• Title/Summary/Keyword: 계기착륙시스템

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Receiving System Design of ILS Navigation Signal Using SDR (SDR을 이용한 ILS 항행신호 수신 시스템 설계)

  • Minsung Kim;Ji-hye Kang;Kyung Heon Koo;Kyung-Soon Lee
    • Journal of Advanced Navigation Technology
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    • v.28 no.3
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    • pp.254-261
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    • 2024
  • Accurate guidance during landing and take-off is important, and instrument landing system (ILS) has been used for stability and verification. Regular inspections are conducted for stable operation, and there is research to perform inspection using drones in addition to ground vehicles and measurement aircraft. Using SDR and single board computer, which can receive wide frequency range, we designed a small system that receives and processes localizer signals through GNU Radio. To check signal processing characteristics through GNU Radio, we simulated with MATLAB Simulink and confirmed the theoretical values. Difference in depth of modulation (DDM) and approach angle can be calculated when the aircraft enters the runway. And GNU Radio implemented real-time signal processing wirelessly using transmission control protocol (TCP). This gives the results within the error of 0.5% when the aircraft entered the runway center line and 0.27% for the angle of 1° degree. Compared to the inspecting and maintaining ILS signals using aircraft or ground vehicles, it is possible to implement a receiving system using small SDR that can be mounted for drone.

The Digital Redundancy Design for Back-up Mode Operation of Aviation Intercom (항공용 인터콤의 백업 모드 운용을 위한 디지털 방식의 이중화 설계)

  • Jeong, Seong-jae;Cho, Kyung-hak;Kim, Dong-hyouk;Lee, Seong-woo
    • Journal of Advanced Navigation Technology
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    • v.26 no.5
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    • pp.358-364
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    • 2022
  • The Inter Communication System for avionics is in charge of processing all voice signals that internal calls between Pilot and Co-pilot, internal calls between Pilots and Crews, external calls through communication equipment such as Ultra/Very High Frequency Receiver/Transmitter(U/VHF RT), audio signal monitoring for navigation and mission equipment such as VHF Omnidirectional Range/Instrument Landing System(VOR/ILS), Tactical Air Navigation(TACAN), audio signal output for voice recording to Flight Data Recorder(FDR) and Data Transfer System(DTS), and warning/caution audio signal generate about the status and threat of aircraft. Because Inter Communication System for avionics is sensitive to noise in the case of analog audio signals, a redundant design that can protect audio signal from electromagnetic noise inside/outside of aircraft is required for the mission of pilots and crews. In this paper, Normal/Back-up operation mode and redundancy design plan based on digital method for the redundancy of the digital Inter Communication System for avionics and manufacturing, verification results are described.