• Title/Summary/Keyword: TAKE-OFF

검색결과 913건 처리시간 0.029초

절사층 총합추정을 위한 복합추정량 (An Alternative Composite Estimator for the Take-Nothing Stratum of the Cut-Off Sampling)

  • 황종민;신기일
    • Communications for Statistical Applications and Methods
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    • 제19권1호
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    • pp.13-22
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    • 2012
  • 절사표본 추출법은 절사층, 표본층, 전수층으로 모집단을 분리한 후 표본층과 전수층의 조사결과를 이용하여 전체 모집단의 총합을 추정하는 방법이다. 이 방법은 왜도가 심한 사업체조사에서 흔히 사용하는 방법이다. 절사층의 총합 추정은 전체 모집단 총합 추정에 영향을 미치므로 절사층 총합의 정확한 추정은 매우 중요하다. 최근 김지학과 신기일 (2011)은 절사층에서 소수의 표본을 추출하여 얻은 결과와 기존의 추정량에서 얻은 결과를 선형결합하는 복합추정법을 제안하였다. 본 논문에서는 최량선형불편예측(best linear unbias predictor; BLUP)을 이용한 새로운 복합추정량을 제안하였으며 모의실험을 통하여 기존의 방법과 새로운 복합 추정량의 우수성을 비교하였다.

유도 공중회전낙법의 COG변인 분석 (A COG Variable Analysis of Air-rolling-breakfall in Judo)

  • 김의환;정재욱;김성섭
    • 한국운동역학회지
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    • 제15권3호
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    • pp.117-132
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    • 2005
  • It was to study a following research of "A Kinematic Analysis of Air-rolling-breakfall in Judo". The purpose of this study was to analyze the Center of Gravity(COG) variables when performing Air-rolling-breakfall motion, while passing forward over(PFO) to the vertical-hurdles(2m height, take off board 1m height) in judo. Subjects were four males of Y. University squad, who were trainees of the demonstration exhibition team, representatives of national level judoists and were filmed by four 5-VHS 16mm video cameras(60field/sec.) through the three dimensional film analysis methods.COG variable were anterior-posterior directional COG and linear velocity of COG, vertical directional COG and linear velocity of COG. The data collections of this study were digitized by KWON3D program computed The data were standardized using cubic spline interpolation based by calculating the mean values and the standard deviation calculated for each variables. When performing the Air-rolling-breakfall, from the data analysis and discussions, the conclusions were as follows : 1. Anterior-posterior directional COG(APD-COG) when performing Air-rolling-breakfall motion, while PFO over to the vertical-hurdles(2m height) in judo. The range of APD-COG by forward was $0.31{\sim}0.41m$ in take-off position(event 1), $1.20{\sim}1.33m$ in the air-top position(event 2), $2.12{\sim}2.30m$ in the touch-down position(event 3), gradually and $2.14{\sim}2.32m$ in safety breakfall position(event 4), respectively. 2 The linear velocity of APD-COG was $1.03{\sim}2.14m/sec$. in take-off position(event 1), $1.97{\sim}2.22m/sec$. gradually in the air-top position(event 2), $1.05{\sim}1.32m/sec$. in the touch-down position (event 3), gradual decrease and $0.91{\sim}1.23m/sec$. in the safety breakfall position(event 4), respectively. 3. The vertical directional COG(VD-COG) when performing Air-rolling-breakfall motion, while PFO to the vertical-hurdles(2m height) in judo. The range of VD-COG toward upward from mat was $1.35{\sim}1.46m$ in take-off position(event 1), the highest $2.07{\sim}2.23m$ in the air-top position(event 2), and after rapid decrease $0.3{\sim}0.58m$ in the touch-down position(event 3), gradual decrease $0.22{\sim}0.50m$ in safety breakfall position(event 4), respectively. 4. The linear velocity of VlJ.COG was $1.60{\sim}1.87m/sec$. in take-off position(event 1), $0.03{\sim}0.08m/sec$. gradually in the air-top position(event 2), $-4.37{\sim}\;-4.76m/sec$. gradual decrease in the touch-down position(event 3), gradual decrease and -4.40${\sim}\;-4.77m/sec$. in safety breakfall position(event 4), respectively. When performing Air-rolling-breakfall showed parabolic movement from take-off position to air-top position, and after showed vertical fall movement from air-top position to safety breakfall. In conclusion, Ukemi(breakfall) is safety fall method Therefore, actions need for performing safety fall movement, that decrease and minimize shock and impact during Air-rolling-breakfall from take-off board action to air-top position must be maximize of angular momentum, and after must be minimize in touch-down position and safety breakfall position.

해수압 진동을 이용한 파력발전 장치 및 방법 (Apparatus and Method for Wave Energy Convertor using Under-water Pressure Oscillation)

  • 송승관;박진배
    • 전기학회논문지
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    • 제60권12호
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    • pp.2260-2264
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    • 2011
  • This paper describes the development of an wave energy convertor. We devise a new type of the wave energy convertor which generates electricity by means of under-water pressure oscillation. This wave energy convertor is installed on the seabed floor. That is, there is no exposed body on the surface of the sea. The wave energy convertor comprises an activated assembly which is adapted to be displaced in response to water pressure oscillation to vary the volume of bellows cavity and a power take off assembly which generates electricity in response to movement of the activated assembly.

