• Steel and Composite Structures
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• 제3권6호
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• pp.403-420
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• 2003

In the paper one investigates the benefits deriving from the introduction of SMA provisions in a structure subject to dynamic excitation and vertical loads. At this purpose one considers a multi-degree-of-freedom (mdof) shear elastic-plastic frame and designs couples of super-elastic SMA tendons to be placed at critical locations of the structure. Particular attention is focused on the reduction of $P-{\Delta}$ effects.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 추계 학술대회논문집
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• pp.136-141
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• 2006

A prediction of store separation trajectory using grid survey method has been conducted. For the grid survey method, store's aerodynamic flowfield data such as freestream and grid data is needed to solve 6 degree of freedom(6-DOF) equations of motion. In the presented study, aerodynamic flowfield data was generated by Euler solver instead of CTS wind tunnel test. The predicted trajectories shows good agreement with CTS test results.

• Journal of Advanced Marine Engineering and Technology
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• 제35권5호
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• pp.632-639
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• 2011

해양 파력 발전 시스템의 설계를 위하여 본 연구에서는 6-자유도운동해석 기법을 적용한 3차원 CFD 해석으로 두 개의 부유체에 대한 거동을 유입되는 파의 성질에 따라 해석하였다. 수조모델내에서의 파의 생성형상을 현재 실험에서 가장 많이 사용되는 피스톤 형식의 조파기와 동일한 형태의 파를 생성하였으나 얕은 수심으로 인하여 바닥면에서 생성되는 에크만 경계층에 의해 파의 에너지가 감쇄되는 현상을 보였다. 생성된 파를 이용하여 파장에 따른 부유체의 거동을 계산한 결과 파장이 5m인 경우 부유체의 최대 진폭은 0.3m, 파장 1m인 경우 최소 진폭은 0.15m 그리고 파장 6m인 경우 부유체간 최대 거리는 1.06m로 계산되었다.

• International Journal of Aeronautical and Space Sciences
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• 제11권2호
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• pp.69-79
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• 2010

This paper describes the experimental framework for the control system design and validation of a rotorcraft unmanned aerial vehicle (UAV). Our approach follows the general procedure of nonlinear modeling, linear controller design, nonlinear simulation and flight test but uses an indoor-installed multi-camera system, which can provide full 6-degree of freedom (DOF) navigation information with high accuracy, to overcome the limitation of an outdoor flight experiment. In addition, a 3-DOF flying mill is used for the performance validation of the attitude control, which considers the characteristics of the multi-rotor type rotorcraft UAV. Our framework is applied to the design and mathematical modeling of the control system for a quad-rotor UAV, which was selected as the test-bed vehicle, and the controller design using the classical proportional-integral-derivative control method is explained. The experimental results showed that the proposed approach can be viewed as a successful tool in developing the controller of new rotorcraft UAVs with reduced cost and time.

• 한국정밀공학회지
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• 제29권8호
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• pp.906-912
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• 2012

This paper presents the new method for a six-degree-of-freedom (DOF) motion measurement and those dynamic characterizations in an ultraprecision linear stage using angle sensor-implemented grating interferometry. It consists of a diffractive optical element, a corner cube, four separate two-dimensional position sensitive detectors, four photodiodes and auxiliary optics components. From the previous study, it was confirmed that the proposed optical system could measure a six-DOF motion error in a linear stage. In this article, six-DOF motion dynamic characteristics of the stage were investigated through the step response and with respect to the conditions with a different speed of a slide table. As a result, the natural frequency and damping ratio according to a six-DOF direction was obtained. Also, it was seen that the speed of slide table had an significant effect on a six-DOF displacement motion, especially, X, which was considered as the effect of friction mechanism and local elastic mechanical deformation in a slide guide.

• 대한기계학회논문집
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• 제10권5호
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• pp.689-697
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• 1986

본 연구에서는 3자유도(3방향의 병진운동만 고려) 고무마운트모형의 타당성을 검증하기 위하여, 먼저 고무자체의 물성치인 강성계수와 감쇠계수를 진동수와 초기변 형률에 따라 실험을 통해 구하였다. 질량행렬의 모든요소를 쉽게 구할 수 있는 간단 한 시험구조물을 제작하고 여기에 고무아운트를 부착하여 6자유도를 갖는 모의 엔진- 마운트계를 구성한 후 가진실험을 통해 얻은 오무드 매개변수들과 고무의 물성치를 이 용한 컴퓨터 시뮬레이션의 결과를 비교함으로써 고무아운트 모형의 타당성을 검증하였 다. 특히 본 연구에는 유압가진 실험으로부터 얻은 실험결과를 바탕으로 고무의 강 성계수를 주파수의 1차함수로 고려한 경우와 전진동수 영역에서 균일하다고 가정하는 경우를 비교하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2005년도 ICCAS
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• pp.2120-2125
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• 2005

