• Title/Summary/Keyword: 승강타

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An Experimental Study on Effect of Angle of Attack on Elevator Control Force for Underwater Vehicle with Separate Fixed Fins (별도의 고정타를 갖는 수중운동체 승강타의 제어력에 미치는 받음각의 영향에 대한 실험적 연구)

  • Park, CJeong-Hoon;Shin, Myung-Sub;Choi, Jae-Yeop;Hwang, Jong-Hyun;Shin, Young-Hun;Kim, Yeon-Gyu
    • Journal of Ocean Engineering and Technology
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    • v.30 no.4
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    • pp.243-252
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    • 2016
  • Conventionally, the static angle of attack and static elevator tests are carried out separately to estimate hydrodynamic stability derivatives of underwater vehicles. However, it is difficult to verify the interaction between the angle of attack and elevator angle in such cases. In this study, we perform a static elevator with angle of attack test where both the angle of attack and elevator angle are varied simultaneously. The experimental results show that the angle of attack has an influence on the elevator control force and that this tendency is dependent on the sense in which the angle of attack and elevator angle are varied. We predict level flight performance using hydrodynamic derivatives estimated through this experiment. The predictions considering the effect of angle of attack show good agreement with trials conducted in the open sea.

A Study on Design Process and Control Test of Manta-type Unmanned Underwater Test Vehicle (Manta 형상 무인잠수정의 설계과정 및 제어실험에 관한 연구)

  • Byun, Seung-Woo;Yim, Jong-Guk;Kim, Joon-Young
    • Proceedings of the KAIS Fall Conference
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    • 2009.12a
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    • pp.152-155
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    • 2009
  • 본 논문에서는 Manta 형상 무인잠수정의 자유항주모델을 설계하였고 이를 이용하여 제어실험을 실시하였다. 제작된 MUUTV모형은 직진방향으로 1개의 추진기를 가지고 있으며, 승강타와 방향타를 이용하여 수심 및 방향 제어를 실시하게된다. MUUTV는 수심제어시 사용되는 수심을 측정하기 위한 압력센서, 방향제어를 위해 방향각 측정을 위한 마그네틱 컴파스가 설치되어있으며, 잠수정의 전체적인 운용을 위한 Windows XP기반의 소형 On-board PC104가 장착되어있다. 시뮬레이션에 사용된 6자유도 운동모델은 PMM실험과 이론적 추정을 통해 얻어진 유체동역학계수와 파라미터를 이용하여 구성된다. 잠수정의 운동성능과 제어응답을 비교하기 위해 PID, 슬라이딩모드, 퍼지, 제어기가 설계되었으며, 이를 통해 제어 성능을 비교하고자 하였다. 또한 제작된 모델을 이용하여 수심 및 방향제어 실험을 수조에서 실시하였다.

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Simulation Analysis on Air Stream Around the Tail Wing of Airplane (비행기 꼬리날개 주위의 기류에 관한 시뮬레이션 해석)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.20 no.1
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    • pp.23-27
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    • 2011
  • This study analyzes about the variation of pressure and stream velocity according to the movement of tail wing. The pressure at the front part of airplane becomes lower than at the rear part and the stream velocity has decreased by being bumped against the wing of airplane. The pressure at the front part of rudder becomes higher than at its rear part according to the movement of rudder among the tail wings of airplane. The more stream velocity becomes decreased, the more rudder spreads out. As the tail wing of airplane folds, the pressure at its front part becomes higher. And the pressure at its rear part becomes lower than at its front part. The more tail wing of airplane folds, the more stream velocity becomes decreased.

A Study on Flight Characteristics and Flight Control Methodology for a Wing In Ground Effect Vehicle (지면효과익기의 비행특성 해석 및 비행제어 방식에 관한 연구)

  • Song, Yongkyu
    • Journal of Advanced Navigation Technology
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    • v.5 no.1
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    • pp.19-25
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    • 2001
  • In this study an analysis on flight characteristics and flight control methods for a wing in ground effect vehicle is made. In order to closely view its nonlinearity a few limit cycles are examined and related to the characteristics of the linearized systems. Several flight control methods are compared for the cruise mode with initial height error and command tracking mode of ascending, cruise, and descending. In comparison performance and the implementation aspects are examined. For the possible control inputs, combinations of elevator, thrust, and flap are considered and LQR-based output command tracking scheme is applied in the control system design.