인간동력 항공기 임무 형상 선정 연구 (Study on the Selection of Mission Profiles of Human Powered Aircraft)

  • 천제현;한철희
    • 융복합기술연구소 논문집
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    • 제5권1호
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    • pp.19-22
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    • 2015
  • Human powered aircraft (HPA) is an airplane that uses only human power for its propulsion. The human power as a power resource and an engine produce the available power that is very crucial to the success of the HPA. In the present paper, the human power characteristics for completing the mission profile are discussed focusing on the take-off and climbing performance. The mission profile is designed by using an athlete's power generation. It is believed that present analysis can be helpful for the mission profile design and athletes exercise program development for the HPA competitions.

프로펠러와 고양력 장치와의 공력간섭에 대한 수치해석 연구 (NUMERICAL STUDY OF PROPELLER AND HIGH LIFT DEVICE AERODYNAMIC INTERFERENCES)

  • 박영민;김철완;정진덕;이해창
    • 한국전산유체공학회지
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    • 제16권4호
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    • pp.47-54
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    • 2011
  • A rotating propeller of turboprop aircraft gives much effect on the aerodynamic characteristics of wing such as lift, moment and stall. Specially propeller effect on the wing surface is much more dominant when aircrafts are in landing or take-off conditions. In the present paper, three dimensional Navier-Stokes simulations for the interaction of propeller and wing were carried out for medium sized turboprop aircraft. For rotating propeller, unsteady sliding mesh method was used to simulate a relative motion between moving and static bodies. For the power effect analysis in landing and take off configurations, double slotted flap was also considered and the aerodynamic characteristics were investigated. It was shown that the propeller slipstream enhanced the lift slope including maximum lift by eliminating local flow separation region and this enhancement was more dominant with high lift device.

AE 신호를 이용한 HDD 슬라이더 공기베어링의 부상상태 측정 (Measurement of the Flying Characteristics of HDD Slider Air Bearing Using AE Signal)

  • 김재직;정태건
    • 대한기계학회논문집A
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    • 제25권9호
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    • pp.1391-1399
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    • 2001
  • The AE measurement is one of the most convenient methods for detecting contacts between the slider and the disk. The AE method has been widely used in the investigation of the tribology of sliding interfaces due to its convenience. We examined the relationship between the AE signal and the flying height of a slider. We investigated the influence of the disk linear velocity on the AE rms signal by using the AE measurement system. The experiment also gives the relationship between the take-off velocity and the disk surface conditions. To investigate the behavior of the slider further, the variances of the AE signals are analyzed. The experimental results indicate that the increase in the magnitude of the AE rms signal does not necessarily mean the slider/disk contacts.

Adaptive Fuzzy Controller Design for Altitude Control of an Unmanned Helicopter

  • Kim, Jong-Kwon;Park, Soo-Hong;Cho, Kyeum-Rae;Jang, Cheol-Soon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.590-593
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    • 2005
  • Unmanned Helicopter has several abilities such as vertical Take off, hovering, low speed flight at low altitude. Such vehicles are becoming popular in actual applications such as search and rescue, aerial reconnaissance and surveillance. These vehicles also used under risky environments without threatening the life of a pilot. Since a small unmanned helicopter is very sensitive to environmental conditions, it is generally known that the flight control is very difficult problems. The nonlinear adaptive fuzzy controller design procedure and its applications for altitude control of unmanned helicopter were described in the paper. This research was concentrated on describing the design methodologies of altitude controller design for small unmanned helicopter acquiring autonomous take off and vertical movement. The design methodologies and performance of the altitude controller were simulated and verified with an adaptive fuzzy controller. Throughout simulation results, I showed that the proposed adaptive controllers have enhanced control performance such as robustness, effectiveness and safety, in the altitude control of the unmanned helicopter.

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Moliere의 희극에 나타난 의상 Imagery에 관한 연구II-재치를 뽐내는 아가씨들을 중심으로- (The Study of Clothing Imagery Expressed in Moliere`s PlayII-focused on Les precieuses Ridicules-)

  • 이영숙
    • 복식문화연구
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    • 제9권3호
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    • pp.447-457
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    • 2001
  • Moliere completed classical French comedy by combining farce and commedia dell\`arte. Moliere believed that it was a plays obligation to give a lesson and entertainment. Moliere recreated commedia dell\`arte\`s typical acting patterns and characters in his work. He created with Lully comedie ballet that combined ballet and comedie for taste of Louis 14. Les precieuses ridicules critically displayed women at that time. Both contemporary high status women\`s custom and behavior were the targets of the author\`s synical criticism. There are three notable clothing imageries are shown in this work. First, Moliere used a variety of items in order to show emptiness of noble at that time. Items are ribbon and loop decorated rhingrave, feather decorated hat, perfumed wig and glove, lace covered canon and flower decorated shoes. Second, the author showed people\`s stutus through their clothes. Last, the author used clothing used clothing as a metaphor for hypocrisy. Thus when he said “take off the clothes” he meant take off hypocrisy and return truth.

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AE 신호를 이용한 HDD 슬라이더 공기베어링의 부상상태 측정 (Measurement of the Flying Characteristics of HDD Slider Air Bearing Using AE Signal)

  • 김재직;정태건
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2000년도 추계학술대회 논문집
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    • pp.97-101
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    • 2000
  • The AE measurement is one of the most convenient methods for detecting contacts between slider disk. The AE method has been widely used in the investigation of the tribology of sliding interfaces due to the convenience of using AE sensor. In this study, we examined the relationship between the AE signal and the flying height of a slider. We tried to know the influence of the disk velocity on the AE rms signal by using the AE measurement system. The experiment also gives the relationship between the take-off velocity and the disk surface state. To investigate the behavior of the slider further, the variances of the AE signal are analyzed. The results about a subambient pressure slider indicate that the increase in the magnitude of AE rms signal does not necessarily mean the slider/disk contacts.

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