In orbit Estimation of Satellite inertial matrix using STLS

Abstract

Abstract: Dynamics equations of inertial matrix estimation were deduced. The structured total least norm (STLN) algorithm was used to estimate the parameters. Theoretical analysis shows that the STLS solution is maximum likelihood estimate when the sensor noise is Gaussian. This method has two advantages over existing methods: sensor noise is considered and the consistency of the estimate is proved.

Key words: Structured total least squares, Structured total least norm, Maximum likelihood estimate, Consistent estimate, Inertial matrix, In orbit estimation, Satellite attitude control

LIN Jia-Wei, WANG Ping. In orbit Estimation of Satellite inertial matrix using STLS[J]. , 2010, 30(6): 31-38.

References

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