• 제목/요약/키워드: Takeoff

검색결과 189건 처리시간 0.024초

관계네트워크의 정보 확산에서 혁신자와 허브가 Early Takeoff와 확산크기에 미치는 영향 연구 (Influence of Innovator or Hub in Relational Network to Early Takeoff and Diffusion Size at Takeoff)

  • 옥경영
    • 한국콘텐츠학회논문지
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    • 제12권9호
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    • pp.348-356
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    • 2012
  • 본 연구는 SNS와 같은 관계네트워크의 구성원 중에서 혁신자와 허브가 정보 확산 초기 발생하는 이른 도약(early takeoff)과 도약시점의 확산크기에 어떠한 영향을 미치는 지를 파악하는 것을 목적으로 한다. 이를 위해 본 연구는 다음과 같이 가설을 설정하였다-가설 1은 네트워크에서 혁신자 와 허브는 이른 도약(early takeoff)에 영향을 미칠 것이다, 가설 2는 네트워크에서 혁신자와 허브는 도약시점의 확산크기에 영향을 미칠 것이다. 가설을 검증하기 위해 우리나라 SNS중에서 C사이트를 대상으로 로그데이터를 수집하여 혁신자와 허브를 추출하고 이들의 정보 수용행동을 다항로짓분석 및 회귀분석하였다. 그 결과, 네트워크에서 허브는 이른 도약과 도약시점의 확산크기에 모두 긍정적인 영향을 미치며, 혁신자는 확산크기에만 긍정적인 영향을 미치는 것으로 나타났다. 또한 허브는 혁신자 보다 이른 도약과 도약시점의 확산크기에 있어 상대적인 영향이 더 큰 것으로 나타났다. 이러한 결과는 네트워크에서 허브는 높은 연결성을 통해 자신의 정보수용행동을 빠른 시간에 관계네트워크내 구성원들에게 확산시킬 수 있기 때문인 것으로 보인다. 이러한 결과를 바탕으로 몇 가지 시사점과 한계점을 토의하였다.

실무 기반 건축공사 물량산출 교육용 컨텐츠 개선 방안에 관한 연구 (A Study on the Improvement of Practice-based Construction Quantity Takeoff Educational Contents)

  • 박지환;최창훈;한충희;이준복
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2015년도 춘계 학술논문 발표대회
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    • pp.217-218
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    • 2015
  • There are various standards and manuals on the quantity takeoff for construction estimation. However, a lot of time and money has been spent on retraining because of difference between practice and education. Therefore, the main purpose of this paper is to suggest improvement to analyze problems and limitations of the existing educational content for quantity takeoff. In order to achieve research objective, comparative analysis for quantity takeoff contents is carried out. This study will be extended to assist in effective quantity takeoff in building projects by supplementing the existing issues with quantity takeoff contents and developing a BIM-based quantity takeoff multimedia contents that use diverse media to increase the understanding on the subject for a non-professional.

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국외 8m 이상 멀리뛰기 선수와 국내 선수들의 운동학적 비교 분석 (The Kinematic Comparison and Analysis between National Long Jumpers and Foreign long Jumpers with record of over 8 meter)

  • 류재균;장재관
    • 한국운동역학회지
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    • 제15권3호
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    • pp.133-142
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    • 2005
  • The purpose of this study was to compare of the kinematic variables from takeoff preparation to takeoff used by long jumpers who recorded over 8meters in 2002 Busan Asian Game and 2003 Daegu Universiade and 2001 national championship. The kinematic characteristics from the last three stride to takeoff at the takeoff board were analyzed such as velocities, heights and angles. The conclusion were as follows; In order to record over 8meters the national long jumpers should have under 5cm height variation at the penultimate stride of the run-up. In the approach phase the horizontal velocity of the jumpers should reach to 10m/s in touchdown at takeoff board The vertical velocity must have 3.75m/s simultaneously in order to record 8meters. The jumpers need to continue talent of the horizontal velocity in touchdown at takeoff board and require jumping power of the takeoff leg at takeoff board The appropriate body variation range ratio between takeoff and touchdown should be 1.2 vs 1 and the trunk angle at touch down on the board should be close to the erect posture for higher body flight.

항공기 이륙중량 추정을 위한 관련 요인 분석 (B737-800을 중심으로) (Analysis of Associated Factors for Aircraft Takeoff Weight Estimation (Based on B737-800))

  • 이승표;구성관
    • 한국항행학회논문지
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    • 제27권5호
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    • pp.658-665
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    • 2023
  • 이륙중량은 항공기의 탄소 배출량과 연료 소모량을 추정할 때 정확도를 향상시킬수 있는 중요한 열쇠이다. 하지만 이륙중량은 항공사의 경영전략을 유추할 수 있는 민감한 유상하중 정보가 포함되어 있어 외부 유출이 불가능하다. 선행연구에서 이륙중량을 추정할 수 있는 몇 가지 모델이 제시되었지만, 연구자는 알 수 없는 조종사가 설정하는 변수들에 의해 연구의 한계가 존재한다고 지적한다. 본 연구에서는 이러한 한계를 통제할수 있는 방법을 제시하기 위해 이륙중량과 연관된 여러 변수를 확인하였다. 그중 이륙중량의 정확도를 향상시킬수 있는 변수를 선별하였고 이를 상용화된 ADS-B 정보에 적용하여 추정 방법을 제시한다. 제시하는 추정 식은 평균적인 이륙중량을 추정하는 것이 아니라 이륙중량 범위 내의 모든 구간에서 추정을 할 수 있다.

