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Identification of multivariable high performance turbofan engine dynamics from closed loop dataThe multivariable instrumental variable/approximate maximum likelihood (IV/AML) method or recursive time-series analysis is used to identify the multivariable (four inputs-three outputs) dynamics of the Pratt and Whitney F100 engine. A detailed nonlinear engine simulation is used to determine linear engine model structures and parameters at an operating point using open loop data. Also, the IV/AML method is used in a direct identification mode to identify models from actual closed loop engine test data. Models identified from simulated and test data are compared to determine a final model structure and parameterization that can predict engine response for a wide class of inputs. The ability of the IV/AML algorithm to identify useful dynamic models from engine test data is assessed.
Document ID
19820012465
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Engineering (General)
Report/Patent Number
NASA-TM-82785
NAS 1.15:82785
E-1120
Report Number: NASA-TM-82785
Report Number: NAS 1.15:82785
Report Number: E-1120
Meeting Information
Meeting: IFAC Symp. on Identification and System Parameter Estimation
Location: Washington, DC
Country: United States
Start Date: June 7, 1982
End Date: June 11, 1982
Accession Number
82N20339
Funding Number(s)
PROJECT: RTOP 505-32-6B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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