Aero-Engine Fault Diagnosis Using Improved Local Discriminant Bases and Support Vector Machine

Table 1

Results of the experimental study.

Target classes	Sample size	Recognition results			Recognition rate [%]	Total [%]
		Faultless	Rub-impact	Unbalance
Faultless	20	20	0	0	100	100.00
Rub-impact	20	0	20	0	100
Unbalance	20	0	0	20	100