• Journal of the Korean Society for Precision Engineering
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• v.12 no.2
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• pp.59-68
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• 1995

In this study, the effects of the power transmission units on the rotational accuracy are investigated experimentally in a hydrostatic spindle. The effects of warm up time, unbalancing and the position of measuring sensor are pre-examined for the determination of measuring conditions. The misalignment of the power transmission units and the vibration excited by the fluctuation of belt are considered as the dominant parameters of error motion. The variation and scatter of run out at the range of 0 to 3,000rpm in rotational speed are appropriated for the camparison of availabilities of the transmission units to precision spin- dles.

• Journal of the Institute of Electronics and Information Engineers
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• v.54 no.7
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• pp.81-89
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• 2017

Autofocus(AF) Method is essential to overcome the performance degradation due to motion measurement errors under airborne SAR environment. In this paper, back-projection algorithm(BPA) is applied to SAR raw data acquired under the squinted mode, and preprocessing algorithm of AF for BPA is investigated. To apply AF to SAR image effectively, image backplane rotation method and doppler location alignment function for BPA are proposed. The proposed method is applied to SAR raw data acquired in a flight test and shows excellent performance improvement in real data.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.9 no.8
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• pp.1722-1729
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• 2005

In this paper, we used the quadruped walking robot Titan-VIII in order to carry out this simulation of sway compensation trajectory. The attitude angle ${\phi}_r$ and ${\phi}_p$ is obtained from 3-D motion sensor that is attached at the center of robot body and the attitude control carried out at every 10[ms] for stable gait of robot. Duty factor, that is fixed at 0.5. When we change period T into 1.5, 2.0, 3.0[sec] each and moving distance per period is changed into 0.2, 0.3(m), we sim띠ate several walking experiment of robot. and then we analyze the experiment results if there are any difference between the imaginary ZMP and actual ZMP of robot and the stable gait of robot is realized.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.78-78
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• 2017

현재 국내에 공급되고 있는 잡곡류 수확기는 보행형 예취기, 탈곡기 위주의 저능률 기계화 수준으로 고능률의 콤바인 수확기 개발이 필요하며, 특히 잡곡류가 소규모 경작지의 영세농가 위주로 재배되어 저가격의 소형 콤바인 수확기 개발이 절실히 요구되고 있다. 따라서 본 연구는 소규모 밭의 두류 및 잡곡 수확작업에 적응성이 뛰어나며, 농기계 임대사업소의 활용도를 높일 수 있고, 여성과 고령자도 쉽게 운전할 수 있어 수확작업의 노동력을 크게 절감할 수 있는 저가격의 25kW급 자주식 소형 콤바인을 개발하고자 시작기를 설계 제작하였다. 시작기의 주요부로 엔진은 25kW/2600rpm 3기통 디젤엔진을 탑재하였으며, 동력전달부는 주변속 3단, 부변속 2단의 선택맞물림 기어식의 변속장치를 이용하였다. 주행부는 궤도형으로 조향클러치와 습식 원판식 제동장치를 채용하였다. 전처리부는 선단거리 1700 mm의 디바이더와 상하좌우 수동 조절되는 회전속도 약 42 rpm의 정오각형 릴로 구성하였으며, 전처리부의 최대 승강높이는 740 mm이었다. 작물이송부는 돌기부착 오거와 체인컨베이어로 구성되어 있으며, 탈곡부는 단동형 축류식의 직경 440 mm, 길이 1180 mm의 급동과 높이 65 mm, 지름 10 mm의 46개 강봉형 급치, 격자형 수망으로 구성하였으며, 회전속도는 약 325 rpm으로 작동하도록 하였다. 선별 정선부는 요동 송풍선별식으로 곡립판, 볏짚체, 곡립체, 송풍팬으로 구성하였고 송풍팬의 회전속도는 약 850 rpm, 요동진동수는 약 5.8 Hz로 작동하도록 하였다. 곡물이송부와 재처리부는 수평이송 외경 103 mm, 수직이송 외경 110 mm의 피치가 모두 82 mm인 스크류컨베이어를 이용하였으며, 곡물탱크는 용량이 250 로 2개의 배출구로 곡물을 포대에 담도록 하였다. 그 외 시작기는 운전조작부, 유압장치부, 전기장치부 등을 갖도록 설계 제작하였다. 전체적인 기체의 크기는 길이${\times}$폭${\times}$높이 $3935{\times}1900{\times}2440mm$이었으며, 기체 중량은 약 1753 kg이었다. 콩 대상 기초 성능시험 결과 시작기의 작업속도는 약 0.5 m/s, 작업능률은 약 11 a/h로 나타났다.

