Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Design of Variable Data Transfer Rate Asymmetric TDD System Using Turbo Decoder with Double Buffer Controller

이중 버퍼 제어기 구조의 터보 복호기를 사용한 전송률 가변 비대칭 TDD 시스템 설계

  • Received : 2018.10.02
  • Accepted : 2018.12.28
  • Published : 2019.02.01
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Abstract

This paper proposes a variable data transfer asymmetric TDD(Time Division Duplex) system for small UAV(Unmanned Aerial Vehicle) data link system. In the proposed method, a turbo decoder with a double buffer controller is proposed to apply turbo decoder with long decoding time to asymmetric TDD system. The proposed method achieves variable data transfer rate and maximum data transfer rate. The advantage of the proposed method is demonstrated by its data transfer rate. The measured data transfer rate is more than 1.8 times than that of symmetric TDD system. In addition, PER(Packet Error Rate) performance is the same and data transfer rate is variable.

본 논문에서는 소형 무인기 데이터 링크 시스템에 적용이 가능한 전송률 가변 비대칭 TDD(Time Division Duplex) 방식에 대해 다루었다. 긴 복호 시간이 필요한 터보 복호기를 비대칭 TDD 방식에 적용하기 위하여 이중 버퍼 제어기 구조의 터보 복호기를 제안하였다. 제안 방법은 전송률 가변과 동일 송수신 시간에 최대의 데이터 전송이 가능하다. 제안 방식을 적용한 데이터 링크 시스템을 제작하여 성능을 확인하였다. 측정 결과, 대칭 TDD 방식에 비해 전송률은 최대 약 1.8배 증가하였다. PER(Packet Error Rate) 성능은 동일하며, 전송률 가변이 가능함을 확인하였다.

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References

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