군용항공기의 이.착륙 패턴에 따른 소음 영향 분석 (Analysis of the Noise Effects due to the Variation of Military Aircraft Flight Patterns of Takeoff and Approach)

  • 이진영;이찬;길현권
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 춘계학술대회논문집
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    • pp.626-629
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    • 2008
  • The present study investigates the effect of the flight patterns of military aircraft for takeoff and approach on noise map. Aircraft noise modeling and simulation have been made on a Korean military airport by INM(Integrated Noise Model). The flight path of a military aircraft is modeled with takeoff, overfly, approach and touch-and-go modes. The present INM simulations are conducted for various cases with change of different takeoff and approach modes. It show that the change of takeoff and approach modes can cause considerable noise effects on the noise influence region around the airport.

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음성지시 기반 항공기 이륙 시스템의 구현 (Realization of Aircraft Takeoff Systems Based on Voice Instructions)

  • 양청일;전병규;임상석
    • 한국항행학회논문지
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    • 제12권6호
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    • pp.559-566
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    • 2008
  • 본 논문에서는 UAV를 포함한 모든 항공기를 위한 음성지시기반의 새로운 이륙시스템의 구현을 제안한다. 본 이륙제어 시스템은 음성인식, 환경결정, 명령수행으로 구성된다. 음성인식기술을 도입함으로써 제안된 이륙시스템은 조종사에게 단순화된 이륙과정과 더욱 신뢰할 수 있는 편리한 이륙제어 수단을 제공한다. 이 새로 제안된 음성인식기반 이륙 시스템은 이륙과정에서 발행할 수 있는 조종사 실수나 출발지연과 같은 문제를 감소시킴으로써 사고를 예방할 수 있고 궁극적으로는 항공안전에 크게 기여할 수 있다는 장점을 갖는다.

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달리기시 최고 속도 및 피로 구간의 3차원 동작 분석 (3-Dimensional Analysis of the Running Motion in the Max-Velocity Phase and the Fatigue Phase During 400m Sprint by Performed Elementary School Athletes)

  • 배성제
    • 한국운동역학회지
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    • 제16권4호
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    • pp.115-124
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    • 2006
  • This study was conducted to investigate the running motion in the max-velocity phase(150-160m) and the fatigue phase(350-360m) during 400m sprint by performed elementary school athletes. Eighteen elementary school male athletes who achieved at least the 3rd place in the sprint at the Korea Gangwon-Do elementary school track and field meetings during 2004 and 2005 were selected as subjects. The running motions performed by the subjects were recorded using two 8mm high speed cameras at the nominal speed of 100 frames per second. The Direct Linear Transformation technique was adopted from the beginning of filming to the final stage of data extraction. KWON 3D motion analysis package program was used to compute the 3 Dimensional coordinates, smoothing factor in which lowpass filtering method was used and cutoff frequency was 6.0 Hz. The movement patterns during foot touchdown and takeoff for the running stride were related with the biomechanical consideration. Within the limitations of this study it is concluded: In order to increase running velocity, several conditions must be fullfilled at the instant of leg touchdown and takeoff during the fatigue phase(350-360m). First, the body C.O.G(Center of Gravity) height should be raised at the instant of leg touchdown and takeoff during the fatigue phase. Second, the foot contact time should be shortened and the takeoff distance should be increased at the foot takeoff during the fatigue phase. Third, the shank angular velocity with respect to a transverse axis through the center of gravity should be increased during the leg touchdown and takeoff in the fatigue phase. Forth, the active landing style described as clawing the ground with the sole of the foot should be performed during the leg touchdown and takeoff in the fatigue phase) phase. Fifth, In order to increase running velocity in the fatigue phase while taking a slightly greater leg knee angle and body lean angle within the range of the subject's running motion during the fatigue phase would result in greater flight distance.

B747-8 Automatic Speedbrake Control System에 대한 해석적 연구 (Commentary Study on Automatic Speedbrake Control System of B747-8)

  • 문봉섭;남명관;최연철
    • 한국항공운항학회지
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    • 제26권3호
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    • pp.40-47
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    • 2018
  • Reducing aircraft speed is the important task in the Rejected Takeoff and/or landing process. It is known that the effect of the Speedbrake is most important factor during the rejected takeoff maneuver in particular near V1 on the critical field length runway. The B747 designer created Automatic Speedbrake Control System to relieve pilot workload, improves brake operation and ensures proper Speedbrake operation for rejected take off. However, those who make the Rejected Takeoff procedure ignored the Automatic function and made it does all manual operations. This lets procedures difficult, complicated, and a cause of confusion and pilot error. This study was conducted to commentary the mechanism and function of the Automatic Speedbrake Control System of B747-8 and to propose appropriate B747-8 Rejected Take off procedures for its function to reduce the workload of pilots and contribute to reduce the possibility of pilot error during Rejected Takeoff.

항공기 이륙추력 감소법 적용 (Application of Aircraft Reduced Takeoff Thrust Method)

  • 노건수
    • 한국항공운항학회지
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    • 제15권3호
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    • pp.70-76
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    • 2007
  • The benefits for using reduced takeoff thrust are many, ranging from lower maintenance and operating costs to improved engine and dispatch reliabilities. Some pilots, however, are apprehensive about using reduced thrust. They are particularly reluctant to use the maximum permissible level of reduced thrust. Two common arguments are (1)If reduced thrust is used, then the airplane will not be able to clear the obstacles if an engine fails during takeoff, and (2)If the maximum allowable assumed temperature is used, then there will be no stopping margin left if the takeoff is aborted. There is the notion that using reduced thrust sacrifices safety. The intent of this discussion is to: (1)Show that reduced thrust performance meets all regulatory requirements (2)Show that the Assumed Temperature method includes inherent extra performance margins (3)Show how to maximize performance margins while maximizing thrust reduction.

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