• 수산해양기술연구
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• 제30권3호
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• pp.182-188
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• 1994

In recent years, navigational and fisheries instruments are rapidly advancing. Especially data processing. data transferring and data interchange throughout the digital signals has been in high progress. Even though the ship's heading is also provided by a gyro-compass, an electro-magnetic compass studying by us currently is easy to issue adequate data to instruments requiring the information for the ship's heading. especially in small fishing boats. As the main element of the electro-magnetic compass is a three-axis magnetic sensors, the developing of the high performance sensor is in highly necessity in the beginning. This paper describes on the development of electro-magnetic compass of three-axis fixed type by using three-axis detection new type magnetic sensor without gimbals. even though usual electro-magnetic compass have to need necessarily a gimbal system in order to keep horizontal condition of the compass.

• 한국항공우주학회지
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• 제32권9호
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• pp.35-40
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• 2004

본 연구에서는 최적화된 스커트 형상을 설계하기 위한 기초 자료를 얻기 위하여 스커트 의 확산각 및 길이 변화에 따른 노즐의 공력하중 특성을 고속 풍동시험을 통하여 조사하였다. 적절한 스커트를 사용하면 없을 때에 비해 김발의 구동력을 1/10 수준까지도 줄일 수 있었으며 시험 결과는 추후 스커트 형상 설계 데이터베이스로 활용하기 위해 정규화 하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.110-112
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• 2003

The researchers, who seek geological and environmental information, depend on the remote sensing and aerial photographic datum from various commercial satellites and aircraft. However, the adverse weather conditions and the expensive equipment can restrict that the researcher can collect their data anywhere and any time. To allow for better flexibility, we have developed a compact, a multispectral automatic Aerial photographic system. This system's Multi-spectral camera can catch the visible (RGB) and infrared (NIR) bands (3032${\ast}$2008 pixel) image. Our system consists of a thermal infrared camera and automatic balance control, and it managed and controlled by a palm-top computer. And it includes a camera gimbals system, GPS receiver, weather sensor and etc. As a result, we have successfully tested its ability to acquire aerial photography, weather data, as well as GPS data, making it a very flexible tool for environmental data monitoring.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2004년도 추계학술대회논문집
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• pp.337-340
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• 2004

Stabilizing systems with Gyroscope are extensively used in various tracking devices for attaining the system's objective. Because of putting performance first in importance of system and focusing on specification of parts, designers are sometimes passing over the dynamic characteristics of system in vibrating condition. In this paper, we were dealing with unstable stabilizing control due to coincidence of stabilization platform natural frequency and that of Gyroscope used for sensing rate. For solving this problem, statics and dynamic test of silicon rubber with 3 different hardness were performed and similar stabilizing system was adopted to prove reasonability of rubber choice and static pre-strain.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2009년도 춘계학술대회
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• pp.615-618
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• 2009

2-axis Pan-Tilt의 개발을 위하여 선박용 PAN/TILT의 운동특성 측정 및 분석, 구조설계,제작 및 Test의 순서를 거쳐 최적설계와 제작을 수행한 연구결과로서 나노드라이빙정밀용으로 성능을 보여준다.

• 항공우주기술
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• 제13권2호
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• pp.18-28
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• 2014

네 개의 반작용휠이 장착된 위성에 두 개의 우주검증용 제어모멘트자이로가 탑재되었다고 가정하고, 이들을 이용한 위성 고기동 방법에 대해서 연구해 보았다. 토크가 큰 제어모멘트자이로를 먼저 사용하여 위성의 자세오차를 줄인 후에, 반작용휠을 통해 나머지 자세오차를 제어하는 방법을 제안하였다. 본 방법을 사용할 경우, 제어모멘트자이로에서 발생하는 특이점 문제를 회피할 수 있으며, 토크 명령 계산시 김벌각 정보가 필요 없다는 장점이 있다. 또한 시뮬레이션을 통해, 본 방법이 기존에 연구된 방법들에 비해 위성의 기동성능에는 큰 차이가 없으며, 필요한 반작용휠의 모멘텀도 크게 줄어드는 것을 확인하였다.

