• 한국항공우주학회지
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• 제41권5호
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• pp.350-356
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• 2013

먼거리에서 접촉하지 않고 측정할 수 있다는 장점으로 인해 사진계측은 항공분야에서도 널리 활용되고 있다. 본 연구에서는 한 대의 카메라로 6자유도 해석을 수행하는 사진계측에서 발생할 수 있는 오차를 분석하였다. 사진계측의 오차 분석 프로그램을 개발하였으며, 사진계측 문제를 공선조건에 기반한 기하학적 문제로 변환하여 프로그램을 검증하였다. 각 좌표계간 6자유도 해석을 위해 필요한 카메라 포즈에 대한 통계량은 정규분포한다는 것을 수치실험을 통해 유추할 수 있었으며, 모표준편차를 이용하여 사진계측의 오차를 정량화하였다.

• 한국항해항만학회지
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• 제40권5호
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• pp.231-239
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• 2016

In general, the attitude of a high-speed planning boat changes following a speed change. Since the hydrodynamic forces acting on a ship differ according to the change of its underwater shape, it is difficult to estimate its hydrodynamic force compared to that of a large commercial ship. In this paper, 6 Degrees Of Freedom (DOF) equations of motion that express the maneuvering motion of a planning boat are modeled by analyzing its motion characteristics based on various sea trial tests. Finally, a maneuvering simulation is carried out and a validation of the equations of motion is confirmed with the results of sea trial tests.

• Structural Engineering and Mechanics
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• 제5권1호
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• pp.33-49
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• 1997

A method of analysis is proposed for curved multicell box girder grillages. The method can be used to analyze box girder grillages comprising straight and/or curved segments. Each segment can be modelled by a number of beam elements. Each element has three nodes and the nodal degrees of freedom (DOF) consist of the six DOF for a conventional beam plus DOF to account for torsional warping, distortion, distortional warping, and shear lag. This element is an extension of a straight element that was developed earlier. For a more realistic analysis of the intersection regions of non-colinear box girder segments, the concept of a rigid connector is introduced, and the compatibility requirements between adjoining elements in those regions are discussed. The results of the analysis showed good agreement with the shell finite element results, but the proposed method of analysis needs a fraction of the time and effort compared to the shell finite element analysis.

• Smart Structures and Systems
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• 제5권3호
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• pp.279-290
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• 2009

Two degrees of freedom resonant systems are employed to improve the resonant property of resonant sensor, as compared to a single degree of freedom resonant system. This paper presents design, development and testing of two degrees of freedom resonant sensor. To measure absolute mass, cantilever shaped two different masses (smaller/absorber mass and bigger/drive mass) with identical resonant frequency are mechanically linked to form 2 - Degree-of-Freedom (DOF) resonator which exhibits higher amplitude of displacement at the smaller mass. The same concept is extended for measuring differential quantity, by having two bigger mass and one smaller mass. The main features of this work are the 3 - DOF resonator for differential detection and the microcontroller based closed loop electronics for resonant sensor with piezoelectric sensing and excitation. The advantage of using microcontroller is that the method can be easily extended for any range of measurand.

• 대한기계학회논문집A
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• 제28권5호
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• pp.495-502
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• 2004

In this paper, kinematic structure of parallel manipulator having 6-DOF is determined to follow the specific trajectory represented by several curves expressed by the parametric variable functions. In addition, the parallel manipulator is designed to have a high dexterity by considering a kinematic isotropy which can stabilize the motion of the moving platform in the restricted workspace.

• Journal of Electrical Engineering and Technology
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• 제6권5호
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• pp.618-625
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• 2011

This paper presents a double excited three degree-of-freedom (3DOF) motor. The proposed 3DOF motor is designed with a laminated structure, making it easy to manufacture. In addition, it has windings on the stator and rotor, and does not require an expensive permanent magnet. We explain the structure, principle of motion, and design of the proposed motor, and perform an analysis of the static characteristics using the two- and three-dimensional finite element methods (3D FEM). The feasibility of 3D FEM analysis is confirmed by comparing the 3D FEM analysis and experimental results for the rolling and pitching motion. We also confirm the occurrence of holding torque in every motion.

