• Journal of the Korean Society for Precision Engineering
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• v.14 no.12
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• pp.114-120
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• 1997

For compensating the error motion of hydrostatic tables, we have introduced a way that the clearance of table is controlled corresponding to the amount of eror with the actively controlled variable capillary, named as ACC. In previous paper, through the basic test, it was confirmed that by the use of ACC, the error motion within 2.7$\mu$ m of a hydrostatic table could be compensated with the resolution of 27nm, 1/100 contollable range, and with the frequency bandwidth of 5.5Hz, structurally. In this paper, we performed practical compensation of the linear and angular motion error of hydrostatic table using ACC. For improving the compensated motion accuracy, iterative control method is put into the control system. The experimental results show that by the simultaneous compensation of error, the linear and angular motion error are improved upto 0.25$\mu$ m and 0.4arcsec, which are about 1/10 and 1/3 of the non-compensated motion errors respectively.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1991.04a
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• pp.59-67
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• 1991

공작기계의 정밀도는 가공물의 최종 치수 정밀도와 직접적으로 연계되는 공작기계의 전체적 성능 평가를 위한 주요인자 중의 하나이다. 공작기계 위치 결정 정밀도에가장 큰 영항을 주는 인자로서는 이송계의강성, Back lash, 안내면의 습동저항 그리고 이송 계의 자세변화등이 해당된다. 본 연구에서는 이송나사로구동되는 CNC 원통 연삭기의 숫돌대(Wheel Head)축 이송 구동계의 오차발생 요인에 대해 실험적인 검토를 수행하였다. 이를 위하여 이송 구동계의 정강성에따른 영향과 이송 안내면의 각운동에 의한 위치정밀도 영향 및 위치 검출 장치의 종류에 따른 위치오차의 재현성(Repeatatility)의 유무를 레이 저 간섭계를 이용한 정밀 측정을 통하여 비교 검토함에 의해 이송 오차를 최소화 시킬 수 있는 CNC 공작기계이송 구동축 설계의 기본 방향을 마련하는데 역점을 두고 연구를 수행하게 되었다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2003.11a
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• pp.579-585
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• 2003

This paper investigates the whirling, tilting and flying motion of a HDD spindle system supported by FDB experimentally. Experimental setup is built to measure the flying, whirling and tilting motion of the HDD spindle system, and three capacitance probes fixed on the xyz-micrometers measure the displacement of a HDD spindle system in the xyz-directions. This research shows that the tilting and whirling motion is mostly dependent on the centrifugal force and the gyroscopic moment due to the unbalanced mass of a HDD spindle. It also shows that the rotating HDD spindle starts to float to the equilibrium position in the z-direction until the weight of the rotating spindle is equal to the supporting pressure generated in the upper and lower thrust bearing.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.11
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• pp.837-847
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• 2020

A velocity profile for flapping flight is optimized to increase the power efficiency of 20g weighted flapping wing micro air vehicle in hover. The experimental optimization of flapping velocity profile is carried out with a real sized flapper, and various velocity profiles are realized by non-circular gear. Kriging with noise is adopted as a meta model of the profile optimization to reflect the data noise by uncertainty. The optimization results confirm that the flapping efficiency (thrust-to-power ratio) is substantially improved (11.3%) through the elastic deformation that carries the angular kinetic energy from previous stroke.