• 한국항공우주학회지
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• 제37권12호
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• pp.1217-1224
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• 2009

고정익 항공기가 3차원의 복잡한 경로를 추종하기 위해 필요한 비교적 간단하며 효과적인 유도 제어 방법을 제시한다. 소개되는 방법은 비선형 경로 추종 유도 기법을 외부 루프로 사용한다. 외부 루프는 원하는 경로와 함께 항공기의 현재 위치와 속도를 바탕으로 비행 경로를 변화하기 위한 가속도 명령을 생성한다. 가속도 명령은 중력과 벡터적으로 결합되어 Specific Force Acceleration을 만든다. 이렇게 생성된 Specific Force Acceleration은 내부 루프를 위한 명령으로 쓰이는데, 이는 항공기가 가속도 자체보다는 Specific Force Acceleration을 더 직접적으로 제어할 수 있기 때문이다. 나아가 배면 비행이나 Slow Roll, Knife-Edge 등과 같은 옆미끄럼짐 기동을 하기 위해 필요한 롤 자세 제어 기법도 제시한다. 마지막으로 표준이 되는 여러 가지 곡예비행 경로들에 대한 시뮬레이션을 수행함으로써 제시된 기법의 성능을 검증한다.

• 한국소음진동공학회논문집
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• 제24권8호
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• pp.592-599
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• 2014

A torsional vibration at driveline happens seriously at rapid vehicle acceleration. The torsional vibration at driveline can be reduced by optimization of joint angle and yoke phase angle of driveline. But, the joint angle of driveline is changed according to vehicle driving condition as acceleration, deceleration, forward and backward driving, so that excessive vibration is transmitted to vehicle body at specific driving condition. Especially under rapid acceleration condition, vibration transmitted to body could be maximized because excitation force at rapid acceleration is bigger than that at normal driving condition due to changed joint angle. The torsional vibration of driveline can be kept at low level by controlling suspension parameter to minimize rigid axle displacement as well as optimizing joint angles considering the vehicle acceleration condition.

• 한국항공우주학회지
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• 제45권2호
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• pp.106-113
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• 2017

항공기 및 지상 이동체 등에 사용되는 자세 및 방위 결정 시스템은 자세를 결정하기 위해 중력가속도 벡터와 지구자기장 벡터를 이용한다. 이를 위해 가속도계와 자력계를 이용하게 되는데, 가속도계의 경우 중력가속도뿐만 아니라 항체의 운동 가속도까지 포함하게 되어 가속 중에는 자세결정이 어려워진다. 본 논문에서 다루는 가속도 보상 방법은 가속도계에서 얻은 비력으로부터 GPS 수신기를 통해 계산한 항체의 가속도를 빼주어 이를 해결하는 방법이다. 기존의 알고리즘은 보상한 벡터를 상수 형태로 간주해 이용하게 되는데, 본 논문에서는 이로 인한 오차를 분석하고 측정치로부터 모델을 재유도해 성능을 개선했다. 기존의 알고리즘이 내포한 오차 요인과 본 논문에서 제안한 알고리즘에 의해 자세 추정 성능이 개선됨을 컴퓨터 시뮬레이션을 통해 확인했다.

• 전자공학회논문지T
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• 제36T권1호
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• pp.64-70
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• 1999

본 논문에서는 매니퓰레이터로 작업체 이동시 이동방향 가, 감속에 따른 미끄럼, 회전등의 위치에러 방지를 위한 그리퍼 힘 제어를 작업계획도를 설정해 구간별로 알아본다. 또한 작업체와 매니퓰레이터사이에 가장 정확한 정보를 제공할 수 있는 tactile 센서를 그리퍼에 부착해 연속적으로 tactile 영상 데이터 추론을 통해 미끄럼과 회전을 감지한다. 계산된 파지력과 감지된 에러량 비교를 통해 보상제어와 이를 응용한 최적의 파지력을 구할 수 있다. tactile 센서로는 압각센서인 FSR(Froce Sensing Resistor)을 사용해 22×22 센서회로를 구성하였다. 전처리로써 연속적인 taxel 수를 문턱값으로 설정해 필터링 작업을 하였고, 모멘트 메써드를 감지 알고리즘으로 사용해 실험하였다.

• 제어로봇시스템학회지
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• 제16권3호
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• pp.40-45
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• 2010

물체의 운동을 측정하기 위하여 관성 센서(inertial sensor)에 대한 배경 지식이 없는 사용자가 가속도계(accelerometer)를 사용하고자 할 경우 센서의 이름이 주는 혼동에 의하여 물체의 운동 가속도(acceleration)를 쉽게 얻어낼 수 있으리라 기대하게 된다. 반면, 가속도계가 실제 측정하여 주는 값은 비력 가속도(acceleration due to specific force)에 해당되므로 적절한 처리를 부가하지 않으면 기대한 바와 같이 물체의 운동 가속도를 얻을 수 없다. 가속도계의 측정값으로부터 운동 가속도를 추출하기 위해서는 중력장 가속도 (gravitational acceleration), 중력 가속도 (acceleration due to gravity), 비력 가속도, 그리고 운동 가속도 사이의 관계를 명확하게 구분 이해할 필요가 있다. 본 고에서는 앞선 고들에서 다룬(막대) 벡터, 좌표값, 좌표계, 좌표변환행렬, 그리고 코리올리 효과 등의 개념을 확장하여 다양한 개념의 가속도들을 구분 설명하였다.

