• 대한기계학회논문집A
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• 제35권1호
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• pp.115-120
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• 2011

본 논문에서는 해양 풍력발전기를 해상 크레인으로 리프팅하기 위해 두 개의 탄성 붐을 가진 해상 크레인을 모델링 하고 동적 거동을 시뮬레이션 하였다. 운동 방정식은 강체와 탄성체가 포함된 다물체계 동역학을 기반으로 구성하였다. 외력으로는 유체정역학 힘, 규칙파에 의한 유체동역학 힘, 와이어로프의 장력, 계류력, 그리고 중력이 고려되었다. 두 개의 탄성 붐을 사용한 시뮬레이션 결과는 탄성 붐 한 개를 사용한 경우와 비교하여 모델의 타당성을 검증하였다. 5-MW(megawatt)급 해양 풍력 발전기를 해상 크레인이 리프팅하는 경우에 대해 동적 거동을 시뮬레이션하고 그 결과를 분석하였다.

• 한국해양공학회지
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• 제36권1호
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• pp.50-60
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• 2022

The deep ocean engineering basin (DOEB) of the Korea Research Institute of Ship and Ocean Engineering (KRISO) is equipped with an extreme-environment reproduction facility that can analyze the motion characteristics of offshore structures and ships. In recent years, there have been requirements for a wide range of six-degree-of-freedom (6-DOF) motion measurements for performing maneuvering tests and free-running tests of target objects (offshore structures or ships). This study introduces the process of developing a wide-area motion measurement technology by incorporating the auto-tracking technology of the towing carriage system to overcome the existing 6-DOF motion measurement limitation. To realize a wide range of motion measurements, the automatic tracking control system of the towing carriage in the DOEB was designed as a speed control method. To verify the control performance, the characteristics of the towing carriage according to the variation in control gain were analyzed. Finally, a wide range of motions was tested using a model test object (a remotely operated vehicle (ROV)), and the wide-area motion measurement technology was implemented using an automatic tracking control system for a towing carriage.

• Structural Engineering and Mechanics
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• 제30권5호
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• pp.535-558
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• 2008

This study evaluates seismic performance of the school buildings with the selected template designs in Turkey considering nonlinear behavior of reinforced concrete components. Six school buildings with template designs were selected to represent major percentage of school buildings in medium-size cities located in high seismic region of Turkey. Selection of template designed buildings and material properties were based on field investigation on government owned school buildings in several cities in western part of Turkey. Capacity curves of investigated buildings were determined by pushover analyses conducted in two principal directions. The inelastic dynamic characteristics were represented by equivalent single-degree-of-freedom (SDOF) systems and their seismic displacement demands were calculated under selected ground motions. Seismic performance evaluation was carried out in accordance with recently published Turkish Earthquake Code that has similarities with FEMA-356 guidelines. Reasons of building damages in past earthquakes are examined using the results of performance assessment of investigated buildings. The effects of material quality on seismic performance of school buildings were investigated. The detailed examination of capacity curves and performance evaluation identified deficiencies and possible solutions for template designs.

• 제어로봇시스템학회논문지
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• 제14권9호
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• pp.916-924
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• 2008

In this paper dynamic modeling parameters were estimated using a frequency domain estimation method. A systematic flight test method was employed using preprogrammed multistep excitation of the swashplate control input. In addition when one axis is excited, the autopilot is engaged in the other axis, thereby obtaining high-quality flight data. A dynamic model was derived for a small scale unmanned helicopter (CNUHELI-020, developed by Chungnam National University) equipped with a Bell-Hiller stabilizer bar. Six degree of freedom equations of motion were derived using the total forces and moments acting on the small scale helicopter. The dynamics of the main rotor is simplified by the first order tip-path plane, and the aerodynamic effects of fuselage, tail rotor, engine, and horizontal/vertical stabilizer were considered. Trim analysis and linearized model were used as a basic model for the parameter estimation. Doublet and multistep inputs are used to excite dynamic motions of the helicopter. The system and input matrices were estimated in the frequency domain using the equation error method in order to match the data of flight test with those of the dynamic modeling. The dynamic modeling and the flight test show similar time responses, which validates the consequence of analytic modeling and the procedures of parameter estimation.

• 대한조선학회논문집
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• 제36권1호
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• pp.1-14
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• 1999

Nakato & Ha[2]는 정상풍(steady wind) 및 파랑충격의 외력을 받는 소형경주정의 운동 및 전복에 관한 시뮬레이션 연구 결과를 발표하였다. 경주정의 시뮬레이션은 실험 데이터를 이용하고 외력을 고려한 항공역학에서 일반적으로 사용되는 6자유도 운동방정식을 풀어서 수행하였다. 본 논문에서는 선미플랩을 부착하여 양력을 발생토록하여 Nakato & Ha의 운동 방정식을 수정하였다. 플랩에 의한 경주정의 제어는 바람과 파도의 중첩된 외부교란에 의한 전복현상을 상당히 억제시킬 수 있음을 알았다.

