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Output feedback regulator design for jet engine control systemsA multivariable control design procedure based on the output feedback regulator formulation is described and applied to an F100 turbofan engine model. Full order model dynamics, are incorporated in the example design. The effect of actuator dynamics on closed loop performance is investigated. Also, the importance of turbine inlet temperature as an element of the dynamic feedback is studied. Step responses are given to indicate the improvement in system performance with this control. Calculation times for all experiments are given in CPU seconds for comparison purposes.
Document ID
19780040989
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Merrill, W. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: National Electronics Conference
Location: Chicago, IL
Start Date: October 13, 1977
End Date: October 14, 1977
Accession Number
78A24898
Distribution Limits
Public
Copyright
Other

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