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Design, evaluation and test of an electronic, multivariable control for the F100 turbofan engineA digital, multivariable control design procedure for the F100 turbofan engine is described. The controller is based on locally linear synthesis techniques using linear, quadratic regulator design methods. The control structure uses an explicit model reference form with proportional and integral feedback near a nominal trajectory. Modeling issues, design procedures for the control law and the estimation of poorly measured variables are presented.
Document ID
19800017817
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Skira, C. A.
(Systems Control, Inc., Palo Alto Calif., United States)
Dehoff, R. L.
(Air Force Aero Propulsion Lab. Wright-Patterson AFB, OH, United States)
Hall, W. E., Jr.
(Systems Control, Inc., Palo Alto Calif., United States)
Date Acquired
August 10, 2013
Publication Date
February 1, 1980
Publication Information
Publication: AGARD Advan. Control Systems for Aircraft Powerplants
Subject Category
Aircraft Propulsion And Power
Accession Number
80N26316
Distribution Limits
Public
Copyright
Other
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