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Radio Frequency Interference on the GNSS Receiver due to S-band Signals

S 대역 신호에 의한 위성항법수신기의 RF 신호간섭

  • Kwon, Byung-Moon (KSLV-II R&D Head Office, Korea Aerospace Research Institute) ;
  • Shin, Yong-Sul (KSLV-II R&D Head Office, Korea Aerospace Research Institute) ;
  • Ma, Keun-Su (KSLV-II R&D Head Office, Korea Aerospace Research Institute) ;
  • Ju, Jeong-Gab (Alternative Navigation Division, Navcours Co., Ltd.) ;
  • Ji, Ki-Man (KSLV-II R&D Head Office, Korea Aerospace Research Institute)
  • Received : 2019.03.29
  • Accepted : 2019.04.25
  • Published : 2019.05.01

Abstract

This paper describes the RF(Radio Frequency) interference on the GNSS receiver due to the S-band signals transmitted from the transmitters in the Test Launch Vehicle, and analyzes the cause of the RF interference. Due to the S-band signals that have relatively high power levels compared with GNSS signals, an LNA(Low Noise Amplifier) in the active GNSS antenna was saturated, and the intermodulation signal within GNSS in-bands was produced in the LNA whenever two S-band signals were received from the GNSS antenna. For these reasons, the C/N0 of the satellite signals in the GNSS receiver was attenuated severely. The design of the LNA was changed in order to protect the RF interference due to the S-band signals and the suppression capability of the RF interference was confirmed in the new LNA through the comparison of the old LNA.

본 논문은 시험발사체에 탑재된 송신기에서 송신되는 S 대역 신호에 의해 위성항법수신기에서 나타난 RF 신호간섭을 설명하고, 그 원인을 분석한다. 능동형 위성항법안테나의 LNA는 항법위성 신호와 비교하여 상대적으로 신호세기가 매우 높은 S 대역 신호에 의해 포화되었으며, 2개의 S 대역 신호가 위성항법안테나에 수신될 때마다 GNSS 대역에 해당하는 상호변조신호가 LNA에서 발생하였다. 이러한 현상으로 인해 위성항법수신기에서 계산된 항법위성신호의 C/N0가 크게 감쇄하였다. S 대역 신호에 의한 RF 신호간섭을 차단하기 위하여 위성항법안테나 LNA의 설계변경을 수행하였고, 설계변경 전 후의 LNA에 대해 수행한 비교시험을 통하여 설계변경된 LNA에서 S 대역 신호에 의한 RF 신호감쇄 현상이 억제될 수 있음을 확인하였다.

Keywords

References

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