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Feedback linearization for control of air breathing enginesThe method of feedback linearization for control of the nonlinear nozzle and compressor components of an air breathing engine is presented. This method overcomes the need for a large number of scheduling variables and operating points to accurately model highly nonlinear plants. Feedback linearization also results in linear closed loop system performance simplifying subsequent control design. Feedback linearization is used for the nonlinear partial engine model and performance is verified through simulation.
Document ID
19910057048
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Phillips, Stephen
(Case Western Reserve University Cleveland, OH, United States)
Mattern, Duane
(NASA Lewis Research Center Cleveland; Sverdrup Technology, Inc., Brook Park, OH, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 91-2000
Accession Number
91A41671
Funding Number(s)
CONTRACT_GRANT: NAG3-1232
Distribution Limits
Public
Copyright
Other

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