• Title/Summary/Keyword: Antenna Tracking System

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A Study on the Tracking Antenna System for Satellite Communication Using Embedded Controller

  • Kim, Jong-Kwon;Cho, Kyeum-Rae;Lee, Dae-Woo;Jang, Cheol-Soon
    • 제어로봇시스템학회:학술대회논문집
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    • 2004.08a
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    • pp.413-416
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    • 2004
  • The tracking antenna system must be always pointed to a satellite for data link among moving vehicles. Especially, for an antenna mounted on a moving vehicle, it needs the stabilized the antenna system. So, software and hardware, signal processing of motion detection sensors, real-time processing of vehicle dynamics, trajectory estimation of satellite, antenna servo mechanism, and tracking algorithm, are unified in the antenna system. The purpose of this paper is to design the embedded tracking antenna control system for satellite communication. The embedded OS(Operating System) based stabilization and tracking algorithm was implemented. The performance of the designed embedded control system was verified by the real satellite communication test.

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An Improvement of Performance in a Satellite Antenna Tracking Control System for Mobile DAB Reception (DAB수신을 위한 이동체용 위성 안테나 트랙킹 시스템의 성능 개선)

  • Jeong Joong-Sung
    • Journal of Advanced Marine Engineering and Technology
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    • v.28 no.7
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    • pp.1178-1184
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    • 2004
  • This paper presents the development of a satellite antenna tracking control system using a plane antenna for mobile DAB(Digital Audio Broadcasting) reception. To track more rapidly in the antenna of this system, this simple tracking system only tracks a direction of azimuth using pendulum in the direction of elevation. This system should track using the AGC(Automatic Gain Control) of the signal level which can receive DAB in spite of the changing of point and movement of the mobile. The directional gyro sensor is attached to solve the delay time in the Proposed tracking algorithm. The effectiveness of both the stabilization and tracking algorithm is demonstrated through experiment measuring AGC signal level. The implemented satellite antenna tracking control system is shown to be excellent for mobile DAB reception.

A Study on the Validation of Tracking Performance of a Big Parabola Antenna System (대형 접시형 안테나 추적성능 검증에 관한 연구)

  • Oh, Chang-Yul;Oh, Seung-Hyeub
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.10 no.5
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    • pp.77-82
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    • 2010
  • The tracking performance of the big tracking antenna system using Radio Frequency is very important for the tracking and position measuring for the flight vehicle, but the precise measuring of the tracking performance is not easy, especially for the big antenna system such as ground telemetry antenna or tracking radar in space application because it's characteristics could be different in accordance with the antenna direction. In this paper, the error factors impacting on the tracking performance (pointing accuracy and tracking accuracy) and the ranges of each factor are reviewed, and the simple and efficient method to measure the tracking performance is introduced which using low earth orbit as the signal source. Finally, the measurement results for the telemetry ground antenna in NARO Space Center are reviewed.

A study on the tracking algorithm of satellite antenna system (위성 안테나 시스템의 추적 알고리즘에 관한 연구)

  • 강우신;조창호;이상철;조도현;이상효
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.128-128
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    • 2000
  • An antenna tracking technique, referred to as "step track", is commonly used in communication applications. In this paper, an algorithm to improve the step-tracking technique for satellite tracking is proposed. We suggest a method by which the antenna scans the azimuth, detects the satellite signal without the position information, and points quickly to the direction receiving the signal of peak level. After reaching the peak level, the step-track system maintains enough signal levels to receive satellite broadcasting normally. Performance of the Tracking Algorithm proposed in this paper are verified with simulation.

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Antenna Alignment Method for Low Angular Error of 3-axis Tracking System

  • Lee, Jeom Hun;Kim, Young Wan;Kim, Nae Soo;Lee, Ho Jin
    • International Journal of Aeronautical and Space Sciences
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    • v.2 no.1
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    • pp.44-54
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    • 2001
  • This paper describes the antenna alignment method of the tracking antenna system for LEO satellite. The purpose of the antenna alignment is to reduce the angular error due to the structural alignment and the monopulse null point alignment error. The angular error of 3 axis tracking system is the key performance parameter that should be minimized to accurately track satellite movement. The angular error is analyzed via a simulation and boresight measurement. The simulation is done with formulas to be derived from vector concept for 3-axis movement. The formulas of the structural alignment are verified by comparing the formula result with the field measurement. Also, the angular error due to monopulse null shift is obtained via boresight measurement. Based on the analyzed and measured results, the antenna alignment was performed and was verified via tracking test of operating LEO satellite.

