• Journal of Communications and Networks
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• 제17권4호
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• pp.419-427
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• 2015

There have been increases in the elderly population worldwide, and this has been accompanied by rapid growth in the health-care market, as there is an ongoing need to monitor the health of individuals. Wireless body area networks (WBANs) consist of wireless sensors attached on or inside the human body to monitor vital health-related problems, e.g., electrocardiograms (ECGs), electroencephalograms (EEGs), and electronystagmograms (ENGs). With WBANs, patients' vital signs are recorded by each sensor and sent to a coordinator. However, because of obstructions by the human body, sensors cannot always send the data to the coordinator, requiring them to transmit at higher power. Therefore, we need to consider the lifetime of the sensors given their required transmit power. In the IEEE 802.15.6 standard, the transmission topology functions as a one-hop star plus one topology. In order to obtain a high throughput, we reduce the transmit power of the sensors and maintain equity for all sensors. We propose the multiple-hop transmission for WBANs based on the IEEE 802.15.6 carrier-sense multiple-access with collision avoidance (CSMA/CA) protocol. We calculate the throughput and variance of the transmit power by performing simulations, and we discuss the results obtained using the proposed theorems.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1994년도 하계학술대회 논문집 A
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• pp.39-42
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• 1994

The application of speed or position control technique in AC drives demands accurate position and velocity feedback information. Generally, resolver and absolute encoders are used as a velocity or position sensor. But they increase cost and when the sampling frequency is faster than sensoer's output frequency we can't Set exact information. In order to solve this problem this thesis proposes a speed and a position observer design for Permanent-Magnet Synchronous Motors(PMSM) specialty in low speed drives. Most literatures on this topic design the observer based on the field_oriented d_q model. But in this thesis, a new approach to machine dynamics is proposed. Since it is difficult to design the observer using the nonlinear model, the machine model is here linearlized at the operating point. The observer designed is implemented by software using Intel's 8097 microprocessor and verifies the proper performance of observer by simulation and experiment.

• 제어로봇시스템학회논문지
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• 제14권3호
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• pp.248-253
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• 2008

This paper presents a sensing system for smart home which can detect an location transition events such as entrance/exit of a member and identify the user in a group at the same time. The proposed system is compose of two sub-systems; a wireless sensor network system and a database server system. The wireless sensing system is designed as a star network where each of sensing modules with ultrasonic sensors and a Bluetooth RF module connect to a central receiver called Bluetooth access point. We propose a method to discriminate a user by measuring the height of the user. The differences in the height of users is a key feature for discrimination. At the same time, the each sensing module can recognize whether the user goes into or out a room by using two ultrasonic sensors. The server subsystem is a sort of data logging system which read the detected event from the access point and then write it into a database system. The database system could provide the location transition information to wide range of context-aware applications for smart home easily and conveniently. We evaluate the developed method with experiments for three subjects in a family with the installation of the developed system into a real house.

• 한국지능시스템학회논문지
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• 제23권2호
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• pp.100-106
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• 2013

본 논문에서는 3개의 바퀴를 취하는 삼각형 구조의 전방향 청소로봇의 설계와 제어에 대해 소개한다. 시뮬레이션과 실험을 통해 제안하는 방법의 동작을 검증한다. 전방향 구조는 어느 방향으로 움직일 수 있다. 천장의 마커를 사용하는 StaGazer 센서를 사용하여 로봇의 위치와 헤딩각을 알아냈다. 추가로 초음파 센서를 부착하여 장애물을 검출할 수 있도록 하였다. 실험을 통해 시스템의 성능을 평가하였다.

• Journal of Astronomy and Space Sciences
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• 제36권3호
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• pp.181-186
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• 2019

The attitude information of spacecraft can be obtained by the sensors attached to it using a star tracker, three-axis magnetometer, three-axis gyroscope, and a global positioning signal receiver. By using these sensors, the spacecraft can be maneuvered by actuators that generate torques. In particular, electromagnetic-torque bars can be used for attitude control and as a momentum-canceling instrument. The spacecraft momentum can be created by the current through the electrical circuits and coils. Thus, the current around the electromagnetic-torque bars is a critical factor for precisely controlling the spacecraft. In connection with these concerns, a solar-cell array can be considered to prevent generation of a magnetic dipole moment because the solar-cell array can introduce a large amount of current through the electrical wires. The maximum value of a magnetic dipole moment that cannot affect precise control is $0.25A{\cdot}m^2$, which takes into account the current that flows through the reaction-wheel assembly and the magnetic-torque current. In this study, we designed a 300-W solar cell array and presented an optimal wire-routing method to minimize the magnetic dipole moment for space applications. We verified our proposed method by simulation.

