• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.278-281
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• 2003

The focus of this research is to realize the function which is equivalent to the active suspension system, with controlling semi-active suspension through the attenuation of power variable damper in lower cost and smaller energy. Actually some semi-active suspension systems have been adopted, but they are not sufficient in performance. The authors intended to develop more effective and practical system and applied the optimal control technique. The results of experiments with practical suspension system showed a degree of improvement of comfortableness.

• 한국실천공학교육학회논문지
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• 제5권1호
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• pp.34-39
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• 2013

본 연구에서는 사용자에게 가상환경에 존재하는 교육컨텐츠와 자연스럽게 안터랙션 할 뿐 아니라 인터랙션 양에 따라서 사용자에게 햅틱 정보를 전달해 줄수 있는 휴대용 입력장치를 제시한다. 제안하는 시스템은 사용자의 움직임을 측정하고 움직임에 따라서 사용자에게 햅틱 정보를 되돌려 준다. 교육 컨텐츠와 사용자의 인터랙션에 따른 햅틱 감각을 생성하기 위해 제안하는 입력장치는 모션 제어기, 햅틱 액츄에이터, 무선 통신 모듈, 그리고 모션센서로 구성한다. 사용자의 모션 입력을 측정하기 위해서 가속도 선서를 사용한다. 실험을 통해 제안하는 시스템이 떨림없이 안정적이고 연속적인 햅틱 감각이 생성됨을 파악한다.

• Smart Structures and Systems
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• 제8권3호
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• pp.303-320
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• 2011

Comparing to active damage monitoring, impact localization on composite by using time reversal focusing method has several difficulties. First, the transfer function of the actuator-sensor path is difficult to be obtained because of the limitation that no impact experiment is permitted to perform on the real structure and the difficulty to model it because the performance of real aircraft composite is much more complicated comparing to metal structure. Second, the position of impact is unknown and can not be controlled as the excitation signal used in the active monitoring. This makes it not applicable to compare the difference between the excitation and the focused signal. Another difficulty is that impact signal is frequency broadband, giving rise to the difficulty to process virtual synthesis because of the highly dispersion nature of frequency broadband Lamb wave in plate-like structure. Aiming at developing a practical method for on-line localization of impact on aircraft composite structure which can take advantage of time reversal focusing and does not rely on the transfer function, a PZT sensor array based phase synthesis time reversal impact imaging method is proposed. The complex Shannon wavelet transform is presented to extract the frequency narrow-band signals from the impact responded signals of PZT sensors. A phase synthesis process of the frequency narrow-band signals is implemented to search the time reversal focusing position on the structure which represents the impact position. Evaluation experiments on a carbon fiber composite structure show that the proposed method realizes the impact imaging and localization with an error less than 1.5 cm. Discussion of the influence of velocity errors and measurement noise is also given in detail.