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A Study on the Elevator Spar Improvement for the Operating Aircraft (장기 운영항공기 승강타 날개보 구조개선 연구)

  • Shim, Daisung;Kim, Mantae;Yeom, Hyowon;Im, Dongmin;Kim, Youngjin;Uhm, Wonseop
    • Journal of the Korea Institute of Military Science and Technology
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    • v.19 no.6
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    • pp.675-680
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    • 2016
  • This is a study for the improvement of the defected elevator spar in operating aircraft. The elevator spar web holes were analyzed to find out the cause of the cracks. The fatigue striations were observed and the cracks occurred by the repetitive stresses during the elevator works. Also the outboard connection structure of the elevator and horizontal stabilizer was more weak shape than the inboard. The design changes were recommended and the analyses were performed to verify the improvement of the changed shapes.

Study of Longitudinal Stability and Elevator Control of a Human Powered Aircraft, TORUK MAKTO I (인간동력 항공기 TORUK MAKTO I 세로 안정성 및 승강타 제어연구)

  • Park, Joohee;Kim, Younsoo;Han, Cheolheui
    • Journal of Aerospace System Engineering
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    • v.9 no.3
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    • pp.12-16
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    • 2015
  • 인간동력 항공기 TORUK MAKTO I에 대하여 양력선이론 및 XFOIL을 사용하여 도출한 공력계수 및 미계수 값과 CATIA를 사용한 관성모멘트 추정 값을 사용하여 지면효과 및 주익과 무게중심 사이의 수직거리 변화가 인간동력 항공기의 세로 정안정성에 미치는 영향과 수평미익(스테빌레이터) 변위각제어에 따른 세로 동안정성 해석 연구를 수행하였다. 연구결과 지면효과가 정적여유에 미치는 영향은 미미했다. 공력중심과 무게중심 사이의 수직거리가 세로 정안정성에 미치는 영향은 매우 컸으며, 수직거리 증가는 세로 정안정성을 증가시켰다. 수평미익 변위각 제어에 따른 세로 동안정성 해석 결과 장주기 진동특성과 감쇄특성이 매우 나쁜 것으로 나타났다. 향후 항공기의 동특성을 고려한 세로 동안정성 해석 및 측풍에 의한 가로 및 방향 안정성 해석연구를 수행할 예정이다.

An Analysis of Harmonics on Inverter Elevator System (인버터 승강기 시스템의 고조파 실태 분석)

  • 김정태;이기홍;홍규장
    • The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.8 no.5
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    • pp.41-48
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    • 1994
  • 국내에서 제작된 인버터 승강시 시스템의 고조파 발생량을 분석하고 타 전기설비에 미치는 영향을 알아보기 위하여 고층 아파트와 빌딩에 설치된 인버터 승강기를 대상으로 고조파 전압·전류를 측정하였다. 그 결과 인버터 승강기 시스템의 총고조파 전압 왜형율은 작게 나타났으나, 총고조파 전류 왜형율은 상당히 큰 것으로 밝혀졌다. 공동주택의 전기설비에 미치는 영향으로는, 역률 개선용 콘덴서에는 큰 문제가 되지 않으나 비상 발전기를 고려하여 인버터 승강기 시스템의 고조파 발생량을 줄일 필요가 있는 것으로 나타났다. 또한, 비상발전기의 허용 %등가역상전류와 본 연구의 실측값을 고려하여 인버터 승강기 시스템의 고조파 전류 규제값을 총고조파 전류 왜형율 40% 이하가 되도록 권장값을 제안하였다.

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Study on the Aeroservoelastic Stability Analysis with ZAERO (ZAERO를 활용한 서보공력탄성학적 안정성 해석기법 연구)

  • Rho, Hong-Gi;Bae, Jae-Sung;Hwang, Jai-Hyuk
    • Journal of Aerospace System Engineering
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    • v.14 no.5
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    • pp.1-8
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    • 2020
  • The aeroservoelastic analysis that deals with the interactions of the inertial, elastic, and aerodynamic forces and the influence of the control system have been performed. MSC Nastran was used for the free vibration analysis of the structure model as the pre-analysis. ZAERO was used to calculate the unsteady aerodynamic forces. The unsteady aerodynamic forces were verified by comparing with Doublet Hybrid Method. Karpel's Minimum-State Approximation method was used for approximation of the aerodynamic forces to the Laplace domain in the frequency domain. The aeroservoelastic state-space equation was obtained by combining the aeroelastic equation with the actuator dynamics. The analysis of aeroservoelastic stability concerning the elevator input of the high aspect ratio model was performed. The root-locus method and time-integration method were used for the analysis of aeroservoelastic in frequency and time domain.