• 천문학회보
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• 제40권1호
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• pp.54.3-54.3
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• 2015

To probe the star formation in local and early Universe, the NISS with a capability of imaging spectroscopy in the near-infrared is being developed by KASI. The main scientific targets are nearby galaxies, galaxy clusters, star-forming regions and low background regions. The off-axis optical design of the NISS with 15cm aperture was optimized to obtain a wide field of view (FoV) of $2deg.{\times}2deg.$ as well as a wide spectral coverage from 0.9 to $3.8{\mu}m$. The opto-mechanical structure was designed to be safe enough to endure in both the launching condition and the space environment. The dewar will operate $1k{\times}1k$ infrared sensor at 80K stage. The NISS will be launched in 2017 and explore the large areal near-infrared sky up to $200deg.^2$ in order to get both spatial and spectral information for astronomical objects. As an extension of the NISS, KASI is planning to participate in a new small space mission together with NASA. The promising candidate, SPHEREx (Spectro-Photometer for the History of the Universe Epoch of Reionization, and Ices Explorer) is an all-sky survey satellite designed to reveal the origin of the Universe and water in the planetary systems and to explore the evolution of galaxies. Though the survey concept is similar to that of the NISS, the SPHEREx will perform the first near-infrared all-sky imaging spectroscopic survey with the wider spectral range from 0.7 to $5{\mu}m$ and the wider FoV of $3.5deg.{\times}7deg.$ Here, we report the current status of the NISS and introduce new mission for the near-infrared imaging spectroscopic survey.

• Journal of Biosystems Engineering
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• 제36권2호
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• pp.116-121
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• 2011

This study was conducted to develop a robust navigator which could be in positioning for precision farming through developing a plural GPS receiver with 4 sets of GPS antenna. In order to improve positioning accuracy by integrating GPS signals received simultaneously, the algorithm for processing plural GPS signal effectively was designed. Performance of the algorithm was tested using a simulation program and a fixed point on WGS 84 coordinates. Results of this study are aummarized as followings. 1. 4 sets of lower grade GPS receiver and signals were integrated by kalman filter algorithm and geometric algorithm to increase positioning accuracy of the data. 2. Prototype was composed of 4 sets of GPS receiver and INS components. All Star which manufactured by CMC, gyro compass made by KVH, ground speed sensor and integration S/W based on RTOS(Real Time Operating System)were used. 3. Integration algorithm was simulated by developed program which could generate random position error less then 10 m and tested with the prototype at a fixed position. 4. When navigation data was integrated by geometrical correction and kalman filter algorithm, estimated positioning erros were less then 0.6 m and 1.0 m respectively in simulation and fixed position tests.

• 항공우주기술
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• 제11권2호
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• pp.19-25
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• 2012

정지궤도복합위성은 천리안위성에 비하여 고품질의 영상품질을 요구하며 지구센서 대신 별센서의 사용으로 인하여 고정밀의 탑재용 궤도정보생성이 요구된다. 이는 고정밀의 궤도 결정이 바탕이 되어야 한다. 천리안위성의 경우는 항공우주연구원에 설치된 추적 안테나를 이용하여 레인징을 수행하고 이를 바탕으로 궤도결정을 수행하였다. 정지궤도복합위성의 정밀한 궤도결정을 위하여 항공우주연구원에서는 축섬에 새로운 추적장비를 준비중에 있다. 본 논문에서는 대전과 축섬에 위치한 정지궤도복합위성을 가정하여 궤도결정을 수행했을 경우 궤도결정 및 예측 오차와 테이블 방식의 탑재용궤도정보 생성기의 궤도정밀도를 분석하였다. 본 논문에서는 공분산해석과 수치적인 방법을 통하여 궤도정밀도를 해석하였다. 두 해석결과를 종합하여 최종적인 궤도오차를 산출하였다.

• 한국항공우주학회지
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• 제45권9호
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• pp.734-745
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• 2017

달 착륙선의 항법 시스템은 자율 정밀 항법 성능을 확보하기 위해 관성측정기와 별추적기, 고도계, 속도계, 지형상대항법 카메라 등 다양한 항법용 전장부품으로 구성되는데 착륙선의 착륙 시나리오와 임무 요구 성능에 따라 적합한 성능의 항법용 전장부품 선정이 필요하다. 본 논문에서는 달 착륙선에 요구되는 항법용 전장부품의 사양을 공분산해석을 통해 분석하였다. 77차 상태변수로 구성되는 기준 시스템 오차모델과 센서의 측정모델을 정의하고 착륙선의 임무 요구 성능은 90m($3{\sigma}$) 착륙 위치 정확도를 요구하는 정밀탐사 임무와 6km($3{\sigma}$)의 착륙 오차가 허용되는 영역탐사 임무로 구분하였다. 자율항법 시작 시점에 따라 PDI(Powered descent initiation)와 DOI(Deorbit initiation) 시나리오로 나누고 항법용 전장부품의 조합과 착륙 시나리오에 따른 성능 분석을 통해 가상의 임무 요구 성능을 만족하기 위한 항법 시스템의 요구사양을 도출하였다.

• 한국항공우주학회지
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• 제33권3호
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• pp.93-98
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• 2005

과학기술위성2호는 2007년 12월에 발사될 예정이다. 이 위성의 주관측기는 DREAM으로서, 주요 임무는 지구 또는 대기로부터 발생되는 복사에너지를 라디오파 대역에서 관측하는 것이다. 이 외 과학기술위성2호는 과학기술 실험용기기로서 정밀디지탈 태양센서, 2중헤드 별센서 등이 탑재되며, 과학기술위성2호의 자세제어 및 모멘텀 덤핑용 과학기술실험용 탑재체로서 펄스형 플라즈마 추력기가 실린다. 본 논문에서는 관측기기 및 과학기술실험용 탑재체 등의 운용모드를 고려한 과학기술위성2호의 운용모드에 따른 전력의 수요예측에 대하여 연구하였고, 임무를 수행하는 동안 안정적인 전력을 공급하기위한 필요전력에 대하여 분석하였다.