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

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Nonlinear Observer Design for Satellite Angular Rate Estimation by SDRE Method

SDRE 기법을 이용한 위성 각속도 추정용 비선형 관측기 설계

  • Received : 2014.06.17
  • Accepted : 2014.09.04
  • Published : 2014.10.01
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Abstract

The estimation of the angular rate of a satellite has been discussed. A nonlinear observer has been proposed based on the state-dependent Riccati equation method. A sufficient stability condition for the convergence of estimation error has been presented. This condition is related to a state-dependent algebraic Riccati equation. It has been derived by transforming nonlinear error dynamics into a Lipschitz nonlinearity. An observer gain is obtained from this condition. Numerical simulations are presented to verify the proposed method.

위성의 각속도를 추정하는 비선형 관측기의 설계방법을 제안한다. SDRE 기법을 이용하여 관측기를 설계하는데, 오차 수렴에 대한 충분조건을 제시하였다. 대수 Riccati 형태의 이 조건은, 비선형 항을 Lipschitz 형태로 변환하고 이에 대한 수렴 조건을 유도하여 구해진다. 이 조건으로부터 관측기의 게인을 구할 수 있으며, 시뮬레이션을 이용하여 제안한 방법을 검증하였다.

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References

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