• 한국군사과학기술학회지
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• 제14권3호
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• pp.405-413
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• 2011

Defense Systems Test Center in ADD supports increasingly various missile test requirements such as higher altitude event, multi target operation and low-altitude, high velocity target tracking. In this paper, we have proposed the development of instrumentation radar tracking status simulator based on virtual reality. This simulator can predict the tracking status and risk of failure using several modeling algorithms. It consists of target model, radar model, environment model and several algorithms includes the multipath interference effects. Simulation results show that the predict tracking status and signal are similar to the test results of the live flight test. This simulator predicts and analyze all of the status and critical parameters such as the optimal site location, servo response, optimal flight trajectory, LOS(Line of Sight). This simulator provides the mission plan with a powerful M&S tool to rehearse and analyze instrumentation tracking radar measurement plan for live flight test at DSTC(Defense Systems Test Center).

• 한국산학기술학회논문지
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• 제21권10호
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• pp.541-546
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• 2020

함정용 탐색레이더는 표적 탐지 및 추적, 함포사격 지원 기능을 수행하는 함정 전투체계의 장비로써 표적에 대한 방위, 거리, 고도의 3차원 항적 정보를 산출하고 표적 탐지 및 추적에 대한 임무를 수행한다. 탐색레이더는 안테나부, 송수신부, 처리부, 공기건조기부로 구성되며 안테나부는 송신 신호를 방사하고 표적에서 반사된 신호를 수신하며 송수신부는 신호를 증폭 또는 합성하는 역할을 수행한다. 탐색레이더는 안테나로부터 수신된 신호를 이용하여 운용자에게 다양한 방법으로 표적 정보를 제공한다. 본 연구에서는 탐색레이더에서 식별한 표적에 대한 정보를 레이더전시기를 통해 전시할 때 나타난 문제점들을 식별하고 원인을 분석하여 개선하였다. 식별된 문제점은 함정의 변침에 따라 B-scope에 나타나는 TWS 추적 표적이 소실되는 현상이다. 탐색레이더의 TWS 추적 알고리즘에 의해 함정의 기동과 관계없이 지속적으로 추적해야 할 표적을 소실하는 것이다. TWS 추적 알고리즘에서 매 scan마다 획득된 표적의 거리, 방위, 속도 정보를 자함으로부터의 상대적 위치정보로 활용하지 못하는 문제점을 발견하여 추적 알고리즘에서 안정적으로 표적의 위치정보를 업데이트할 수 있도록 개선하였다. 개선된 TWS 추적 알고리즘을 이용하여 탐색레이더 운용에서 정상적 표적 추적 전시상태를 확인하였다.

• 반도체디스플레이기술학회지
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• 제12권2호
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• pp.85-91
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• 2013

In this paper, the parabolic antenna aims to the precise location of a moving ship or car that can be designed system using the gyro sensor. The parabolic antenna has controlled by stepping motor that is a lot of noise and slow response of speed. It has solved the problem which is noise and slow response using the BLDC motor. Also, in order to suppress the noise two-axis control and a separate encoder to the six degrees of freedom motion system was implemented in a precise location. Generally, the gyro sensor is not required to system that doesn't move the six degrees of freedom motion system. But the system will be applied to the moving such as ships or cars. Finally, we presented the position control algorithm at the sometimes controlled both gyro sensor and BLDC motor. This system was tracking that the location of the antenna to the desired angle and errors almost didn't happen when the system was moved 6 degrees of freedom.

• Journal of Astronomy and Space Sciences
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• 제37권4호
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• pp.237-247
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• 2020

The ground tracking support is a critical factor for the navigation performance of spacecraft orbiting around the Moon. Because of the tracking limit of antennas, only a small number of facilities can support lunar missions. Therefore, case studies for various ground tracking support conditions are needed for lunar missions on the stage of preliminary mission analysis. This study analyzes the ground supporting condition effect on orbit determination (OD) of Korea Pathfinder Lunar Orbiter (KPLO) in the lunar orbit. For the assumption of ground support conditions, daily tracking frequency, cut-off angle for low elevation, tracking measurement accuracy, and tracking failure situations were considered. Two antennas of deep space network (DSN) and Korea Deep Space Antenna (KDSA) are utilized for various tracking conditions configuration. For the investigation of the daily tracking frequency effect, three cases (full support, DSN 4 pass/day and KDSA 4 pass/day, and DSN 2 pass/day and KDSA 2 pass/day) are prepared. For the elevation cut-off angle effect, two situations, which are 5 deg and 10 deg, are assumed. Three cases (0%, 30%, and 50% of degradation) were considered for the tracking measurement accuracy effect. Three cases such as no missing, 1-day KDSA missing, and 2-day KDSA missing are assumed for tracking failure effect. For OD, a sequential estimation algorithm was used, and for the OD performance evaluation, position uncertainty, position differences between true and estimated orbits, and orbit overlap precision according to various ground supporting conditions were investigated. Orbit prediction accuracy variations due to ground tracking conditions were also demonstrated. This study provides a guideline for selecting ground tracking support levels and preparing a backup plan for the KPLO lunar mission phase.

