• Title/Summary/Keyword: Takeoff

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BIM기반 건축적산 매뉴얼 개발을 위한 만족도 분석에 관한 연구 (Study on the Satisfaction Analysis for Development of Construction Estimating Manager based on 3D Data)

  • 최창훈;이준복;한충희;소지윤
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2014년도 추계 학술논문 발표대회
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    • pp.222-223
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    • 2014
  • According to the improvement of IT technology, an enhanced efficiency of management system in the construction industry is expected since a quotation system with BIM (Building Information Modeling) technique effectively estimates construction materials. For an enhanced efficiency of management system, related guidelines, standards, and manuals based on BIM are required, but the lack of this information causes difficulty to utilize in practice. In the paper, the satisfaction analysis was performed in order to promote the completeness of construction estimating manager that can be presented criteria and details of BIM-based quantity-takeoff, classification criteria.

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공항의 신뢰성 향상을 위한 최적 주기장 배정과 운영지원시스템 (Optimizing Gate Assignment and Operation Support System for Reliability Improvement of Airport)

  • 이희남;이창호
    • 대한안전경영과학회:학술대회논문집
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    • 대한안전경영과학회 2004년도 추계학술대회
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    • pp.221-227
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    • 2004
  • This study develops a improved gate assignment algorithm and decision support system using its algorithm to extract a assignment result minimizing a walking distance of passengers in airport and maximizing the utilization rate of avaliable gates in domestic airports. By operation support system, it may contribute greatly in efficient enlargement of airport operation and increase the airport reliability through quickly coping with takeoff and landing delay of flight due to weather change, preservation and repair of gate, etc. Also, passengers who use airport terminal can minimize time and walking distance for departure, arrival, and transit, and it may greatly reduce the additional operation cost for common gates through maximizing the utilization rate for exclusive usage gates for airplanes which use gates.

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아두이노를 이용한 틸트 프롭형 비행체 구현 (Implementation of Tilt Prop Vehicle using Arduino)

  • 박명철;정현동;장양혁;박정우
    • 한국컴퓨터정보학회:학술대회논문집
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    • 한국컴퓨터정보학회 2018년도 제57차 동계학술대회논문집 26권1호
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    • pp.141-142
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    • 2018
  • 현재 시중에 판매되는 비행체들은 수동으로 조종을 하고 조종법이 미숙한 사람들은 다루기 힘들며 레저용으로 짧은 비행거리를 가지고 있고 간단한 영상촬영, 지형측정 등의 간단한 용도를 가졌다. 본 연구에서는 무인기의 FC(Flight Controller)의 인터페이스를 이용한 원리, 동작을 통하여 사용자의 조종 능력 향상을 기대할 수 있으며 Arduino 와 Pixhawk를 이용한 수직 이착륙기를 제작하여 활주로에 대한 제약을 없애고 멀티콥터와 비교하여 보다 좀 더 효율적인 비행을 할 수 있고자 한다.

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국내 건설 산업에서의 물량산출 특성을 고려한 공법기반 견적자동화 시스템 개발 (Development of Construction Method based Automated Estimation System Considering Characteristics of the Domestic Construction Industry)

  • 정준호;이창희;김성아;진상윤;최철호
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2010년도 정기 학술대회
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    • pp.93-96
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    • 2010
  • 현재 국내외에서 Building Information Modeling을 적용한 여러 분야의 연구가 활발하게 진행되고 있으며, 일부 국외에서는 3D 기반의 견적을 실제 프로젝트에 반영하고 있다. 반면, 국내 건설 프로젝트에서는 여전히 2D 설계도면과 물량산출 프로그램을 이용하여 견적이 이루어지고 있다. 작업의 신속성 및 정확성을 중요시하는 국내 견적 문화에서는 3D 기반의 물량산출 방식 도입을 부정적으로 바라보는 시각이 있으나, 향후 건설 산업의 경쟁력 확보를 위해서 3D 기반 견적작업이 필요하다. 이에 국외에서 상용화된 견적 시스템을 국내 건설 프로젝트에 적용한 결과, 몇 가지 한계점이 있는 것으로 드러나 국내 견적 방식에 적합한 3D기반의 물량산출 프로그램 개발이 절실한 상황이다. 따라서 본 연구에서는 국내 건설 산업에서의 물량 산출 특성을 반영한 공법기반 견적자동화 시스템 개발 및 검증을 통해 국내 3D 기반의 견적 도입을 앞당기고자 한다.

