A Modified Least Squares Estimator for Gas Turbine Identification
Aero propulsion technical memo.
AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)
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A simple estimator is proposed for use in extracting the spool dynamic characteristics of a gas turbine engine. It provides realistic estimates even when the inputoutput signals are contaminated by high levels of measurement noise. As a result, it has the potential to form the basis of a useful engine health monitoring tool. Keywords Parameter estimation Transient response Jet engines Fault diagnosis Australia.
- Jet and Gas Turbine Engines