Research Article

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

Table 3

Experiment results of sensor measurements estimation during dynamic process.

Sensor fault during dynamic processRDEstimation
time/ms

sensor 0.00300.00220.00140.00210.00510.0280.6122
sensor0.00320.00280.00180.00260.00530.00260.6391
sensor0.00350.00200.00160.00200.00450.00230.6384
sensor0.00340.00260.00100.00190.00530.00220.6402
sensor 0.00380.00240.00180.00180.00510.00270.6431
sensor0.00360.00300.00170.00210.00460.00290.6128