International Journal of Aeronautical and Space Sciences

  • 제11권2호
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  • Pages.80-86
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  • 2010
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Attitude Estimation for Satellite Fault Tolerant System Using Federated Unscented Kalman Filter

  • Bae, Jong-Hee (Department of Mechanical and Aerospace Engineering, Seoul National University) ;
  • Kim, You-Dan (Department of Mechanical and Aerospace Engineering, Seoul National University)
  • 발행 : 2010.06.15
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초록

We propose a spacecraft attitude estimation algorithm using a federated unscented Kalman filter. For nonlinear spacecraft systems, the unscented Kalman filter provides better performance than the extended Kalman filter. Also, the decentralized scheme in the federated configuration makes a robust system because a sensor fault can be easily detected and isolated by the fault detection and isolation algorithm through a sensitivity factor. Using the proposed algorithm, the spacecraft can continuously perform a given mission despite navigation sensor faults. Numerical simulation is performed to verify the performance of the proposed attitude estimation algorithm.

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참고문헌

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피인용 문헌

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