• 한국염색가공학회지
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• 제25권4호
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• pp.287-291
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• 2013

Nowadays, terms such as 'Smart Textile', 'Intelligent Textile' and 'Wearable Computing' are commonly used in everyday contexts. And radio-frequency identification (RFID) is the use of a wireless non-contact system that uses radio-frequency electromagnetic fields to transfer data from a tag attached to an object, for the purposes of automatic identification and tracking. These products are required technologies which are textile treatments, printing, ink, etc. Durability of textile substrates is an essential marker for conductive ink printing process. Especially, heat stability is important, since conductive ink should be processable (annealing, curing) at temperatures below $150^{\circ}C$. This study was application of RFID on textiles. The textile pre-treatment processes should be carried out to use RFID antenna on textiles.

• 대한전기학회논문지:전력기술부문A
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• 제48권7호
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• pp.903-908
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• 1999

In this paper, it is proposed the phase shifter array active system to receive digital satellite broadcasting for vehicle. To receive satellite broadcasting data in vehicle, it is inevitable to have active antenna system, which traces the satellite in real time. Also if it is used in vehicle, it must be thin and light structure. To develop this type of antenna system, several techniques should be integrated properly. These are the design and manufacturing technique of high gain antenna, algorithm for tracking satellite and its manufacturing technique, controller design and manufacturing technique, system integration technique and so on. The validity of the proposed AVDBS system was confirmed by simulation and experimental results.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제5권1호
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• pp.191-210
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• 2011

Topology management, which includes neighbor discovery, tracking and updating, is a key area that need to be dealt with appropriately to increase network performance. The use of directional antenna in Wireless Mesh Networks is beneficial in constructing backbone networks viewing the properties of directional antenna. The backbone links must be robust to obtain better network performance. In this paper, a simple yet effective topology protocol is presented that performs well compared to its predecessors. Our protocol constructs the topology with the constraints in the number of links per node. The full topology is constructed in two phases. The resultant topology is termed as Web-topology. The topology formed is robust, efficient, and scalable.

• 한국전자통신학회논문지
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• 제11권2호
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• pp.145-150
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• 2016

자율주행 차량 구현에 있어 차량의 위치에 대한 정확한 정보가 실시간으로 제공되어야 한다. 이동기준국 차분 측위 기술은 차량에 복수의 안테나에서 수신한 신호의 위상차를 통해 정밀 측위 정보를 생성하는 기술로, 이를 위해 차량의 평평하고 넓은 루프를 접지면으로 하는 이중대역 및 이중 원형편파 안테나 개발이 필수적이다. 본 논문에서 제안하는 안테나는 GPS L1과 L2 주파수 대역에서 공진을 일으키는 이중대역 안테나로써, 기존 안테나와 달리 급전부가 안테나 측면에 위치하여 복수의 안테나를 필요로 하는 시스템에 적합하다. 안테나 설계안은 중요 파라미터들의 이론값을 토대로 모델링한 초기 모델을 3D 전파시뮬레이션 소프트웨어를 이용해 최적화하는 방법으로 도출하였다. 최적화된 안테나의 시뮬레이션값과 측정값을 분석한 결과, L1과 L2에서 대역폭 6.1%와 3.7%, 축비 1% 이상임을 확인하였다. 안테나 크기는 $73mm{\times}73mm{\times}6.4mm$로 소형 구조의 장점을 갖췄다.

• 한국산학기술학회논문지
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• 제10권9호
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• pp.2274-2279
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• 2009

본 논문에서는 다중경로에 의한 추적레이더의 추적 오차를 분석하였다. 기존에 소개된 저고도 추적 레이더의 연구내용을 분석 하였고 이를 바탕으로 Matlab을 이용한 추적오차 계산용 수치해석 프로그램을 개발하였다. 본 연구에서는 고도 오차를 계산 할 때 안테나 빔 폭과 지면의 반사계수를 고려하여 좀 더 정밀한 오차 계산방법을 제시 하였다. 제시된 시뮬레이션 결과들이 이론적인 예측 결과와 잘 일치함을 볼 수 있다.

• Journal of Astronomy and Space Sciences
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• 제22권3호
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• pp.243-248
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• 2005

NORAD Two Line Element (TLE) is very useful to simplify the ground station antenna pointing and mission operations. When a satellite operations facility has the capability to determine NORAD type TLE which is independent of NORAD, it is important to analyze the applicable tracking data arcs for obtaining the best possible orbit. The applicable tracking data arcs for NORAD independent TLE orbit determination of the KOMPSAT-1 using GPS navigation solutions was analyzed for the best possible orbit determination and propagation results. Data spans of the GPS navigation solutions from 1 day to 5 days were used for TLE orbit determination and the results were used as Initial orbit for SGP4 orbit propagation. The operational orbit determination results using KOMPSAT-1 Mission Analysis and Planning System(MAPS) were used as references for the comparisons. The best-matched orbit determination was obtained when 3 days of GPS navigation solutions were used. The resulting 4 days of orbit propagation results were within 2 km of the KOMPSAI-1 MAPS results.