Research Article

Method for Predicting Failure Rate of Airborne Equipment Based on Optimal Combination Model

Table 2

Input data model and error data table.

Model and deviationMAERMSEMAPEMSPENRMSER2

MLR0.37820.489441.371.47490.52310.899
GM(1,N)0.33630.365934.381.14080.38960.910
PLS0.33590.201315.210.41990.20560.928
BP0.17490.418428.311.00940.30920.964
SVM0.45140.524848.211.53980.42710.909