• 제목/요약/키워드: Pilot Design

검색결과 963건 처리시간 0.024초

Building Information Model(BIM) 기반의 건축 구조설계 Pilot Study (The Pilot Study of the structural design based on the Building Information Model(BIM))

  • 신태송;조영상;천진호;엄진업;양종민
    • 한국전산구조공학회:학술대회논문집
    • /
    • 한국전산구조공학회 2008년도 정기 학술대회
    • /
    • pp.265-268
    • /
    • 2008
  • With application of IT convergence technique in AEC industry, it is currently conducted the research on the virtual construction system. This paper aims at the pilot study on the structural design based on BIM used in collaboration environment. The work scope of structural design includes the structural analysis model, structural detail model and analytic model and we focuse the research on the interoperability among them. It is partly utilized the transfer module supplied by software developer and partly developed here the interface module through API. This paper shows the interoperability process to pilot test and indicates the problems occurred in interface.

  • PDF

다중 기지국 환경에서의 MIMO-OFDM 시스템을 위한 최적 파일럿 시퀀스 설계 방법 (Optimal Pilot Sequence Design based on Chu sequences for Multi-cell Environments)

  • 강재원;이두호;변일무;김광순
    • 한국통신학회논문지
    • /
    • 제34권11C호
    • /
    • pp.1113-1121
    • /
    • 2009
  • 본 논문에서는 기지국간 간섭이 큰 다중기지국 환경에서 multiple-input multiple output (MIMO) orthogonal frequency division multiplexing (OFDM) 시스템을 위한 파일럿 시퀀스 설계 방법 및 채널 추정 기법을 제안한다. 제안 파일럿 시퀀스의 경우 평균 제곱 오류치 (Mean Square Error)를 최소화시키며, 설계된 파일럿에 적합한 채널 추정 방법을 제안한다. 제안된 파일럿 시퀀스 및 채널 추정 기법은 추 시퀀스의 상관관계 특성을 이용해 설계되며 모의실험을 통해 설계된 파일럿 시퀀스를 이용한 채널 추정 기법이 기지국간 간섭을 완화에 효과적임을 보여준다.

비행장갑설계를 위한 사용실태분석 및 개선안 개발 (Usage Analysis and Design Development for Pilot Gloves)

  • 박지은;전은진;정정림;박세권;유희천;김희은
    • 한국의류산업학회지
    • /
    • 제11권5호
    • /
    • pp.764-770
    • /
    • 2009
  • This study was conducted to analyze the wearing condition on gloves for pilots and to suggest the developments for pilot gloves design. This survey was performed with 99 pilots and the questionnaires included items about discomfort, materials and problems when wearing pilot gloves. The respondents felt uncomfortable on the finger tip, the hollow area of the hand and the end of thumb when they move their hands with the gloves. They replied that the finger length, palm length, and circumference of the fingers did not match well. Also they complained there was severe abrasion in the tip of the thumb, finger tips and the middle of the palm of the gloves. The result of these analyses supports the following suggestions. It is necessary to improve durability by applying the additional materials to the severely worn parts. Punching on the glove materials could improve sweat rate and ventilation, and careful washing should be accompanied to prevent the occurrence of linters and transformation after laundering. And it is needed to prepare an accurate and more diversified size system and to design the gloves fitted to the individual hands. With these in mind, it is required to propose solutions for pilot gloves with reference to the survey results in order to design appropriate pilot gloves in terms of movement, size and material. It was concluded that an analysis of the wearing condition and developments are useful for ergonomics pilot gloves design.

도심지에서 효율적인 무도갱 2-Arch 터널의 설계사례 (A case study on efficient non pilot 2-Arch Tunnel in the urban)

  • 윤일병;강희준;김홍대;김동식
    • 한국지반공학회:학술대회논문집
    • /
    • 한국지반공학회 2010년도 춘계 학술발표회
    • /
    • pp.543-552
    • /
    • 2010
  • Due to increase in urban tunnelling as urban population and traffic volume increase, problems related with site security and civil appeal also increase. This paper presents a comparative analysis between conventional 2-arch tunnel method and non-pilot 2 arch tunnel method, which were performed in the basic design of Wie-Rae region. According to the analysis results, non-pilot 2-arch tunnel method is more efficient in terms of stability, constructability, and economic aspect. It is authors' wish that design procedure and method presented in this paper could help the design and construction of non-pilot 2-arch tunnel that should be planned in the near future.

  • PDF

지하 복합플랜트 운영 중 확장을 고려한 격자형 지하공간 파일럿 테스트 (Pilot Test of Grid-Type Underground Space Considering Underground Complex Plant Operation)

  • 이철호
    • 터널과지하공간
    • /
    • 제33권6호
    • /
    • pp.472-482
    • /
    • 2023
  • 격자형 또는 주방식 공법은 수평으로 매장된 광물을 채굴할 목적으로 적용되는 공법이다. 본 연구에서는 자연 암반을 암주로 사용하는 주방식 공법을 지하공간 건설에 적용하기 위해 설계와 파일럿 테스트를 수행하였다. 파일럿 테스트가 수행된 지역은 기존 골재 광산을 운영하는 곳으로 양호한 암반 조건과 적당한 심도를 보유하고 있었다. 파일럿 테스트 부지는 연구 결과 적용이 가능한 광산을 기반으로 접근성, 지반조건 등을 검토하여 후보지를 결정하였으며 상세 지반조사와 설계를 통해 부지 조성공사를 수행하였다. 파일럿 테스트는 암주형상을 8×8 m로 공간의 단면을 8×12 m 크기로 설계되었다. 시험발파를 통해 발파패턴을 결정하고 89공 3 m 굴진 단면 발파를 수행하여 총 92 m 굴진을 완료하였다. 현장 측정을 통해 평균 폭 12.5 m, 평균 높이 8.3 m을 확인하여 연구에서 고려하는 단면 모양과 유사하게 굴착공사를 진행할 수 있었다.

