• Composites Research
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• 제12권3호
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• pp.45-54
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• 1999

본 연구에서는 형상기억합금 선을 편심하게 삽입한 복합적층 보의 좌굴 및 좌굴후 제어에 관한 실험결과를 나타내었다. 임계좌굴하중을 향상하기 위하여 형상회복모멘트의 특성을 활용하였다. 좌굴제어의 범위를 향상시키기 위해 페루프 제어를 사용하여 좌굴후 제어의 거동을 검토하였다. 이러한 좌굴제어 실험을 통하여, 임계좌굴하중을 증가시키고 좌굴모드가 반대방향으로 변화하는 거동을 보의 세장비 및 기하학적 초기결함, 형상기억합금 선의 삽입 위치 등을 고려하여 하중-변위의 결과로부터 정량적, 정성적으로 분석하였다. 적당한 형상회복모멘토를 이용하여 원하는 변형형상을 유지함으로써 외부하중을 받는 보의 좌굴후 제어에서도 적용할 수 있다.

• 제어로봇시스템학회논문지
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• 제8권3호
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• pp.199-207
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• 2002

In this paper, a self-tuning gain-scheduled skyhook control for semi-active suspension systems is investigated. The dynamic characteristics of a continuously variable damper including electro-hydraulic pressure control valves is analyzed. A 2-d.o.f. time-varying quarter-car model that permits variations in sprung mass and suspension spring coefficient is considered. The self-tuning skyhook control algorithm proposed in this paper requires only the measurement of body acceleration. The absolute velocity of the sprung mass and the relative velocity of the suspension deflection are estimated by using integral filters. The skyhook gains are gain-scheduled in such a way that the body acceleration and the dynamic tire force are optimized. An ECU prototype is discussed. Experimental results using a 1/4-ear simulator are discussed. Also, a suspension ECU prototype targeting real implementation is provided.

• 한국항공우주학회지
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• 제47권1호
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• pp.1-8
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• 2019

비례제어밸브를 이용한 초음속 추력편향제어의 특성을 관찰하기 위한 실험적 연구가 진행되었다. 노즐 압력비에 따라 세 가지 서로 다른 추력편향 제어특성이 나타나고, 밸브작동에 따른 강한 이력현상이 관찰되었다. 아울러 이차챔버의 압력이 추력편향에 영향을 주는 주요 인자 중의 하나임이 확인되었다. 이에 이력현상을 회피하고 밸브제어에 따른 안정된 추력편향을 구현하기 위하여 이차챔버의 압력계수를 이용한 제어 알고리즘이 적용되었다. 그 결과 비례제어밸브를 통하여 최대 추력편향각 $20^{\circ}$ 범위에서 안정적인 추력편향제어가 구현 가능함이 확인되었다.

• Structural Engineering and Mechanics
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• 제16권5호
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• pp.519-531
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• 2003

Piezoelectric actuators have long been recognised for use in aerospace structures for control of structural shape. This paper looks at active control of the swept shock wave/turbulent boundary layer interaction using smart flap actuators. The actuators are manufactured by bonding piezoelectric material to an inert substrate to control the bleed/suction rate through a plenum chamber. The cavity provides communication of signals across the shock, allowing rapid thickening of the boundary layer approaching the shock, which splits into a series of weaker shocks forming a lambda shock foot, reducing wave drag. Active control allows optimum control of the interaction, as it would be capable of positioning the control region around the original shock position and unimorph tip deflection, hence mass transfer rates. The actuators are modelled using classical composite material mechanics theory, as well as a finite element-modelling program (ANSYS 5.7).

• International Journal of Control, Automation, and Systems
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• 제4권2호
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• pp.255-270
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• 2006

In this paper, a design method of nonlinear autopilot for ship-to-ship missiles is proposed. Ship-to-ship missiles have strongly coupled dynamics through roll, yaw, and pitch channel in comparison with general STT type missiles. Thus it becomes difficult to employ previous control design method directly since we should find three different solutions for each control fin deflection and should verify the stability for more complicated dynamics. In this study, we first propose a control loop structure for roll, yaw, and pitch autopilot which can determine the required angles of all three control fins. For yaw and pitch autopilot design, missile model is reduced to a minimum phase model by applying a singular perturbation like technique to the yaw and pitch dynamics. Based on this model, a multi-input multi-output (MIMO) nonlinear autopilot is designed. And the stability is analyzed considering roll influences on dynamic couplings of yaw and pitch channel as well as the aerodynamic couplings. Some additional issues on the autopilot implementation for these coupled missile dynamics are discussed. Lastly, 6-DOF (degree of freedom) numerical simulation results are presented to verify the proposed method.

• 한국항공우주학회지
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• 제34권7호
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• pp.35-44
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• 2006

항공기 비행 시, 조종면에 고장이 발생하였을 때 이를 검출하여 제어기를 수정하거나 다른 제어기로 전환하는 방식을 주로 사용한다. 본 논문은 작동기에 고장 발생시 임의의 고장검출 알고리듬을 사용하여 고장을 검출하여, 제어기를 수정/전환하는 방식을 사용하지 않고, 신경회로망과 PCH(Pseudo-Control Hedging) 기법을 이용하여, 발생된 고장정도에 따라 제어기 스스로 판단하여 대체 조종면으로 보상해 주는 재형상 비행제어법칙을 제시한다. 제어시스템은 DMI(Dynamic Model Inversion) 기법을 적용한 내부루프(SCAS : Stability Command Augmentation System)와 Coordinate Turn을 위한 Y축 가속도 피드백 외부루프로 구성한다. 특히 고장 보상을 위해 작동기 포화를 방지하는 PCH 기법을 이중으로 적용하였다. 끝으로 몇 가지 고장상황에 따른 시뮬레이션을 통해 그 가능성을 검증하였다.