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EXAMINATIONS OF METHOD FOR CALCULATING LAE OF HELICOPTER NOISE

  • Matsui, Toshihito;Park, Young-Min;Takagi, Koichi
    • 한국음향학회:학술대회논문집
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    • 한국음향학회 1994년도 FIFTH WESTERN PACIFIC REGIONAL ACOUSTICS CONFERENCE SEOUL KOREA
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    • pp.668-673
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    • 1994
  • The paper presents a simple method for calculating the sound exposure level (LAE) of helicopter noise. It is assumed that a helicopter is a nondirective point source and that A-weighted sound pressure level at an observation point can be expressed by an A-weighted power level and a simple function of the distance from the helicopter. We derived a formula for LAE by integrating the sound energy along a finite or an infinite flight segment. The values calculated form the formula agree well with the results of test flights in which three types of helicopters each were operated in three moving modes of approach, takeoff and level flyover.

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평판 상에서 경사 분류열 부근의 유동에 대한 실험적 연구 (Experimental Study of Flow Near a Flat Plate Around a Row of Inclined Jets)

  • 김은영
    • 한국기계기술학회지
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    • 제13권2호
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    • pp.39-44
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    • 2011
  • An experimental method, based upon wall visualizations, has been developed to observe air flow near a plane wall around a row of five $45^{\circ}$ inclined jets discharging into a cross stream. This study concerns the variation of injection rate R which is one of the most important parameters governing this flow type. The Results are concentrated on the spatial evolution of two lobes with R. These structures are fastened to jets downstream edge and exist for very low injection rate values which are an indication of jets takeoff at the immediate downstream of injection orifices. The velocity rate of 0.42 marks a change in the structure alimentation system.

직선교량에 대한 디지털엔지니어링 모델의 선형연동 프로그램 개발 (Automated Digital Engineering Modeling of Prefabricated Bridges with Parameterized Straight Alignments)

  • 최재웅;강전용;김현민
    • 한국BIM학회 논문집
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    • 제10권4호
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    • pp.40-49
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    • 2020
  • This report describes the development of a program that can be linked to an alignment and extracts related information using a prefab structured digital engineering model. The subject bridge was set as a straight alignment, the Superstructure type as Precast girder and the Substructure type as Precast pier and Cast-in-situ Abutment. We identified the variables required to create a digital engineering model and reviewed them to create the digital engineering model by entering them as numerical values in the program. In addition, it is configured so that the variables linked to the alignment can be entered numerically. The quantity takeoff can be calculated when the design is complete. The purpose of the program development presented in this report is to enable the designers to select the optimal alternative by designing a bridge that best fits their current situation, extracting the relevant information and then by providing it to the manufacturer and construction company.

드론 정밀 측위 기술 동향 (A Trend Survey on Precision Positioning Technology for Drones)

  • 이정호;전주일;한경수;조영수;임채덕
    • 전자통신동향분석
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    • 제38권3호
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    • pp.11-19
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    • 2023
  • Drones, which were early operated by remote control, have evolved to enable autonomous flight by combining various sensors and software tools. In particular, autonomous flight of drones was possible since the application of GNSS-RTK (global navigation satellite system with real-time kinematic positioning), a precision satellite navigation technology. For instance, unmanned drone delivery based on GNSS-RTK data was demonstrated for pizza delivery in Korea for the first time in 2021. However, the vulnerabilities of GNSS-RTK should be overcome for delivery drones to be commercialized. In particular, jamming in the navigation system and low positioning accuracy in urban areas should be addressed. Solving these two problems can lead to stable flight, takeoff, and landing of drones in urban areas, and the corresponding solutions are expected to establish a hybrid positioning technology. We discuss current trends in hybrid positioning technology that can either replace or complement GNSS-RTK for stable drone autonomous flight.

