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 process | RD | Estimation time/ms | | | | | | |
| sensor | 0.0030 | 0.0022 | 0.0014 | 0.0021 | 0.0051 | 0.028 | 0.6122 | sensor | 0.0032 | 0.0028 | 0.0018 | 0.0026 | 0.0053 | 0.0026 | 0.6391 | sensor | 0.0035 | 0.0020 | 0.0016 | 0.0020 | 0.0045 | 0.0023 | 0.6384 | sensor | 0.0034 | 0.0026 | 0.0010 | 0.0019 | 0.0053 | 0.0022 | 0.6402 | sensor | 0.0038 | 0.0024 | 0.0018 | 0.0018 | 0.0051 | 0.0027 | 0.6431 | sensor | 0.0036 | 0.0030 | 0.0017 | 0.0021 | 0.0046 | 0.0029 | 0.6128 |
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