Abstract
The model-plant performance matching of aircraft engine can be used to solve several problems, such as fault diagnosis, model calibration and deterioration estimation etc. A partially mixed high bypass ration turbofan in civil aviation is modeling in simulating environments to constitute a model-plant performance matching benchmark. Depending on the nonlinear thermodynamic model between measured residuals and health factors, the regularization method with parameter competitive criterion is used to optimize the object value of components health factors. Several sets of simulated deterioration and fault data are naturalized as the invaliding cases, the better matching of model-plant is obtained from the simulating results.
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Wang, L., Zhong, D. (2011). Regularization Method Combined with Parameter Competitive Criterion for Model-Plant Performance Matching of Aircraft Engine. In: Liu, C., Chang, J., Yang, A. (eds) Information Computing and Applications. ICICA 2011. Communications in Computer and Information Science, vol 243. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-27503-6_90
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DOI: https://doi.org/10.1007/978-3-642-27503-6_90
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