The principal idea of vibration isolation is to filter out the response of the system over the corner frequency. The isolation objectives are to transmit the attitude control torque within the bandwidth of the attitude control system and to filter all the high frequency components coming from vibration equipment above the bandwidth. However, when a reaction wheels or control momentum gyros control spacecraft attitude, vibration inevitably occurs and degrades the performance of sensitive devices. Therefore, vibration should be controlled or isolated for missions such as Earth observing, broadcasting and telecommunication between antenna and ground stations. For space applications, technicians designing controller have to consider a periodic vibration and disturbance to ensure system performance and robustness completing various missions. In general, past research isolating vibration commonly used 6 degree order freedom isolators such as Stewart and Mallock platforms. In this study, the vibration isolation device has 3 degree order freedom, one translational and two rotational motions. The origin of the coordinate is located at the center-of-gravity of the upper plane. In this paper, adaptive notch filter finds the disturbance frequency and the reference signal in filtered-x least mean square is generated by the notch frequency. The design parameters of the notch filter are updated continuously using recursive least square algorithm. Therefore, the adaptive filtered-x least mean square algorithm is applied to the vibration suppressing experiment without reference sensor. This paper shows the experimental results of an active vibration control using an adaptive filtered-x least mean squares algorithm.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제13권6호
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• pp.2859-2872
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• 2019

Interference alignment (IA) has been a powerful approach to achieve the maximum degree of freedom (DoF) for K users multiple-input-multiple-output (MIMO) interference channels. However, due to the feasibility constraint, aligning all the interference signals at each receiver is impractical for large K without symbol extension. In this paper, we propose two best-effort interference alignment (BEIA) schemes that the network selects the maximum number of interfering transmitters to align their signals given the feasibility conditions when each transmitter-receiver pair has a constant number of data streams. Besides, in case of not all interfering signals aligned at each receiver, an upper bound of the average throughput is derived. Simulation results show that the proposed schemes have superiority over the traditional methods, such as time division multiple access (TDMA) and cluster IA(CIA), in low and moderate signal-to-noise ratio (SNR) region in terms of average user throughput. In addition, the proposed max-min relative interference distance alignment scheme outperforms the proposed scheme of equal interfering transmitters number alignment in terms of both average user throughput and minimum user throughput.

• 한국지반공학회지:지반
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• 제6권1호
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• pp.7-14
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• 1990

주동단에 반력스프링이 부착된 공진주(spring-top resonant column) 시험기 주동단 불완전 고정의 영향을 연구하기 위해 2자유도 모델을 제안하였다. SYMPHONY스프레드쉿트를 이용하여 무차원주파수, F를 구할 수 있도록 전산화하였으며 이로부터 탄성계수를 구할 수 있다. F에 대한 반력 질량의 영향은 반력질량 및 시료의 질량 및 주파수에 관계되는 계수, T<20인 경우에 는 무시할 수 없음을 밝혔다. 시험기 및 시료의 질량과 주파수에 관계되는 계수, Tci가 증가함에 따라 F의 영향 역시 증가하였으나 T도 20인 경우 그 영향은 적었다. 주동단 고정을 위해서는 T, 이 20이상 되어야 함을 제안하였으며 이 경우 SDOF으로 취급할 수 있다. 시료와 시험기의 감쇠비는 F에 크게 영향을 미치지 않음도 밝혔다.

• 한국해양공학회지
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• 제20권6호
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• pp.114-122
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• 2006

The most important thing in the container terminal is to handle the cargo effectively in a limited time. To achieve this objective, many strategies have been introduced and applied. If we consider the automated container terminal, it is necessary that the cargo handling equipment is equipped with more intelligent control systems. From the middle of the 1990s, an automated rail-mounted gantry crane (RMGC) and rubber-tired gantry crane (RTG) have been developed and widely used to handle containers in the yards. Recently, in these cranes, equipment like CCD cameras and sensors have been mounted to cope with the automated terminal environment. In this paper, we try to support the development of more intelligent automated cranes that make the cargo handling be performed effectively in the yards. For this plant, we ought to consider modeling, tracking control, anti-sway system design, skew motion suppressionand complicated motion control and suppressing problems. In this paper, the system modeling and a tracking control approach are discussed, based on a two-degree-of-freedom (2DOF) servo-system design. From the simulation results, the good control performance of the designed control system is evaluated.