Proceedings of International Conference on Control Applications
DOI: 10.1109/cca.1995.555740
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Continuous time identification of turbine system

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Cited by 2 publications
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“…The states are high pressure speed x 1 , low pressure speed x 2 , nozzle area x 3 , and fuel flow rate x 4 measured in bars, inches 2 , kg/sec, and seconds, respectively. Our signal v is the referenced fuel flow rate [17].…”
Section: Gas Turbinementioning
confidence: 99%
“…The states are high pressure speed x 1 , low pressure speed x 2 , nozzle area x 3 , and fuel flow rate x 4 measured in bars, inches 2 , kg/sec, and seconds, respectively. Our signal v is the referenced fuel flow rate [17].…”
Section: Gas Turbinementioning
confidence: 99%