2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics 2010
DOI: 10.1109/isscaa.2010.5633241
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Application of Empirical Bayes Estimation in Error Model Identification of Two Orthometric Accelerometers

Abstract: The high accuracy accelerometer can be demarcated in multiposition tumbling experiment under 1g gravitational field. The g 2 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 experime… Show more

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