Distributed control system with smart actuators and sensors

作者: Richard J. Skertic

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摘要: A system for controlling operation of an aircraft engine includes a master controller, control node coupled to component the and wherein computing device performing diagnosis component. The is configured assess performance during aircraft, determine whether within specification, if not indicate that out specification.

参考文章(26)
Malcolm John Ashby, Sridhar Adibhatla, Methods and apparatus for model based diagnostics ,(2000)
James Saloio, Frequency based fault detection ,(2011)
Matthew William Wiseman, Malcolm John Ashby, Model-based iterative estimation of gas turbine engine component qualities ,(2006)
David M. Mathis, Gary A. Farnsworth, Glenn H. Lane, Louie T. Gaines, Paul S. Evans, Calvin C. Potter, Casey Hanlon, David M. Eschborn, Aircraft accessory monitor ,(2003)
Jesse Floyd Stewart, Mariateresa Paci, Antonio Asti, Giovanni Tonno, Systems and methods for using a combustion dynamics tuning algorithm with a multi-can combustor ,(2011)
Jianbo Zhang, Karl Dean Minto, Erhan Karaca, Methods and systems for neural network modeling of turbine components ,(2008)