Abstract
Gas turbine engines are widely used in many industrial applications and engine condition monitoring is a vital issue for the aircraft in-service use and flight safety. From the variety of condition monitoring methods, the model-based approach is perhaps the most promising for real-time condition monitoring. This approach can predict the engine characteristics at the expense of algorithmic redundancy and requires real-time simulation. The main obstacles for using full thermodynamic models in the engine condition monitoring schemes are high computing load, and inability to incorporate unforeseen changes.
Original language | English |
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Title of host publication | Efficient Modeling and Control of Large-Scale Systems |
Place of Publication | Boston, MA |
Publisher | Springer |
Pages | 89-111 |
Number of pages | 23 |
ISBN (Electronic) | 9781441957573 |
ISBN (Print) | 9781441957566 |
DOIs | |
Publication status | Published - 11 May 2010 |
Externally published | Yes |
Keywords
- Condition Monitoring
- Equation Error
- Reduce Order Model
- Output Error
- Actuator Fault