Optimal Tuner Selection for Kalman-Filter-Based Aircraft Engine Performance Estimation

@inproceedings{2011OptimalTS,
  title={Optimal Tuner Selection for Kalman-Filter-Based Aircraft Engine Performance Estimation},
  author={},
  year={2011}
}
  • Published 2011
An emerging approach in the field of aircraft engine controls and system health management is the inclusion of real-time, onboard models for the inflight estimation of engine performance variations. This technology, typically based on Kalman-filter concepts, enables the estimation of unmeasured engine performance parameters that can be directly utilized by controls, prognostics, and health-management applications. A challenge that complicates this practice is the fact that an aircraft engine’s… CONTINUE READING
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