• Journal of the Korean Crystal Growth and Crystal Technology
• /
• v.30 no.2
• /
• pp.73-77
• /
• 2020

In this study, phosphor ceramics were fabricated, and optical properties were analyzed for application to nextgeneration automotive laser headlamps by using a spherical YAG : Ce phosphor with a garnet structure synthesized based on the spray drying method. The thickness of phosphor ceramic using spherical YAG : Ce phosphor was obtained with 100 ㎛, 150 ㎛, and 200 ㎛ to investigate the effect of thickness on optical properties such as light conversion efficiency, heat dissipation, luminance and color temperature. The results of this study are expected to play a significant role in the manufacturing process for the fabrication of phosphor ceramic by solving issues such as the high cost and low yield in the conventional liquid method to manufacture YAG : Ce nano fluorescent materials.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.44 no.12
• /
• pp.1035-1042
• /
• 2016

By using commercial flight simulation game engine, X-Plane, we have studied QTG(Qualification Test Guide) generation that can satisfy FTD level 5. Flight model is SR-20 of Cirrus. In list of QTG, There are some items to measure control forces. therefore, we have installed CLS(Control Loading System) to flight control devices in order to make it possible to measure control forces. We made Autopilot function externally to make flight model in trim conditions because X-Plane don't provide internal trim routine function. In addition to develop an algorithm, it can automatically perform the test. To avoid the inconvenience to control as it was to be carried out in same conditions. In case of FTD level 5, it is possible to use alternative data sources not only real flight data. By using these alternative data sources, all test results satisfy a scope given by CFR Part 60.

• Journal of Digital Contents Society
• /
• v.16 no.4
• /
• pp.513-522
• /
• 2015

Various types of digital displays from PC monitor up to smart watch have been developed in response to the dramatic technological progress of electronics. Accordingly, web content creators have the need to provide web contents respectively depending on the different display environments, which increases production time and costs. As a technique for overcoming this, the responsive web design method has been proposed, which means a web page with the size of the screen being adjusted depending on the types of display. Although the responsive web system is increasingly implemented in the region of contents search pages of domestic portals, there are still many cases that contents are implemented separately for PC and for mobile. In this paper, we investigate the responsive types of the web implementation of contents search pages of domestic portal, and propose an efficient new UI for responsive web to individual types of contents search pages which responsive design is not applied to.

• Proceedings of the Korean Society for Agricultural Machinery Conference
• /
• 2017.04a
• /
• pp.121-121
• /
• 2017

오늘날 시장에 유통되는 버섯은 대부분 환경이 조절되는 시설 내부에서 재배된다. 버섯은 다른 식물과 달리 버섯의 종류, 품종 등에 따라 요구되는 환경이 매우 다르다. 특히 대부분의 버섯은 버섯이 생육되는 공간의 온도, 수분, 이산화탄소, 조도 등의 관리가 필수적이다. 버섯의 단위면적당 생산량을 극대화하기 위해서는 이들 버섯이 필요로 하는 환경을 버섯의 생육특성에 따라 적합하게 유지해 주어야만 한다. 현재 대부분의 버섯재배사에는 이들 환경을 컨트롤하는 장치가 설치되어 있고, 이들 시스템의 환경 설정은 농업인이 현장에서 버섯의 상태를 확인 한 후 그때그때 경험에 의해 채득한 정보를 기반으로 환경설정을 하고 있는 실정이다. 이렇다 보니 버섯을 재배하는 기간에는 농업인이 재배사 내부의 환경을 관리하기 위해서 항상 버섯재배사에 머물러야 하고, 재배사의 환경관리 때문에 원거리 또는 장기 출타가 어려운 실정이다. 본 연구에서는 기존에 사람이 버섯재배 현장에서 컨트롤하던 환경관리를 원격에서 컴퓨터 또는 모바일로 구현할 수 있는 시스템을 개발하였다. 시스템에서 모니터링 및 제어하는 환경은 온도, 습도, 이산화탄소, 배기팬 및 입기팬의 가동 등 버섯재배 환경관리에 필요한 모든 요소를 모니터링 및 관리할 수 있도록 하였다. 이들 관리 요소는 인터넷이 연결된 컴퓨터에 접속하여 버섯재배사의 환경을 실시간으로 모니터링 하고 필요에 따라 제어를 할 수 있도록 하였다. 또한 컴퓨터에서 볼 수 있는 환경을 스마트폰을 통해서도 볼 수 있고 또한 제어할 수 있도록 하였다. 그리고 버섯배지를 입상 한 후부터 수확시기까지의 관리 환경을 데이터베이스로 만들어 농민이 버섯배지를 입상하고 데이터베이스와 연동한 제어가 되도록 설정하면 버섯재배사 내부의 환경은 데이터베이스의 정보를 읽어 들여 버섯의 생육단계에 따라 자동으로 내부환경이 제어되도록 하였다. 또한 농업인이 원격에서 버섯재배사 내부 버섯의 생육상황을 모니터링 할 수 있도록 재배사 상부에 CCD 카메라를 달아 실시간으로 버섯의 생육상활을 모니터링 할 수 있도록 구성하였다. 이와 같은 시스템을 사용하면 버섯재배 경험이 없는 농업인도 경험자와 같은 재배관리가 가능하고 원격에서 재배사 내부환경을 모니터링하고 제어 할 수 있기 때문에 농업인이 재배사에 매여 있지않아도 될 것으로 판단된다.

