• Title/Summary/Keyword: Gyrocompass Correction

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Gyrocompass Correction and Pointing Accuracy Improvement of the Ship-Borne Mobile Down Range Antenna for Launcher Telemetry (우주발사체 텔레메트리용 해상 이동형 다운레인지 안테나의 자이로컴퍼스 보정과 포인팅 정확도 향상)

  • Lee, Sun-Ik;Yeom, Kyung-Whan
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.25 no.5
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    • pp.532-541
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    • 2014
  • The ship-borne mobile down range telemetry antenna system having 4.6 m reflector antenna and 3-axis mounting structure at S-band requires the precise pointing accuracy at sea for the launch mission. Using the LEO satellites tracking, a method to determine and verify the antenna pointing and tracking performance, and to find the pointing bias which dominantly contributes to the pointing inaccuracy, is presented. Based upon the tests conducted on the Jeju sea and Pacific sea, the pointing bias is determined and its origin is also identified as the drift of the heading angle of the gyrocompass. The applied systematic correction taking into account the pointing bias, and the achieved improvement of the pointing accuracy are shown. Thanks to the correction, it is presented that this antenna tracked the launcher(KSLV-I) stably within the required pointing accuracy in the following KSLV-I third launch.

Implementation of the Azimuth Correction Device using Astronomical Observation (천측을 이용한 방위 보정 장치의 구현)

  • Lim, Jin-Kook;Yim, Jae-Hong
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.21 no.4
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    • pp.846-854
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    • 2017
  • In this paper, we proposed a method to reduce the error of compass by combining the ceiling technique used in the past with modern IT technology. We combined an encoder and the Azimuth Circle for applying an algorithm. The algorithm is able to calculate the true north by using astronomical observation. Finally, we implemented the embedded system possible to indicate various situations and perform calculations. As a result, it isn't only able to calculate the true north with an error of about $0.2^{\circ}$ but also takes less than 5 seconds. Originally, using astronomical observation requires more than 5minutes. So it is analyzed as convenient by solving the problem of taking lots of time. Especially, we present the tolerance less than $0.5^{\circ}$ by the analysis of the existing gyrocompass and the bearing standard of IMO. In conclusion, we clearly confirm that the results of this paper are possible to reduce the error of various compasses in a real world.