DocumentCode
3044150
Title
Application of Empirical Bayes Estimation in Error Model Identification of Two Orthometric Accelerometers
Author
Jiang, Yansong ; Su, Baoku ; Liu, Yu
Author_Institution
Space Control & Inertial Technol. Res. Center, Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
8-10 June 2010
Firstpage
218
Lastpage
221
Abstract
The high accuracy accelerometer can be demarcated in multiposition tumbling experiment under 1g gravitational field. The g2 observation model of Two Orthometric Accelerometers can eliminate the corner error. there is a serious multicollinearity exit in this system because some model coefficient mix together. In view of above question, this article has given the arithmetic of Empirical Bayes Estimation(EB), and applied this method in model which is mentioned above. The result of the simulation and the experiment shows that compared with the conventional least squares method and the generalized diagonal ridge estimation, the Empirical Bayes Estimation can overcome the influence of the multicollinearity and can separate two coefficients which are The Second-Order Terms and the cross-coupling terms.
Keywords
Bayes methods; accelerometers; least squares approximations; conventional least squares method; empirical Bayes estimation; error model identification; generalized diagonal ridge estimation; orthometric accelerometers; Accelerometers; Accuracy; Equations; Estimation; Least squares methods; Mathematical model; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633241
Filename
5633241
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