• Journal of Advanced Marine Engineering and Technology
• /
• v.34 no.1
• /
• pp.69-75
• /
• 2010

A model ship equipped with the Weis-Fogh type ship's propulsion mechanism, which is consisted of one wing in a squared channel, was constructed. Sailing and vibration tests of the model ship were performed with the opening angles in a pool. The results are summarized as follows. The thrust and the speed of model ship were the highest for the spring-type wing of which the opening angle is automatically controlled in one stroke. Moreover, these values were approximately reduced by 4% from $30^{\circ}$ opening angle to $15^{\circ}$ in order. The maximum amplitude and RMS values of the model ship were the lowest for the wing having the opening angle of $30^{\circ}$, but were the largest for spring-type wing. And in case of the same opening angle, these values were lower for the ship on sailing than that on stationary.

• Journal of the Korean Institute of Telematics and Electronics C
• /
• v.36C no.7
• /
• pp.10-16
• /
• 1999

This paper describes a low voltage swing bus driver using FCSR(Feedback Control Swing voltage Reduction) which can control bus swing voltage within a few hundred of mV. It is proposed to reduce power consumption in On-chip interface, especially for MDL(Merged DRAM Logic) architecture wihich has wide and large capacitance bus. FCSR operates on differential signal dual-line bus and on precharged bus with block controlling fuction. We modeled driver and bus to scale driver size automatically when bus environment is variant. We also modeled coupling capacitance noise(crosstalk) of neighborhood lines which operate on odd mode with parallel current source to analysis crosstalk effect in the victim-line according as voltage transition in the aggressor-line and environment in the victim-line. We built a test chip which was designed to swing 600mV in bus, shows 70Mhz operation at 3.3V, using Hyundai 0.8um CMOS technology. FCSR operate with 250Mhz at 3.3V by Hspice simulation.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.41 no.3
• /
• pp.217-225
• /
• 2013

Typical quadrotor aircraft use four differential thrust vectors to control the motion. In this study, we design a quadrotor aircraft using collective and cyclic control to improve the shortcomings of existing quadrotor aircraft. The quadrotor aircraft with cyclic control can fly at various attitudes due to the excessive control degrees of freedom. Hence the quadrotor aircraft with cyclic control is suitable as high performance aircraft. In this study, modeling and stability analysis of the quadrotor aircraft have been performed using FLIGHTLAB. LQR control systems were designed using linear models at various flight conditions and verified through nonlinear simulations using MATLAB.

• Korean Journal of Food Science and Technology
• /
• v.22 no.4
• /
• pp.479-485
• /
• 1990

For the automation of a evaporation process, computer based evaporation system was built and applied to acquisition of the process variables with an centrifugal thin film evaporator(Centri-Therm, CT-1B). Controls of the process conditions were performed by computer system for pressure, feeding rate, steam, evaporation temperature and flow rate of cooling water. The data acquisitions were also performed by computer system for the changes in the concentration and temperature readings for steam, evaporation and cooling water at the both inlet and outlet. The control and the acquisition variables were collected through the interface device and analyzed by programs using the PASCAL language. To control the feeding rate during the concentration process, inverter was used. The cooling water for the vapor condensation was controlled by the valve controller and should be supplied with the flow rate of 125 kg/h. The maximum vapor condensation rate was 41.7kg/h at the feeding rate of 125 kg/h.

• Journal of Korea Multimedia Society
• /
• v.13 no.4
• /
• pp.526-534
• /
• 2010

This paper describes an algorithm which merges two HDR pictures taken under different exposure time to display on the LDR devices such as LCD or CRT. The proposed method does not generate the radiance map, but directly merges using the weights computed from the input images. The weights are firstly produced on the pixel basis, and then blended with a Gaussian function. This process prevents some possible sparkle noises caused by radical change of the weights and contributes to smooth connection between 2 image informations. The chrominance informations of the images are merged on the weighted averaging scheme using the deviations of RGB average and their differences. The algorithm is characterized by the feature that it represents well the unsaturated area of 2 original images and the connection of the image information is smooth. The proposed method uses only 2 input images and automatically tunes the whole internal process according to them, thus autonomous operation is possible when it is included in HDR cameras which use double shuttering scheme or double sensor cells.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.46 no.7
• /
• pp.583-591
• /
• 2018

In this paper, we propose a new deployment test equipment that is characterized for the deployment test of single large solar panel with tape spring hinge. To perform the deployment test on ground, a device that takes gravity compensation into account should be used to create a zero gravity environment similar to that in orbit. We analyzed the advantages and disadvantages of the most commonly used deployment test equipment in the past through simple conceptual design, analysis, and tests to judge whether it is applicable to the deployment of the solar panel to be tested. A dummy frame was proposed to reduce the air drag effect during on-ground test and a self-aligning ball bearing and adjusting screws were applied to the deployment test equipment to solve the alignment problem with the gravity axis. And a horizontal bearing for radial movement applied to compensate for the change of the axis of the tape spring hinge. From these, we solved the problems of the conventional deployment test equipment by developing and verifying the new deployment test equipment characterized for the solar panel to be deployed in this paper.