• International Journal of Aeronautical and Space Sciences
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• 제2권2호
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• pp.1-18
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• 2001

A numerical technique for simulating the separation dynamics of strap-on boosters jettisoned in the dense atmosphere is presented. Six degree of freedom rigid body equations of motion are integrated into the three-dimensional unsteady Navier-Stokes solution procedure to determine the dynamic motions of strap-ons. An automated Chimera overlaid grid technique is introduced to achieve maximum efficiency for multi-body dynamic motion and a domain division technique is implemented in order to reduce the computational cost required to find interpolation points in the Chimera grids. The flow solver is validated by comparing the computed results around the Titan IV launch vehicle with experimental data. The complete analysis process is then applied to the. H-II launch vehicle, the central rocket in japans space program, the CZ-3C launch vehicle developed in China and the KSR-III, a three-stage sounding rocket being developed in Korea. From the analyses, separation trajectories of strap-on boosters are predicted and aerodynamic characteristics around the vehicles at every time interval are examined. In addition, separation-impulse devices generally introduced for safe separation of strap-ons are properly modeled in the present paper and the jettisoning force requirements are examined quantitatively.

• 대한조선학회논문집
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• 제40권4호
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• pp.16-21
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• 2003

The very large container ships have been built recently and those ships have very small structural rigidity compared with the other conventional ships. As a result, the destruction of ship hull is occurred by the springing including to warping phenomena due to encounter waves. In this study, the solutions of hydrodynamic coefficients are obtained by solving the three dimensional source distribution method and the forward speed Green function representing a translating and pulsating source potential for infinite water depth is used to calculating the integral equation. The vessel is longitudinally divided into various sections and the added mass, wave damping and wave exciting forces of each section is calculated by integrating the dynamic pressures over the mean wetted section surface. The equations for six degree freedom of motions is obtained for each section in the frequency domain and stiffness matrix is calculated by Euler beam theory. The computations are carried out for very large ship and effects of bending and torsional ridigity on the wave frequency and angle are investigated.

• 한국해양공학회지
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• 제30권2호
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• pp.84-90
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• 2016

In this study, a six degree-of-freedom motion analysis of a wind-wave hybrid platform equipped with numerous wave energy converters (WECs) was carried out. To examine the effect of the WECs on the platform, an analysis of one-way coupling was carried out, which only considered the power take-off (PTO) damping of the static WECs on the platform. The equation of motion of a floating platform with mooring lines in the time domain was established, and the responses of the one-way coupled platform were then compared with the case of a platform without any coupling effects from the WECs. The hydrodynamic coefficients and wave exciting forces were obtained from the 3D diffraction/radiation pre-processor code WAMIT based on the boundary element method. Then, an analysis of the dynamic responses of the floating platform with or without the WEC effect in the time domain was carried out. All of the dynamics of a floating platform with multiple wind turbines were obtained by coupling FAST and CHARM3D in the time domain, which was further extended to include additional coupled dynamics for multiple turbines. The analysis showed that the PTO damping effect on platform motions was negligible, but coupled effects between multiple WECs and the platform may differentiate the heave, roll, and pitch platform motions from the one without any effects induced by WECs.

• 한국지능시스템학회논문지
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• 제26권2호
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• pp.147-152
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• 2016

형상기억합금은 가열되거나 냉각될 때 모양과 강도가 변화하면서 큰 힘을 발생한다. 와이어 형태의 형상기억합금은 열을 가하면 길이가 축소되면서 상당히 큰 힘을 발휘하며, 소음없는 운동을 발생시킬 수 있으므로 모터를 대체할 수 있는 구동기로 활용가능하다. 이런 형상기억합금 구동기는 전기로 직접 가열할 수 있으며, 큰 범위의 운동을 만들어내는데 사용될 수 있다. 본 논문에서는 형상기억합금 구동기를 이용하여 3 개의 손가락을 가진 6 자유도의 로봇 손을 개발하고 제어하는 것에 대해 기술한다. 각 손가락은 2 개의 관절을 가지고 있으며, 각 관절은 길항(拮抗) 운동을 위해 서로 반대로 동작하는 두 개의 힘줄에 의해 구동된다. 부드러운 운동을 위한 충분한 힘을 만들어 내기 위해 각 힘줄은 2 개의 형상기억합금 구동기가 병렬로 구성된다. 형상기억합금 구동기를 가열하기 위한 전류를 제어하기 위해 PWM 드라이버를 채용하였으며, 실험을 통해 손가락의 길항 작용을 평가한다.

• 한국해양공학회지
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• 제29권3호
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• pp.270-282
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• 2015

A submerged body moving near the free surface needs to maintain its attitude and position to accomplish missions. It is necessary to validate the performance of a designed controller before a sea trial. The hydrodynamic coefficients of maneuvering are generally obtained by experiments or computational fluid dynamics, but these coefficients have uncertainty. Environmental loads such as the wave exciting force and suction force act on the submerged body when it moves near the free surface. Thus, a controller for the submerged body should be robust to parameter uncertainty and environmental loads. In this paper, the six-degree-of-freedom equations of motions for the submerged body are constructed. The suction force is calculated using the double Rankine body method. An adaptive control method based on an artificial neural network and proportional-integral-derivative control are used for the depth controller. Simulations are performed under various depth and speed conditions, and the results show the effectiveness of the designed controller.