• 대한기계학회논문집
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• 제15권2호
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• pp.497-506
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• 1991

In this paper, a new construction for training simulator of R/C helicopter based on two types of servo controller is proposed. Two modified algorithms (algorithm I and II) for servo controller design are presented. Algorithm I is developed by adopting Davison's method in the case that the expressions for the homogeneous differential equations of reference input and disturbance are different types, and algorithm II is done by considering error weighting function for the servo controller of algorithm I . The linear fractional transformation method is incorporated in both design methods in order to assign the closed loop poles of the servo system in a specified region. The helicopter simulator is composed by the gimbals with two freedom of rolling and pitching. The reliability and validity for the design methods of the proposed servo controller are investigated through the practical experiment for the simulator by using 16bits micro-computer with A/D and D/A converters. It can be observered from the experimental results that the proposed servo controller is applicable to practical plants since the simulator is robust for the arbitrary disturbance and it follows to the given reference input without significant steady state error.

• 한국정보통신학회논문지
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• 제7권6호
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• pp.1146-1152
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• 2003

선박이나 자동차 등의 이동체에서, 이동중에 위성 TV를 볼 수 있도록 하기 위해서는 이동체용 TV 위성 수신안테나 개발이 요구된다. 현대사회에서 TV가 갖고 있는 정보는 정보 수집을 위한 매체로서의 기능뿐만 아니라, 이미 우리생활의 일부가 되어 있다. 특히 한국에서는 무궁화위성을 이용한 다채널위성방송이 시작되어 화질과 음질에서 뛰어난 프로그램을 제공하고 있어 위성을 이용한 TV수신은 이미 대중화되기 시작하였다. 본 연구에서는 수평추적은 자이로센서를 이용한 방위정보와 수신신호 강도를 측정 비교하는 하이브리드형 추적알고리즘을 사용하였고, 수직방향추적은 짐발(무게추)을 이용한 선박용 위성 TV 수신안테나 시스템을 개발하였다. 본 연구의 결과로서 소형으로서 경제적인 가격의 27dBi 평판배열안테나와 선박의 움직임이 롤링, 피칭$\pm$30도까지도 추적이 가능한 추적 알고리즘을 개발하였다.

• 한국정밀공학회지
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• 제31권9호
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• pp.813-820
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• 2014

This paper presents design and performance validation of a method for motion compensation using fast steering mirror. First of all, the schematics of the Electro Optical/Infra-Red (EO/IR) and step-stare image gathering system for an aerial reconnaissance are introduced. Because of the steering mirror with low inertia so called Back scan mechanism (BSM), the fast step-stare image gathering technique that is required for taking a high-definition still image will be realized. After then, the BSM hardware includes motors and feedback sensors are introduced. Also, the motion profile for BSM will be designed to compensate roll scan motion of the gimbals. At the end of this paper, designed profile and tracking performance of the EO/IR system with BSM will be validated through experiments.

• 한국소음진동공학회논문집
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• 제21권10호
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• pp.951-959
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• 2011

In this study, an OTM(on-the-move) antenna which is mounted on ground vehicles and is used for mobile communication between vehicle and satellite while moving was addressed. Since LOS(line-of-sight) of antenna should direct satellite consistently while vehicle moving to guarantee high satellite communication quality, active antenna LOS stabilization is a core technology for OTM antenna. Stabilization of a satellite tracking antenna which consists of 2-DOF gimbals, an elevation gimbal over an azimuth gimbal, was considered in this study. In consideration of driving mechanism which consists of gear train and flexible driving shafts, a two-mass-system dynamic model coupled with vehicle motion was presented. An internal PI-control loop + outer PI-control loop structure has been suggested in order to damp the torsional vibration and stabilize control system. The classical pole-placement method was applied to design control gains. In addition, a vehicle motion compensation control beside of the feedback control loop has been suggested to improve LOS stabilization performances. The feasibility of the proposed control design was verified along with some experimental results.