\circ}$ was more severe than that at $30^{\circ}$. Ultimately, $30-35^{\circ}$ views were shown to yield good quality shoulder oblique images. In conclusion, this method may be very useful for the patients who are uncomfortable and for the emergency patients. In order to get similar or comparable view, the same X-tube angle is recommended to be used before and after the operation. Therefore, we hope that this new angled method seems to be efficient.

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Estimation of Thruster Efficiency for Koreasat I, II under APEMAC Operation (무궁화위성1, 2호 APEMAC을 통한 추력기 효율 추정 연구)

  • Park, Young-Woong;Park, Bong-Kyu;Nam, Moon-Gyung;Bang, Hyo-Choong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.8
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    • pp.141-147
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    • 2002
  • Estimation of thrusters efficiency is a very important process at the end of lifetime of a satellite. This paper introduces a technique to estimate the efficiency change of thrusters considering bubble effect for Koreasat I. During APEMAC(Automatic Pitch Error/ Momentum Adjust Control), the change in thruster efficiency is estimated to compare the attitude telemetry data of the Koreasat I with the results of the control logic using Simulink. The outcome of this study is expected to contribute to improving the operational load at the end of generic communication satellite mission.