• Earthquakes and Structures
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• 제24권1호
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• pp.53-64
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• 2023

Earth fissures with several kilometers will inevitably approach or cross the metro line, significantly threatening the safety of the underground structure in the earth fissure site. However, the influence of the earth fissure site's amplification effect on the metro station's dynamic response is still unclear. A representative earth fissure in Xi'an was taken as an example to establish a numerical model of a metro station in the earth fissure site. The dynamic response characteristics of the metro stations at different distances from the earth fissure under various seismic waves were calculated. The results show that the existence of the earth fissure significantly amplifies the dynamic response of the nearby underground structures. The responses of the axial force, shear force, bending moment, normal stress, horizontal displacement, inter-story drift, and relative slip of the metro station were all amplified within a specific influence range. The amplification effect increases with the seismic wave intensity. The amplification effect caused by the earth fissure has relatively weak impacts on the axial shear, shear force, bending movement, normal stress, and horizontal movement; slightly larger impacts on the inter-story drift and acceleration; and a significant impact on the relative slip. The influence ranges of the axial force and normal stress are approximately 20 m. The influence ranges of the acceleration and inter-story drift can reach 30 m. Therefore, the seismic fortification level of the underground structure in the earth fissure site needs to be improved.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제50권3호
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• pp.136-143
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• 2001

A micro particle manipulator, which is devised for trapping particles at fixed positions by negative dielectrophoretic force (DEP force), has been fabricated and experimented. It is composed of square type electrode arrays fabricated by nickel electroplating with the height of 28 ${\mu}m$. To improve the quality of electroplated nickel electrodes, plating conditions have been optimized. Micro particles used in this study are polystyrene spheres and their to the specific position and trapped. The DEP force along the moving path of the particles has been estimated by the motion equation of a single particle. The displacement of a particle with an elapsed time was measured using a high-speed camera (1000 frames/sec). The velocity and acceleration of the particle were calculated from the measured data. The DEP force acting on the particle was estimated.

• International Journal of Control, Automation, and Systems
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• 제4권1호
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• pp.10-16
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• 2006

In this paper, moving a fragile object from an initial point to a specific location in the minimum time without damage is studied. In order to achieve this goal, initially, the maximum acceleration and velocity ranges are specified. These ranges can be dynamically generate on the planned path by the manipulator. The path can be altered by considering the geometrical constraints. Later, considering the impulsive force constraint on the object, the range of maximum acceleration and velocity are obtained to preserve object safety while the manipulator is carrying it along the curved path. Finally, a time-optimal trajectory is planned within the maximum allowable range of acceleration and velocity. This time-optimal trajectory planning can be applied to real applications and is suitable for both continuous and discrete paths.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
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• pp.327-332
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• 2006

In airborne gravimetry, there are two data streams. One is the specific force measured by an air/sea gravimeter or accelerometers, the other is kinematic acceleration measured by DGPS. And the difference of them provides the gravity disturbance information. To satisfy the requirement of most applications, an accuracy of 1mGal $(1mCal=10^{-5}m/s^{2})$ with a spatial resolution of 1km is the aim of current airborne gravimetry. There are two different methods to derive the kinematic acceleration. The generally used method is to differentiate the position twice, and the position can be calculated by commercial DGPS software. The main defect of this method is that integer ambiguities need to be fixed to get the precise position solution, but it's not a trivial thing for long base line. And to fix integer ambiguities, the noisier iono-free measurement is used. When differentiation is applied, noise is amplified and will influence the accuracy of acceleration. The other method is to get carrier phase acceleration by differentiate the carrier phase first, and then using the acceleration of GPS satellite to derive the vehicle acceleration. The main advantages include that fixing integer ambiguities is not needed anymore, position can be relaxed to about 10 meters, and smoother acceleration can be got since iono-free measurement is not needed. In some literatures, it's considered that the dynamic performance of the second method is inferior to that of the first. Through analysis, it is found that the performance degradation in dynamic environment results from the simplification of the GPS carrier phase observable model. And an iterative algorithm is presented to compensate the model error. Using a dynamic GPS data from an aeromagnetic survey, the importance of this compensation is showed at last.

• Earthquakes and Structures
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• 제9권4호
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• pp.875-891
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• 2015

Earthquake can occur anywhere in the world and it is essential to design important members in special structures based on maximum possible forces that can be produced in them under severe earthquake. In addition, since the earthquake is an accidental phenomena and there are no similar earthquakes, therefore the possibility of strong earthquakes should be taken into account in earthquake-resistant design of important structures. Based on this viewpoint, finding the critical acceleration which maximizes internal forces is an essential factor in structural design. This paper proposes critical excitation method to compute the critical acceleration in design of important members in special structures. These critical accelerations are computed so that the columns' internal shear force at the base of the structure at each time step is maximized under constraints on ground motion. Among computed critical accelerations (of each time step), the one which produces maximum internal shear force is selected. A numerical example presents to show the efficiency of critical excitation method in determining the maximum internal shear force and base moment under variety of constraints. The results show that these method can be used to compute the resonant earthquake which have large enough effective duration of earthquake strong motion (between 12.86 sec to 13.38 sec) and produce the internal shear force and base moment for specific column greater than the same value for selected earthquakes in constructing the critical excitation (for different cases about 2.78 to 1.29 times the San Fernando earthquake). Therefore, a group of them can be utilized in developing the response spectrum for design of special structures.