• 한국항공우주학회지
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• 제43권12호
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• pp.1124-1131
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• 2015

이 논문은 지상에서 초소형 위성의 랑데부/도킹 알고리즘 개발을 위하여 미세중력환경을 모사해주는 5자유도 지상 테스트베드에 관하여 기술한다. 테스트베드는 지면과의 마찰력을 없애주는 하부와 이 하부에 연결되어 3자유도의 회전운동을 하는 상부로 구성된다. 영상기반의 항법알고리즘 개발을 위하여 카메라와 LIDAR, AHRS 센서를 사용하였고 액추에이터로는 8개의 냉가스 추력기와 3축 방향의 반작용 휠을 사용하였다. 모든 시스템 소프트웨어는 온보드와 리눅스를 기반으로 C++을 사용하여 구현되었다.

• 한국항공우주학회지
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• 제35권5호
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• pp.381-389
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• 2007

외부장착물의 효율적인 분리해석을 위해 6-DOF 시뮬레이션 프로그램을 개발하였다. 이 S/W는 장착물에 작용하는 공기력을 미리 작성된 공력 데이터베이스를 이용하여 간단한 보간으로 얻기에 전산유체역학에 기초한 방법에 비해 매우 빠른 계산시간을 가지며, 고정된 형상의 무장 뿐 아니라 분리 중 날개를 전개하는 무장에 대해서도 해석이 가능하다. 본 논문에서는 날개전개 무장의 공력 데이터베이스를 MSAP(Multi-body Separation Analysis Program)을 이용하여 작성하고, 비정상 감쇠계수를 Missile Datcom을 이용하여 예측하였다. 이 데이터베이스와 6-DOF 시뮬레이션 프로그램으로 무장의 고정된 날개 뿐 아니라, 날개전개에 따른 무장의 분리 안전성을 판단하였다

• Wind and Structures
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• 제26권2호
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• pp.57-68
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• 2018

Wind tunnel tests are conducted to investigate wake-induced vibrations of two circular cylinders with a center-to-center spacing of 4 diameters and attack angle varying from $0^{\circ}$ to $20^{\circ}$ for Reynolds numbers between 18,000 and 168,800. Effects of structural damping, Reynolds number, attack angle and reduced velocity on dynamic responses are examined. Results show that wake-induced vortex vibrations of the downstream cylinder occur in a wider range of the reduced velocity and have higher amplitudes in comparison to the vortex-induced vibration of a single circular cylinder. Two types of wake-induced instability phenomena with distinct dynamic characteristics are observed, which may be due to different generation mechanisms. For small attack angles like $5^{\circ}$ and $10^{\circ}$, the instability of the downstream cylinder characterizes a one-degree-of-freedom (1-DOF) oscillation moving in the across-wind direction. For a large attack angle like $20^{\circ}$, the instability characterizes a two-degree-of-freedom (2-DOF) oscillation with elliptical trajectories. For an attack angle of $15^{\circ}$, the instability can transform from the 1-DOF pattern to the 2-DOF one with the increase of the Reynolds number. Furthermore, the two instabilities show different sensitivity to the structural damping. The 1-DOF instability can be either completely suppressed or reduced to an unsteady oscillation, while the 2-DOF one is relatively less sensitive to the damping level. Reynolds number has important effects on the wake-induced instabilities.

• 한국정밀공학회지
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• 제31권5호
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• pp.423-430
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• 2014

In this study, the five-DOF motion at ultra-precision linear stage under static and dynamic conditions are evaluated through the extending application of ISO 230-2. As the performance factors, the bi-directional accuracy and repeatability of the five-DOF motion are quantitatively evaluated with the measurement uncertainties which are determined using the standard uncertainty of equipment used in experiment. The motion under static condition are analyzed using geometric errors. The five geometric errors except the linear displacement error are measured using optimal measurement system which is designed to enhance the standard uncertainty of geometric errors. In addition, the motion under dynamic conditions are analyzed with respect to the conditions with different feed rate of the stage. The experimental results shows that the feed rate of stage has a significant effect on straightness motions.