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

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Development of a Test System for a Hemispherical Resonator and Control of Vibrating Pattern

반구형공진기 실험장치 개발과 진동패턴 제어

  • Received : 2013.05.02
  • Accepted : 2013.09.09
  • Published : 2013.10.01
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Abstract

The authors have developed a test system for a hemispherical resonator gyroscope by using NI FPGA equipment. We have verified its suitability for the research of resonator gyroscopes through several tests: deriving resonance, controlling amplitudes, and estimating resonator parameters. The authors have adjusted a vibrating pattern to be aligned with the driving axis (or electromagnets). This pattern alignment is a basic and important operation of the FTR mode, which is one of operating modes for resonant gyroscopes.

본 논문에서는 반구형 공진자이로에 대한 연구를 위해 NI FPGA 장비를 기반으로 한 실험 장치를 개발하였고 공진유도, 진폭제어 및 회전실험을 통해 실험 장치에 대한 적합성을 판별하고 시스템에 대한 파라미터를 추정하였다. 또한 공진기의 형상 불 균일로 인해 진동패턴이 표류하는 현상을 확인하고, 이를 정렬시킴으로써 구동모드중 하나인 FTR 모드 구현에 대한 선행연구를 수행하였다.

Keywords

References

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Cited by

  1. Force-To-Rebalance Mode of a Resonator Gyro and Angular Rate Measurement Tests vol.20, pp.5, 2014, https://doi.org/10.5302/J.ICROS.2014.13.1983