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

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Suitability of Singularity Indices for Steering Law Design of Control Moment Gyros

제어모멘트자이로의 구동법칙 설계를 위한 특이성 지수의 적합성

  • Received : 2014.08.21
  • Accepted : 2014.11.10
  • Published : 2014.12.01
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Abstract

Singularity indices for steering law design of CMGs have been analyzed. Several qualitative criteria to evaluate the suitability of indices have been suggested. Fast calculation and consistency with the condition number of the input matrix are the most important ones. Based on these criteria, modified indices have been proposed. Properties of infinite value and finite value indices have been compared and an ad hoc method to combine those properties has been presented. Computer simulation results are given to verify the proposed method.

CMG의 특이점 회피를 위한 구동법칙의 설계와 관련된 특이성 지수를 분석하였으며, 지수를 선택하거나 개발할 때 필요한 정성적인 적합성 기준을 제시하였다. 빠른 계산과 조건수와의 일치성을 중요한 기준으로 선정하였으며, 이에 따라 세 가지의 변형된 지수를 제안하였다. 유한지수와 무한지수의 특성을 비교하였고, 가중치를 이용하여 두 가지의 장점을 결합하는 방안을 제시하였다. 컴퓨터 시뮬레이션을 이용하여 제안한 방법을 검증하였다.

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References

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