International Journal of Aeronautical and Space Sciences

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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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)
  • Published : 2010.06.15
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Abstract

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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References

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