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Fuzzy Control of Data Link Antenna Control System for Moving Vehicles

  • Kim, Jong-Kwon;Cho, Kyeum-Rae;Jang, Cheol-Soon
    • 제어로봇시스템학회:학술대회논문집
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    • 2005.06a
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    • pp.525-528
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    • 2005
  • The tracking antenna system must be always pointed to target moving vehicle. Especially, for an antenna mounted on a movable vehicle, it needs the stabilized antenna system. In this paper, two types of fuzzy controller were derived and applied to a data link antenna system and the altitude control of unmanned helicopter, respectively. A simplified Fuzzy-PID controller was designed for 2-axes antenna stabilization and tracking system and the performance was verified by simulations and experiments. Computer simulations were performed by Matlab and SIMULINK. A 2-Axes antenna (SeaTel 1898 model) was selected as test platform of this research. The antenna was modified by using two Blushless Direct Current motors and an embedded DSP controller. To verify the performance of designed antenna servo control system, the performance of the conventional PID controller and that of the Fuzzy-PID controller, designed by the same PID control gains, were compared.

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Introduction of Satellite Antenna Tracking System in Field (기술사마당_기술자료 - 위성안테나 추적기술의 소개와 실용)

  • Kim, Chang-Yong
    • Journal of the Korean Professional Engineers Association
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    • v.42 no.6
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    • pp.53-57
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    • 2009
  • Antenna Tracking System has been required core technology with special tracking algorithm, and it can be achieved by program tracking, step tracking, optracking, and monopulse tracking as well. Depend on tracking requirement we might be able to apply eligible tracking method in accordance with Geostationary and Inclined Orbit Satellite. Further, we should deeply consider two important factors in order to act up to customer expectation in quality and system performance including competitive price therefore we need maximized endeavor to upgrade not only tracking system performance, but reduction of product through engineering skill and R&D investment.

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Antenna Control System Using Step Tracking Algorithm with H$_{\infty}$ Controller

  • Cho, Chang-Ho;Lee, Sang-Hyo;Kwon, Tae-Yong;Lee, Cheol
    • International Journal of Control, Automation, and Systems
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    • v.1 no.1
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    • pp.83-92
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    • 2003
  • The outdoor antenna servo system is subject to has significant torque disturbances from wind pressures and gusts on the antenna structures, as well as bearing and aerodynamic frictions. This control system should provide a sharp directivity in spite of the environmental disturbances and internal uncertainties. Therefore, the implementation of a real-time controller is necessary for the precise generation of the reference signal and robust tracking performance. In this paper, the discrete-time controller for the quick tracking of a target communication satellite is designed by applying the sampled-data $H_{\infty}$ control theory along with the reference signal generated by an improved conventional step-tracking algorithm. The sampled-data $H_{\infty}$controller demonstrates superior robustness for the longer sampling period when compared with a simple PID controller.

Implementation of GCS and Antenna Tracking System for UAV (UAV용 GCS 및 안테나 추적 시스템 구현)

  • Park, Bumsoon;Choi, Ilgue;Kim, Jichul;Cheon, Dongik;Lee, Sangchul;Oh, Hwa-Suk;Kang, Minyoung
    • Journal of Aerospace System Engineering
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    • v.3 no.4
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    • pp.35-40
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    • 2009
  • The first purpose of this study is to develop a GCS(Ground Control System) by using RF(Radio Frequency) wireless communication equipments for UAV(Unmanned Aerial Vehicle). The second goal is to develop an antenna tracking system operating automatically. UAV receives flight data from a RF wireless system. So the role of antenna tracking system is very important to keep good communication state between UAV and GCS. GCS can check flight data and display a aviation state of UAV in real-time. The flight data displayed in real-time by GCS include the latitude, longitude, altitude, speed and so on. Experiments that measure a communication range and reliability are needed to develop a RF wireless communication system.

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Performance of a Satellite Tracking Antenna Control System for Mobile DBS Reception (차량용 DBS 수신을 위한 위성 추적 안테나 제어시스템의 성능 구현)

  • Kim, Dong-Cheol;Min, Gyeong-Sik;Arai, Hiroyuki
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.39 no.4
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    • pp.216-224
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    • 2002
  • This paper describes a performance of a satellite tracking antenna control system for mobile DBS reception. In order to improve the tracking speed and the stability of this system, a directional sensor function is added to a conventional left-right tracking algorithm. The satellite tracking experiments of the fabricated antenna system for the DBS reception were performed at a highway and an urban area. The measured AGC signal level on the highway was observed above the level to watch television. Therefore, an excellent performance of the hardware system with the tracking algorithm compensated for the directional sensor was confirmed.