기낭 부력 제어에 의한 비행선 이착륙의 인공신경망 적용 (Application of neural network for airship take-off and landing mode by buoyancy control)

  • 장용진;우귀애;김종권;이대우;조겸래
    • 한국항공우주학회지
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    • 제33권2호
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    • pp.84-91
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    • 2005
  • 오랜기간 비행선의 이착륙은 사람에 의한 수동으로 이루어졌으나, 자동제어시스템의 개발과 함께 이를 비행선에 적용하여 보다 정확한 이착륙의 필요성이 대두되었으며, 많은 알고리즘이 개발되고 있다. 본 논문에서는 기낭의 압력제어에 의한 비행선의 이착륙제어를 다룬다. 비행선의 운동방정식은 비선형 방정식으로 매우 복잡하여 우선 간단한 PID제어기에 의한 해법을 제시하였다. 그러나, 운항시 대기조건이 빠르게 변하므로 변하는 예측 불가능한 외란에 대해서는 만족스런 성능을 보이지 못하였다. 따라서, 본지에서는 인공 신경망을 이용한 학습알고리즘을 토대로 원하는 궤적에 빠르게 추종하도록 설계하였다. 일반적으로 인공신경망은 복잡한 문제에 있어서 많은 수의 은닉층과 뉴런이 필요하고 또한 훈련시간이 많이 걸리는 단점이 있기에 이를 해결하기 위해 비행선 이착륙 문제에 대한 일반적인 인공신경망 적용에 대해 연구하였다. 본지에서는 RBFN(radial basis function network)제어기를 설계하였고, 신경 회로망의 가중치는 외란이 인가되거나 부하특성이 비선형적으로 변화되는 것을 고려하도록 기준입력과 실제 비행선 모델의 출력사이의 오차를 최소화하는 방향으로 학습을 진행하였다. 그 결과 최대 15m의 오차를 보이는 PID제어기보다 양호한 결과를 얻었다.

핸드스프링 몸접어 앞공중돌기동작의 운동학적 분석 (The Kinematic Analysis of Handspring Salto Forward Piked)

  • 권오석
    • 한국운동역학회지
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    • 제17권1호
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    • pp.145-153
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    • 2007
  • The purpose of this study is to compare and analyze the phase-by-phase elapsed time, the COG, the body joint angle changes and the angular velocities of each phase of Handspring Salto Forward Piked performed by 4 college gymnasts through 3D movement analysis program. 1. The average elapsed time for each phase was .13sec for Phase 1, .18sec for Phase 2, .4sec for Phase 3, and .3sec for Phase 5. The elapsed time for Phase 1 to Phase 3 handspring was .35sec on average and the elapsed time for Phase 4 to Phase 5 handspring salto forward piked was .7sec on average. And so it showed that the whole elapsed time was 1.44sec. 2. The average horizontal changes of COG were 93.2 cm at E1, 138. 5 cm at E2, 215.7 cm at E3, 369.2 cm at E4, 450.7 cm at E5, and 553.1 cm at E6. The average vertical changes of COG were 83.1 cm at E1, 71.3 cm at E2, 78.9 cm at E3, 93.7 cm at E4, 150.8 cm at E5, and 97.2 cm at E6. 3. The average shoulder joint angles at each phase were 131.6 deg at E1, 153.5 deg at E2, 135.4 deg at E3, 113.4 deg at E4, 39.6 deg at E5, and 67.5 deg at E6. And the average hip joint angles at each phase were 82.2 deg at E1, 60 deg at E2, 101.9 deg at E3, 161.2 deg at E4, 97.7 deg at E5, and 167 deg at E6. 4. The average shoulder joint angular velocities at each phase were 130.9deg/s E1, 73.1 deg/s at E2, -133.9 deg/s at E3, -194.4 deg/s at E4, 29.4 deg/s at E5, and -50.1 deg/s at E6. And the average hip joint angular velocities at each phase were -154.7 deg/s E1, -96.5 deg/s at E2, 495.9 deg/s at E3, 281.5 deg/s at E4, 90.3 deg/s at E5, and 181.7 deg/s at E6. The results shows that, as for the performance of handspring salto forward piked, it is important to move in short time and horizontally from the hop step to the point to place the hands on the floor and jump, and to stretch the hip joints as much as possible after the displacement of the hands and to keep the hip joints stretched and high in the vertical position at the takeoff. And it is also important to bend the shoulder joints and the hip joints fast and spin as much as possible after the takeoff, and to decrease the speed of spinning by bending he shoulder joints and the hip joints quickly after the highest point of COG and make a stable landing.