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
Link To Document :
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