• Journal of the Korean Electrochemical Society
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• v.3 no.1
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• pp.49-56
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• 2000

In the present we.k, temperature dependence of oxygen diffusivity in the polyvinyl chloride (PVC) film $D_f$ formed on gold electrode was investigated using steady-state rotating disk electrode (RDE) technique and modulated electrohydrodynamic (EHD) impedance technique. Both the diffusion rate defined as the ratio of oxygen diffusivity in the PVC film to the film thickness $D_f/\delta_f$ and the time constant $\delta_f^2/D_f$ for oxygen diffusion through the PVC film were obtained from plot of the limiting current versus disk rotation speed and from filing the EHD impedance spectra experimentally measured to those theoretically calculated on the basis of the diffusion equation for mass transport through the non-conductive and porous film, respectively. By combining measured $D_f/\delta_f$ with $\delta_f^2/D_f$, we determined $\delta_f\;and\;D_f$ at room temperature separately. As temperature increased, it appeared that the $D_f$ value measured for the PVC film-covered gold RDE was enhanced more rapidly than that $D_s$ value in the solution measured for the PVC film-free gold RDE. This means that the pores glowing with increasing temperature act as effective diffusion paths within the film. The present in-situ steady-state and modulated EHD measurements prove to be effective for determining $\delta_f\;and\;D_f$, separately and at the same time the porosity of the PVC film at temperatures below glass temperature $T_g$ of the film.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.382-384
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• 2013

해상 해수면에서 운영되는 등부표의 한정된 면적과 공간에서 전력공급을 할 수 있는 한계가 있다. 정보통신기술(ICT) 발달로 e항로표지, 집약관리시스템등 해양교통시설에 최첨단 기술 접목으로 등부표에 소비전력연동시스템 증가로 인해 절대적인 전력량이 부족하다. 이러한 문제를 해결하기 위하여 비바람으로 인한 사방팔방 격동, 격랑, 회전 요동으로 직달 및 산란광을 태양 전지판에 최대로 입사할 수 있도록 태양의 이동궤적에 따라 자동추적되는 신 구조의 다면구체형 태양광 발전시스템을 개발하였다.

• Korean Journal of Optics and Photonics
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• v.14 no.1
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• pp.58-64
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• 2003

In order to read correct data from a disk-type holographic storage medium, it is very important to implement a servo-control in the pick-up module, as in a conventional CD-ROM. We propose a novel servo-control method using a glass plate on the optical axis, which is able to compensate the mechanical errors coming from wobbling of holographic disk and spindle motor. By rotating the glass plate within $\pm$10 degrees, we can reduce the reading errors of $\pm$200 ${\mu}{\textrm}{m}$ to $\pm$15 ${\mu}{\textrm}{m}$.

• Geophysics and Geophysical Exploration
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• v.16 no.2
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• pp.91-96
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• 2013

This study proposes a method to correct inclination of instrument during exploration with a biaxial clinometer and GNSS compass. In 3-component magnetometry, measured vectors are ordinarily described in randomly inclined observation coordinate system due to movement, vibration, and shaking of instrument. Therefore, rotation angles of observation plane are needed to transform it into geodetic coordinate system. In this study, we measured inclination angles of observation plane by using 2-axis clinometer and GNSS compass, and derived proper parameters for rotational transform from them. We applied the conversion method to on-board 3-component magnetometry, and then transformed raw data into proper values on geodetic coordinate system.

• Smart Media Journal
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• v.8 no.4
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• pp.38-45
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• 2019

When there is a spray flow such as from a pesticide nozzle, winds affect the droplet flow of a rotary-wing drone accompanied by a strong wake, with a severe oscillation. Especially, during forwarding flights or when winds come from the side, compare to a simple hovering flight as the droplet is in the effect of aerodynamic drag force, the effect of spraying region becomes even larger. For this reason, the spraying of pesticides using drones may cause a greater risk of scattering or a difference in droplet dispersion between locations, resulting in a decrease in efficiency. Therefore, through proper numerical modeling and its applied simulation, an indication tool is required applicable for the various flight and atmospheric conditions. In this research, we completed both experiment and numerical analysis for the strong downwash from the rotor and flight velocity of the drone by comparing the probability density function of droplet distribution to build a spraying system that can improve the efficiency when spraying droplets in the pesticide spray drone.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.3
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• pp.197-209
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• 2018

In this study, numerical analyses on Quad Tilt Rotor(QTR) are carried out to investigate the interference effect of components and effect of operating condition during forward flight. Actuator Surface Method(ASM) which is implemented in an open source CFD code, OpenFOAM, is used to calculate the flow field around QTR with high computational efficiency. The lift of the front and rear wing is found to increase or decrease depending on the rotation direction of the rotor. At the rear wing, the interference effects of the front and rear rotor appear as a combined manner. Performance change due to the phase difference is found to be insignificant. For both rotors, the locally higher thrust is generated by the blockage effect of the wing. The interference effect of wake from the front nacelle contributes to higher local thrust for the rear rotor compared to the front rotor. And it is observed that the amplitude of thrust oscillation can decrease depending on the phase difference between the rotors. Aerodynamic performances of both rotors and the entire aircraft were compared and analyzed for various operating conditions.