• 한국소음진동공학회논문집
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• 제23권5호
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• pp.463-471
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• 2013

This paper presents design and control of electronic control suspension(ECS) equipped with controllable magnetorheological(MR) damper for passenger vehicle. In order to achieve this goal, a cylindrical type MR fluid damper that satisfies design specification of a middle-sized commercial passenger vehicle is proposed. After manufacturing the MR damper with design parameters, their field-dependent damping forces are experimentally evaluated and compared with those of a conventional damper. A quarter-vehicle MR ECS system consisting of sprung mass, spring, tire, controller and the MR damper is established in order to investigate the ride comfort performances. On the basis of the governing equation of motion of the suspension system, five control strategies(soft, hard, comfort, sport and optimal mode) are formulated. The proposed control strategies are then experimentally realized with the quarter-vehicle MR ECS system. Control performances such as vertical acceleration of the car body and tire deflection are evaluated in frequency domains on random road condition. In addition, performance comparison of WRMS(weighted root mean square) of the quarter-vehicle MR ECS system on random road are undertaken in order to investigate ride comfort characteristics.

• 한국BIM학회 논문집
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• 제6권3호
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• pp.42-48
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• 2016

Structural members are designed to maintain the load-carrying capacity as well as structural strength, and the structural serviceability such as the deflection, cracks, and vibration to give the occupants uncomfortable environment should be checked. Recently, the importance of the vibration has been issued since the Techno Mart accident due to vibration resonance. This study provides a passive vibration control system using the repulsion force of magnets to reduce dynamic vibrations. The systems is devised by importing the constraint condition by a hinge to operate magnets installed at two adjacent locations. The effectiveness of the proposed system is investigated by the vibration control test of a steel beam with and without the control system. It is illustrated in the test that the system is activated by the control forces executed by the magnets and can be utilized in reducing the dynamic responses. The system can be applied to pedestrian bridge and traffic bridge. The applicability is expected in the future by optimizing the factors to affect the dynamic responses like the intensity, mass, locations of magnets.

• 대한치과교정학회지
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• 제31권4호
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• pp.439-445
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• 2001

본 연구의 목적은 기능성 및 골격성 전치부 반대교합 환자에 대한 형태학적 차이점을 비교하는 것이다. 전치부의 기능성 반대교합을 보이는 28증례와 골격성 반대교합을 보이는 31증례를 각각 실험군과 대조군으로 삼았다. 실험군과 대조군의 평균연령은 $9.6{\pm}1.8$세와$9.9{\pm}1.9$세이었다. 측모두부방사선 사진을 촬영하였으며 두 군간의 형태학적 차이를 비교하기 위해 49개 항목에 대한 계측 및 통계학적인 분석을 시행하였다. 계측항목 중 cranial deflection, maxillary depth, ANB, convexity, NPo-AB, APDI, Mx 1-SN, Mx 1-NA angle, Mx 1-NA, Md 1-NB angle and Md 1-NB에서 통계학적인 유의차가 나타났다. 실험군에서는 Class III로의 성장 가능성, 상악골의 전방위치, 상하악골간의 전후방적 부조화 감소, 상악 중절치의 후퇴, 직립 및 하악 중절치의 전돌, 순측경사를 보였다.

• Advances in concrete construction
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• 제10권5호
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• pp.455-462
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• 2020

This study investigated the effect of horizontal casting joints on the mechanical properties and structural behavior of sustainable self-compacting reinforced concrete beams (SCRCB). The experimental research consisted of two stages. The first stage used four types of concrete mixtures which were produced to indicate the effects of cement replaced with cement waste at 0%, 5%, 10%, and 15% by weight of cement content on fresh concrete properties of self-compacting concrete (SCC) such as, passing ability, filling ability, and segregation resistance. In addition, mechanical properties such as compressive, tensile, and flexural strength were also studied. The second stage selected the best mixture from the first stage and studied the effect of horizontal casting joints on the structural behavior of sustainable SCRCBs. The effect of horizontal casting joints on the mechanical properties and structural behavior were at the 25%, 50%, 75%, and 100% of sample height. Load deflection, failure mode, and theoretical analysis were studied. Results indicated that the incorporation of replacement with cement waste by 5% to 10% led to economic and environmental advantages, and the results were acceptable for fresh and mechanical properties. The results indicated that delaying the time for casting the second layer and increasing the cement waste in concrete mixtures had a great effect on the mechanical properties of SCC. The ultimate load capacity of horizontal casting joints reinforced concrete beams slightly decreased compared with the control beam. The maximum deflection of casting joint beams with 75% of samples height is similar with the control beam. The experimental results of reinforced concrete beams were substantially acceptable with the theoretical results. The failure modes obtained the best forced casting joint on the structural behavior at 50% height of casting in the beam.