• Title/Summary/Keyword: Pilot design

Search Result 967, Processing Time 0.018 seconds

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

  • Shin, Tae-Song;Cho, Young-Sang;Cheon, Jin-Ho;Eom, Jin-Up;Yang, Jong-Min
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2008.04a
    • /
    • 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

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

  • Kang, Jae-Won;Rhee, Du-Ho;Byun, Il-Mu;Kim, Kwang-Soon
    • The Journal of Korean Institute of Communications and Information Sciences
    • /
    • v.34 no.11C
    • /
    • pp.1113-1121
    • /
    • 2009
  • In this paper, the channel estimation and pilot sequence design technique of multiple-input multiple-output (MIMO) orthogonal frequency division multiplexing (OFDM) systems in multi-cell environments are studied for situations in which the inter cell interference (ICI) is the dominant channel impairment. We design pilot sequence aiming at minimizing mean square error and propose the channel estimation technique correspond to the designed pilot sequences. The proposed pilot sequences employ the sequences with good correlation properties such as Chu sequence and through simulations, it is shown that channel estimation algorithm using designed pilot sequence is effective for mitigating the ICI.

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

  • Park, Ji-Eun;Jeon, Eun-Jin;Jeong, Jeong-Rim;Park, Sei-Kwon;You, Hee-Cheon;Kim, Hee-Eun
    • Fashion & Textile Research Journal
    • /
    • v.11 no.5
    • /
    • 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.

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

  • Yoon, Il-Byung;Kang, Hee-June;Kim, Hong-Dae;Kim, Dong-Sik
    • Proceedings of the Korean Geotechical Society Conference
    • /
    • 2010.03a
    • /
    • 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

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

  • Chulho Lee
    • Tunnel and Underground Space
    • /
    • v.33 no.6
    • /
    • pp.472-482
    • /
    • 2023
  • The grid-type or room-and-pillar method is applied for the purpose of mining horizontally buried minerals. In this study, design and pilot test were performed to apply the room-and-pillar method which uses natural rock as a rock pillar to the construction of underground space. The area where the pilot test was conducted was in stone mine and had good rock conditions with an appropriate depth (about 30 m) to apply the pilot test. The pilot test site was selected by reviewing accessibility and ground conditions and then site construction was performed through detailed ground investigation and design. The pilot test was designed with a column shape of 8×8 m and a cross-section of 8×12 m. The blasting pattern was determined through test blasting at the site, and blasting of 3 m excavation with 89 holes was performed. Through field observations, the average width of 12.5 m and the average height of 8.3 m were measured. Therefore, it is possible to proceed similar to the cross-sectional shape considered in the design.

Discovered Pilot Designs in MIMO OFDM System with optimization algorithms

  • JunYoung Son
    • International Journal of Internet, Broadcasting and Communication
    • /
    • v.15 no.4
    • /
    • 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.

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

  • Kim, Chong-Sup;Kang, Im-Ju
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.14 no.12
    • /
    • 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.

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

  • Kim, Chong-Sup;Cho, In-Je;Kang, Im-Ju;Hur, Gi-Bong;Lee, Eun-Yong
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.14 no.3
    • /
    • 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.

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

  • 최진철;이기권;박찬우
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.5 no.3
    • /
    • pp.19-24
    • /
    • 2001
  • The Pilot-Tube is the device that measures velocity and altitude of high speed vehicle. Accurate measurements of speed and altitude are essential to the safe and efficient operation of aircraft. For the purpose of determining optimal design parameters of Pilot-Tube such as nose inlet configuration, nose shape, static hole configuration, and static hole location, subsonic flow field was calculated numerically and analyzed. A Pilot-Tube was manufactured based on numerical flow field analysis, and pressure and air velocity was measured experimentally in the wind tunnel. As a result manufacturing and design technologies of the Pilot-Tube were acquired to make flight-device.

  • 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
    • /
    • v.25 no.6
    • /
    • 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