Analytical Redundancy Design for Aeroengine Sensor Fault Diagnostics Based on SROS-ELM

Table 2

Experiment results of sensor measurements estimation under steady state.

Sensor fault under steady state	RD						Estimation time/ms
	sensor	0.0020	0.0021	0.0012	0.0018	0.0034		0.0023	0.6657
sensor	0.0017	0.0023	0.0015	0.0020	0.0036	0.0025	0.6654
sensor	0.0022	0.0021	0.0013	0.0016	0.0033	0.0021	0.6669
sensor	0.0016	0.0025	0.0016	0.0021	0.0038	0.0019	0.6660
sensor	0.0018	0.0028	0.0011	0.0019	0.0032	0.0020	0.6706
sensor	0.0016	0.0024	0.0014	0.0016	0.0035	0.0022	0.6693