Aircraft Gas Turbine Engine Health Monitoring System by Real Flight Data

Table 10

ANOVA results for EGT training.

	ANOVA^a
Model	Sum of squares	df	Mean square	F	Sig.
1
Regression	12753394.90	8	1594174.363	1939.432	0.000^b
Residual	818692.113	996	821.980
Total	13572087.02	1004

^aDependent variable: exhaust gas temperature. ^bPredictors: (constant), ground/air, vertical acceleration, pitch, roll, angle of attack, total air temperature, N2 speed, and N1 speed.