Discovered Pilot Designs in MIMO OFDM System with optimization algorithms

  • JunYoung Son
    • International Journal of Internet, Broadcasting and Communication
    • /
    • 제15권4호
    • /
    • pp.44-50
    • /
    • 2023
  • For Wi-Fi and IoT wireless systems, high-capacity wireless communication technology is being applied using MIMO OFDM. Because of virtu0al subcarriers in the practical MIMO OFDM system, the pilot subcarriers cannot be spaced equally. Thus, it is difficult to obtain a good mean square error (MSE) performance of the channel estimate. This paper proposes applicable methods and the newly discovered locations of pilot subcarriers in four transmitted antennas resulting in a good MSE performance with proposed optimization algorithms.

항공기 비정상 자세, 고도 및 속도 회복을 위한 자동회복장치 설계 및 검증에 관한 연구 (A Study on Design and Validation of Pilot Activated Recovery System to Recover Aircraft Abnormal Attitude, Altitude and Speed)

  • 김종섭;강임주
    • 제어로봇시스템학회논문지
    • /
    • 제14권12호
    • /
    • pp.1302-1312
    • /
    • 2008
  • Relaxed Static Stability(RSS) has been applied to improve flight performance of modern version supersonic jet fighters. Flight control systems are necessary to stabilize an unstable aircraft and to provide adequate handling qualities. Also, flight control systems of modern aircraft employ many safety measure to cope with emergency situations such as a pilot unknown attitude flight conditions of an aircraft in night flight-testing. This situation is dangerous because the aircraft can lose if the pilot not take recognizance of situation. The system called the "Pilot Activated Recovery System" or PARS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of unusual attitudes, speed and altitude. This paper addresses the concept of PARS with AARS(Automatic Attitude Recovery System), ATCS(Automatic Thrust Control System) and MARES(Minimum Altitude Recovery Estimation System), and this control law is designed by nonlinear control law design process based on model of supersonic jet trainer. And, this control law is verified by real-time pilot evaluation using an HQS(Handling Quality Simulator). The result of evaluation reveals that the these systems support recovery of an aircraft unusual attitude and speed, and improve a safety of an aircraft.

항공기 자세회복을 위한 자동회복장치 설계 및 검증에 관한 연구 (A Study on the Design and Validation of Pilot Activated Recovery System to Recovery of an Aircraft Unusual Attitude)

  • 김종섭;조인제;강임주;허기봉;이은용
    • 제어로봇시스템학회논문지
    • /
    • 제14권3호
    • /
    • pp.307-317
    • /
    • 2008
  • Relaxed static stability(RSS) concept has been applied to improve aerodynamic performance of modem version supersonic jet fighter aircraft. Therefore, flight control system are necessary to stabilize an unstable aircraft and provides adequate handling qualities. Also, flight control systems of modem version aircraft employ a safety system to support emergency situations such as a pilot unknown attitude flight conditions of an aircraft in night flight-testing. This situation is dangerous because the aircraft can lose if the pilot not take recognizance of situation. Therefore, automatic recovery system is necessary. The system called the "Pilot Activated Recovery System" or PARS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of unusual attitudes. This paper addresses the concept of PARS and designed using nonlinear control law design process based on model of supersonic jet trainer. And, this control law is verified by nonlinear analysis and real-time pilot evaluation using in-house software. The result of evaluation reveals that the PARS support recovery of an aircraft unusual attitude and improve a safety of an aircraft.

비행체 고도 및 속도계측용 Pilot-Tube 연구 (Development of the Pilot-Tube to Measure Flight Altitude and Velocity)

  • 최진철;이기권;박찬우
    • 한국추진공학회지
    • /
    • 제5권3호
    • /
    • pp.19-24
    • /
    • 2001
  • 대기중에서 움직이는 비행체(항공기, 미사일 등)의 속도 및 고도를 측정하기 위한 장치가 피토관 (Pilot-Tube)이다. 고속으로 비행하는 항공기의 안전하고 효율적인 운항을 위해서는 정확한 비행속도 및 고도측정이 요구된다. 피토관 최적 설계인자 결정을 위해 피토관 Nose의 Inlet부, Nose부 외곽형 상, 정압홀의 형상 및 정압홀 설치 위치 선정을 위한 유동장 해석을 수행하였다. 또한 해석을 통해 얻은 설계자료를 기본으로 제작한 피토관의 풍동실험을 수행하였다. 본 연구를 통해 속도 및 고도 계측용 피토관의 설계기술을 확보하였고 제작기술을 보유하였으며, 유동해석 및 풍동실험을 함으로써 피토관 국산화에 필요한 기본 자료를 얻었다.

  • PDF

Approximating the Outage Probability of the Pilot Channel for IS-95-Based Cellular CDMA Systems in the Soft Handover Region

  • Park, Seung-Keun;Cho, Pyung-Dong;Park, Ki-Shik;Cho, Kyung-Rok
    • ETRI Journal
    • /
    • 제25권6호
    • /
    • pp.523-526
    • /
    • 2003
  • This letter presents an approximation of the outage probability of the pilot channel that can be used for CDMA cell planning. The approximation can determine system parameters for soft handover in IS-95-based cellular CDMA downlink design. Computer simulations show that our analytical results agree with empirical results.

  • PDF