A Legal Study on liability for damages cause of the air carrier : With an emphasis upon liability of passenger (항공운송인의 손해배상책임 원인에 관한 법적 고찰 - 여객 손해배상책임을 중심으로 -)

  • So, Jae-Seon;Lee, Chang-Kyu
    • The Korean Journal of Air & Space Law and Policy
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    • v.28 no.2
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    • pp.3-35
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    • 2013
  • Air transport today is a means of transport that is optimized for exchanges between nations. Around the world, has experienced an increase in operating and the number of airline route expansion that has entered into the international aviation agreements in order to take advantage of the air transport efficient, but the possibility of the occurrence of air transport accidents increased. When compared to the accident of other means of transport, development of air transport accidents, not high, but it leads to catastrophe aviation accident occurs. Air Transport accident many international transportation accident than domestic transportation accident, in the event of an accident, the analysis of the legal responsibility of the shipper or the like is necessary or passenger air carrier. Judgment of the legal order of discipline of air transport accident is a classification of the type of air transport agreement. Depending on the object, air transport agreements are classified into the contract of carriage of aviation of the air passenger transportation contract. For casualties occurs, air passenger transportation accident is a need more discussion of legal discipline for this particular. Korean Commercial Code, it is possible to reflect in accordance with the actual situation of South Korea the contents of the treaty, which is utilized worldwide in international air transport, even on the system, to control land, sea, air transport and welcoming to international standards. However, Korean Commercial Code, the problem of the Montreal Convention has occurred as it is primarily reflecting the Montreal Convention. As a cause of liability for damages, under the Commercial Code of Korea and the contents of the treaty precedent is reflected, the concept of accident is necessary definition of the exact concept for damages of passengers in particular. Cause of personal injury or death of passengers, in the event of an accident to the "working for the elevation" or "aircraft" on, the Montreal Convention is the mother method of Korea Commercial Code, liability for damages of air carrier defines. The Montreal Convention such, continue to be a matter of debate so far in connection with the scope of "working for the lifting of" the concepts defined in the same way from Warsaw Convention "accident". In addition, it is discussed and put to see if you can be included mental damage passenger suffered in air transport in the "personal injury" in the damage of the passenger is in the range of damages. If the operation of aircraft, injury accident, in certain circumstances, compensation for mental damage is possible, in the same way as serious injury, mental damage caused by aviation accidents not be able to live a normal life for the victim it is damage to make. So it is necessary to interpret and what is included in the injury to the body in Korea Commercial Code and related conventions, non-economic damage of passengers, clearly demonstrated from the point of view of prevention of abuse of litigation and reasonable protection of air carrier it must compensate only psychological damage that can be. Since the compensation of delay damages, Warsaw Convention, the Montreal Convention, Korea Commercial Code, there are provisions of the liability of the air carrier due to the delayed arrival of passenger and baggage, but you do not have a reference to delayed arrival, the concept of delay arrangement is necessary. The strict interpretation of the concept of delayed arrival, because it may interfere with safe operation of the air carrier, within the time agreed to the airport of arrival that is described in the aviation contract of carriage of passenger baggage, or, these agreements I think the absence is to be defined as when it is possible to consider this situation, requests the carrier in good faith is not Indian or arrive within a reasonable time is correct. The loss of passenger, according to the international passenger Conditions of Carriage of Korean Air, in addition to the cases prescribed by law and other treaties, loss of airline contracts, resulting in passengers from a service that Korean Air and air transport in question do damage was is, that the fact that Korean Air does not bear the responsibility as a general rule, that was caused by the negligence or intentional negligence of Korean Air is proof, negligence of passengers of the damage has not been interposed bear responsibility only when it is found. It is a clause in the case of damage that is not mandated by law or treaty, and responsible only if the negligence of the airline side has been demonstrated, but of the term negligence "for" intentional or negligent "Korean Air's Terms" I considered judgment of compatibility is required, and that gross negligence is appropriate. The "Korean Air international passenger Conditions of Carriage", airlines about the damage such as electronic equipment that is included in the checked baggage of passengers does not bear the responsibility, but the loss of baggage, international to arrive or depart the U.S. it is not the case of transportation. Therefore, it is intended to discriminate unfairly passengers of international flights arriving or departure to another country passengers of international flights arriving or departure, the United States, airlines will bear the responsibility for the goods in the same way as the contents of the treaty it should be revised in the direction.

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